International Gas Turbine Congress 2011 Osaka
1. Overview

introduction to the research activities of 14 laboratories from 10

The 10th International Gas Turbine Congress (IGTC '11)

universities was presented. The total number of visitors to thesponsored by the Gas Turbine Sciety of Japan (GTSJ) was heldfour-day event exceeded 3950, which substantiated its

in Nakanoshima, Osaka, at the Osaka International Convention

popularity due to the events planned by the exhibitors who

Center (Grand Cube Osaka, GCO) for six days from Sunday,

volunteered.

November 13, to Friday, November 18, 2011. As was theprevious conferences of this series, this event was presented incollaboration with International Gas Turbine Institute (IGTI) of
the American Society of Mechanical Engineers (ASME), theJapan Society of Mechanical Engineers (JSME), the Japan
Society for Aeronautical and Space Sciences (JSASS), and other10 academic societies and organizations from around the world
including United Kingdom, Germany, France, Korea, in
addition to 25 domestic academic societies and organizations.
This conference marked the first one to be hosted by GTSJ after
its transition into a public interest incorporated association in
2011. Marking an increase of 36 percent from the previous 2007
conference's enrolment, registered attendees for this event
totaled 481, with 368 from Japan and 113 from 19 countries
overseas, to truly define the term “international congress.”

Photo 1.1

Congress venue at the Osaka International

The opening lecture on the first day of theConvention Center

conference was a plenary talk commemorating the 10th
congress offered since the initial 1971 event and celebrating 40

A total of 192 technical papers including keynote

years of gas turbine development. A commemorative photospeeches and so forth were presented at this conference, 106

exhibition was also presented as a retrospective of the previous

from Japan and 86 from other countries, which represented anine conferences. In addition, three gas turbine lectures were

40% increase over the previous conference. The lectures were

offered free of charge to high school students, university

lively with numerous participants.

students, and the general public. All exhibits and lectures wereSeven lectures were given on the following topics

successful.

during the keynote speech: (1) Shape Optimization of Casing
Several events planned to enliven the conference

Treatment for a Transonic Axial Compressor to Improve

included a welcome reception, a banquet, and plant tours. All

Operating Stability; (2) New Directions in Turbomachinery

were very successful and attracted many participants. The

Aero-Acoustics; (3) Boosting and Turbocharger Needs for

exhibition, held on the 10th floor of GCO, featured 79 booths

Highlyfrom 39 organizations and offered information on such topics asTechnologies for Concentrated Solar Power Systems and Steamactual gas turbines and models, turbo-superchargers, related

Turbines; (5) Fluid Dynamic Efficiency Optimization of Steaminstrumentation, numerical analysis software. In addition, an

Turbine Stages Considering Leakage Influences and Inter-stage

1

Downsized

Low

Carbon

Vehicles;(4)

RecentReciprocal Interferences; (6) A Suggested Mechanism ofcycles. In addition, this conference included a new theme: 13

Significant Stall Suppression by Air Separator Devices in Axial

papers were presented on steam turbines, which prompted lively

Flow Fans; and (7) Aerodynamic Losses in Turbines With anddiscussion.

Without Film Cooling.

Several events were offered during the conference,

Two plenary talks were given on the following

including a welcome reception attended by approximately 100

topics during the plenary talks: (1) Recollection on the Progress

and a banquet in the Sanraku-no-Ma hall at the Rihga Royalof IGTC over 40 years and (2) Europe's Framework Programme

Hotel attended by more than 190.

for Research in the Field of Aeronautics and Air Transport.

Plant tours with separate destinations were arranged.

Three plenary invited lectures were given on the following

For Tour-1, 27 people visited Senboku LNG Power Plant of

topics: (1) NASA's Future Propulsion Systems Research andOsaka Gas and Sakaiko Power Station of Kansai Electric Power.

Development; (2) Advanced Aeroengine Technologies toTour-2 brought 38 people to the Mitsubishi Heavy Industries

Reduce the Effect of Aviation on the Environment; and (3) How

Co., Ltd., Takasago Factory and Takasago Machinery Works of

to Develop Sustainable Low-Carbon Society (LCS) for Japan

Mitsubishi Heavy Industries and Akashi and Seishin Works ofand Asian Countries? -Model Simulation and Roadmap-. The

Kawasaki Heavy Industries.

special talks consisted of: (1) Learn to Think Like an Expert and

The success of IGTC '11 seemed to have overridden(2) My Hope in Young Gas Turbine Professionals -Approach tothe country’s recent difficulties, including the Great East Japan

Technical Opportunities-.

Earthquake, the nuclear disaster at the Fukushima Daiichi

Two panel discussions and two forums were held on

Nuclear Power Plant, and the sudden appreciation of the

topics: (1) Trends in Aero Engine Technology Associated withJapanese yen, and is attributed to the efforts of collaborating andEnvironmental Issues and CO2 Reduction (Short- and Mid-Termcooperating organizations both from Japan and overseas,

Strategy); (2) CO2 Reduction in Power Plants; (3) Trends inparticipating companies, and the society members. The total

Aero Engine Technology Associated with Environmental Issues

number of participants came to 481 people and 192 papers were

and CO2 Reduction (Long Term Strategy); and (4) Asian Energy

presented. This series of congresses has been held nearly onceand Environmental Strategy.

every four years since 1971 and has truly become an

During the technical session, 172 papers wereinternational conference in both name and actual meaning. Itspresented in 66 sessions excluding three cancelations. The

success demonstrates its worldwide recognition as therooms for the technical sessions were concentrated on the 10th

preeminent international conference concerning gas turbine

and 12th floors of the venue. Although the presentations ran

technologies in Japan. We hope to see the continued prosperity

concurrently in eight rooms, the audience members were able toof this congress as a forum for international exchange in tandem

move among the rooms smoothly. A spirited debate took placewith the ongoing development of gas turbines.

regarding the results of the latest research and development overa wide range of disciplines in various themes relative to gas
turbines, which included practical development and axial fans inaddition to such technologies in centrifugal and axial flow
compressors; centrifugal and axial flow turbines; fuel andcombustion; turbine cooling; noise, shaft, and blade vibration;
coating materials; computational fluid dynamics (CFD);
operations and maintenance; control and measurement; and new2

retrospective and memorial photo exhibition organized by IGTC
2003 Executive Committee Chairman and professor emeritus
Osamu Kawaguchi (Keio University). The third was theimplementation of an open seminar for the general public,
offered by Professor Toshinori Watanabe (University of Tokyo) ;Mr. Hisao Futamura (Japan Aerospace Exploration Agency,
JAXA); and Mr. Tsukasa Yoshinaka (formerly of Pratt and
Whitney, Canada, PWC). The three lectures were planned
during the IGTC ’11 executive committee meeting, and final
Photo 1.2

preparations were conducted by the authors.

Participants of the Gas Turbine Open Seminar heldon the first day of the conference

2.2 Plenary Talk 1
Because this conference was the 10th since the first
International Gas Turbine Congress was held in Tokyo in 1971,
a memorial talk titled ”Steps of IGTC; from 1st to 10th, with
Background of Gas Turbine R&D in Japan“ was given byprofessor emeritus Eisuke Outa (Waseda University). This
lecture detailed the history and technological developments ofgas turbines in Japan during the past 40 years and traced theevolution of this series of international conferences. The
following is a summary of the memorial lecture:
Photo 1.3

In the period immediately after World War II, when

Banquet performance featuring koto musicgas turbine development and production was prohibited, Japanby Ken-ichiro Takeishi (Osaka University)

lost much of its gas turbine-related technology and researchfacilities. However, the continuing efforts of those involved inresearch and development led to the first International Gas

2. Events Commemorating the 10th Congress
2.1 Lecture Marking the 10th Congress

Turbine Congress, which was held in 1971. Subsequently, Gas

IGTC ’11 represents a milestone in that it marks both the 10th

Turbine Committee of Japan was established in 1972, and laterinternational conference as well as the 40th anniversary sincein 1976 became the Gas Turbine Society of Japan. Since then,the first congress was held in 1971. Although no special

this series of international conferences has been held every fourannouncement was made, three events differing from thoseto six years.

implemented in the past were planned and conducted to

The current practice of offering an exhibition inrecollecting the past memories and to position the congress inconjunction with technical sessions and lectures began with thethe future perspectives.

first conference. With the advancements of gas turbine

The first was the plenary talk offered by IGTC 2007

development in Japan, the congresses have attracted many

Executive Committee Chairman and professor emeritus Eisuke

participants from all over the world to present their technicalOuta (Waseda University) to present the memorial lecture

papers as well as built up a cooperative relationship with many

recollecting the 40 years progress of IGTC. The second was theacademic societies and industrial organizations overseas, and3

the series of conferences has been recognized a truly

2.3 Memorial Photo Exhibitioninternational congress.

Held to commemorate the 10th IGTC, the photo exhibition

At each of the international conferences, special

offered general descriptions and scenes of the lecture, exhibition

lectures and panel discussions were addressed by researchers

halls, banquets, and tours from each of the previous nineand experts from various countries to address cutting-edge

conferences from 1971 to 2007. The materials and statistics fortechnologies and industrial challenges. Each conference alsoeach congress were summarized in one poster, and each poster

provided social events such as welcome reception, banquet andwas displayed together with proceedings, abstracts, circulars,

plant tours in addition to opportunities to exchange informationand other items memorable (Photo 2.2). The posters werein a wide range of technical fields.

exhibited in a room on the 10th floor, where the exhibitions by

The speaker addressed that behind the continuously

college students were held.

holding the series of international conferences there have been
numerous

privatesectorsandresearch

The same posters also were displayed on the wallorganizations

next to the registration desk in front of the main hall on the 12th

participating into various national projects related to gas

floor during the whole congress period. Because the main hallturbines, and that the outcomes have been supporting

was a gathering place for many conference participants, thedevelopment and progress of advanced gas turbine technologies

exhibition became a focal point for nostalgia and reflection. In

serving as the backbone of Japanese industries along with someconjunction with the previously mentioned memorial lecture,

historical context. Through these efforts, Japan’s gas turbine

this display offered an opportunity to recall the accumulation oftechnology continues to be employed in a number of disciplines

technology and human interaction of the previous 10

such as power generation equipment including for emergency

conferences. Since participants seemed to express enthusiasm

services, co-generation equipment, and aircraft engine. The

for the next conference, the 11th, we believe this photo

nation's gas turbine technology proved itself reliable particularly

exhibition was a significant milestone. In the future, we wouldin the aftermath of the Great East Japan Earthquake.

like to continue to feature these and future photographs toSummarizing the advancement and development ofpreserve a record of the conference’s academic activities.

gas turbine-related technologies in connection with the previous
40 years of the conferences, the contents of the talk were ofgreat interest to participants, particularly young engineers andresearchers, and will likely serve as useful references in future
research and development.

Photo 2.2

Exhibits and display panels

2.4 Gas Turbine Open Seminar for the General Public
On November 14 (Monday) in the special conference hall, a
Photo 2.1

Plenary talk marking the 10th congress

public seminar was held to introduce gas turbine technology tohigh school, college, and university students, in addition tomembers of the general public. In 2011, gas turbine technology

4garnered the nation-wide attention, and we aimed to enhance the“The Evolution and Future of the Jet Engine—The

substance of these lectures so that members of the general

Heart of an Airplane” was the last of the three lectures for the

public, particularly young people, would have an opportunity togeneral public and was given by Mr. Tsukasa Yoshinaka

understand the effectiveness and consider the benefits of thisformerly of PWC. He began by describing the historicaladvancement. Hence, we invited three experts to present

backgroundlectures beginning with an overall summary of the gas turbine

commercialization, then cited some of the current challenges

and how it relates to power generation, in addition to theregarding jet engines and discussed the future of geared fans andhistorical and future significance in Japanese aviation engine

open rotors. Of particular interest to many members of the

production as well as the history and ongoing technological

general public in the audience, Mr. Yoshinaka completed his

development in the world. Although the lectures for the generallecture by drawing comparisons between the fuel efficiency of

public were held during the international conference, 149

aircraft and automobiles, citing the new A380 as an example.

students were included among the participants.

of

the

rapidity

of

turbo

fan

engineFollowing the lecture session, members of the

The moderator, Mr. Nozaki, opened the seminar byaudience

posed

questionsconcerningtechnologicalintroducing the three lecturers, after which time the lecturesdevelopments in the United States after World War II and thewere held in a relay format.

future rise in temperature of the combustor. Both lecturers gave

The first lecturer was Professor Toshinori Watanabe

concise answers, satisfying both professionals and members offrom the University of Tokyo. In his lecture titled “Thethe general public.

Mechanisms of Gas Turbines—The Source of Electrical and Jet
Power,” he described the makeup and varieties of gas turbines
used for electrical power generation and aviation. In addition, he
addressed current challenges, citing examples of gas turbine
usage during the Great East Japan Earthquake. Professor
Watanabe went on to elucidate concretely about the future
direction of gas turbines. His summary was compact,encompassing a wide range of topics dense with information for

Photo 2.3

Lecturers for the gas turbine open seminarboth students and professionals, and his brief explanation was
followed by lectures from the two speakers.

by Terutaka Fujioka (CRIEPI), Kei-ichi Okai (JAXA),

The next speaker was Mr. Hisao Futamura of JAXA,

Takeharu Hasegawa (CRIEPI), and Osamu Nozaki (JAXA)

whose lecture titled “Go Japan! With Your Craftsmanship Soarin the Sky" focused on the history of jet engine development in

3. Special Lectures, Panels & Forums

Japan. He spoke on the manner in which acquired technological

3.1 Plenary Talks

development knowledge helped to realize the development of

Two separate plenary talks were organized. The details for thethe V2500 with international cooperation, and he revealed thatfirst plenary talk, which commemorated this 10th international

Japan’s technology is at a world-class level in the field ofconference, can be found in Chapter 2. The following is a

individual component manufacturing technology. Mr. Futamurasummary of plenary talk 2.

also addressed the importance of aviation industry for Japan’s

Plenary Talk 2: Europe's Framework Program for Research ineconomy and emphasized the importance of harnessing thethe Field of Aeronautics and Air Transport

traditional fundamental technologies for the country’s future.

Dr. Denos of the European Commission began his title plenary5

talk immediately following the forum on the long-term strategy

technologies

inspace,

communicationsof environmental technology relative to aircraft engines. In his

development,

andtalk, Dr. Denos introduced aviation-related research currently

conversion. In addition, the lecture touched on economic

being conducted under the Seventh Framework Programme andefficiency in the field of aviation and environmentalsummarized the joint research program recently establishedcompatibility with a focus on safety. Dr. Hah went on to cite

between Japan and Europe. In addition, he described futuretargets of approximately 70% in fuel savings; a 75% reduction

collaborative prospects.

of NOx; a 90% reduction in noise using drag/lift mechanisms;

materials andtechnology

structure

for

and

extremeThis program, which encompasses the framework oflightweight constructions; laminar flow wings; fuel-compatible,

European research and development across all science andlow NOx burners; open rotors; ultra-high bypass ratio turbofans;technology-related fields, was started in 2007 and is scheduled

aerodynamic

to run until 2013. It has been allocated approximately 140

implementation.

million euros per year in funding for aviation-related projects

Plenary

divided into four groups: the environment, including global

Technologies to Reduce the Effect of Aviation on thewarming strategies and emissions; economic efficiency; energy,

Environment

including fuel efficiency and alternative fuels; and societal

This discussion was planned with the intention of introducing

aspects, including low-cost fares, safety, and punctuality. Its

the latest technology of aircraft engines and was designed toresearch topics include the aerodynamic characteristics ofaddress environmental concerns. The scheduled lecturer wasaircraft,propulsion

Professor Parker of Rolls-Royce Inc.; however, he was unable totechnology, alternate fuels, and design systems, in addition toattend. Taking his place was Dr. Simon Weeks, also ofgearedinverted

Rolls-Royce Inc.

open-rotor fans, and regenerative intermediate cooling systems.

The

new concepts,

turbofancomposite

sophistication,materials,

inverted

fans,

sound

Invitedshieldstructures;

Lecturelecture

2:

topic

and

distributed

Advanced

Aeroengine

includedanoverview ofFurther, publicly offered research proposals were introduced inenvironmental compatibility constraints imposed on aircraft

2012. The coordinated call with Japan’s (L1) applied researchengines

program was to be funded with 400 million euros from Europe

eco-technologies on which Rolls-Royce is currently working.

and Japan.

After touching on trends in CO2 and SFC reduction, Dr. Weeks

andintroduced

some

of

the

fundamental

presented examples of those developmental technologies,
3.2 Plenary Invited Lectures

including open rotors, lean-burn technology, biofuel use,

Three plenary invited lectures were planned for this conference.

integrated electronic control systems, and advanced cycle

Plenary Invited Lecture 1: NASA’s Future Propulsion Systems

technologies. This lecture renewed the belief of participants that

Research and Development.

multifarious approaches are available for environmental

Mr. Ramon Lugo of NASA’s Glenn Research Center (GRC) was

responsiveness. In addition, Dr. Weeks also made it clear thatscheduled to give a lecture on trends in NASA research andthe spirit of Rolls-Royce has not changed since Charles Rolls

development of propulsion systems. However, due to an

and Henry Royce first met in 1904 and that the company will

emergency, he was unable to make the trip to Japan. The lecture

continue to meet challenge in developing innovative aircraft

was given instead by Dr. Chunill Hah, also of NASA’s GRC.

engines.

The topics of by Dr. Hah lecture included

Plenary Invited Lecture 3: How to Develop a Sustainable

air-breathing propulsion, in-space propulsion and cryogenic

Low-Carbon

fluidsCountries—Model Simulation and Roadmap

management,

physicalscienceandbiomedical

6

Society

(LCS)

for

Japan

and

Asian

The theme of plenary invited lecture 3 addressed urgent global

3.3 Special Talks

environmental issues. In this lecture, Dr. Fujino of the National

Two special talks were scheduled.

Institute for Environmental Studies discussed a plan for AsianSpecial Talk 1: Learn to Think Like an Expert

nations, particularly Japan, to develop future low-carbon

Dr. Wisler, formerly of GE Aviation, newly appointed atsocieties and to incorporate simulation research results to ensure

IGTC ’11 as an honorary member of the Gas Turbine Society of

progress toward that goal.

Japan, gave a presentation concerning engineering education.

Dr. Fujino stated that if the policy objectives toThis lecture analyzed in detail the differences

mitigate global environmental issues can be summed up in the

between technology experts and novices from the perspective of

3E philosophy—energy, environment, and economy—theknowledge

concept of security could be added to create a 3E+S philosophy.

methodologies required to become an expert. Dr. Wisler said it

On this basis, he said, we should the pursue a 3S

is possible to solve a problem by clearly distinguishing facts,

philosophy—smart, secured, and sustainable—with the addition

concepts, and generalizations in a variety of information.

of resilience, or 3S+R. Dr. Fujino said it is precisely now, in theExperts organize technical information into a conceptual

wake of the Great East Japan Earthquake, that we areframework and capture the individual design issues andexperiencing vulnerability in our energy supply, marked by our

problems into a pattern, then comprehensively consider the

reliance on only stockpiled crude oil reserves, and that weelements of that structured information. In contrast to thisshould recognize the necessity of constructing distributed

approach, novices try to solve each individual problem and issueenergy systems to maintain, at a bare minimum, thein a piecemeal fashion. Engineers should acquire the ability to

independence and stability of each region.

think like an expert. As such, they build a structured body ofstructureanddiscussed

simplepointsandScenarios for a low-carbon society have promoted

knowledge, and when faced with new phenomena or problems,“emphasizing harmony with the natural environment” andthey employ critical thinking and the ability to make decisive“reliance on advanced technology.” However, the challenges we

judgments incorporating a body of knowledge. He pointed out

should undertake in the future have shifted to the importance of

there is a fundamental limit to the conventional methods ofa social system design that incorporates the benefits ofthinking taught in universities, particularly in the memorization

technological advances and the creation of mechanisms toof formulas and theories. It is necessary to develop educational

implement regional societies with highly resilient regenerative

programs that involve practical, hands-on knowledge andpower.

lessons that students can experience for themselves.

Photo 3.1

Plenary invited lecture 1

Photo 3.2

7

Dr. Wisler giving his dynamic lecture

Special Talk 2: My Hope in Young Gas Turbine Professionals:

mid-term

strategies

Approach to Technical Opportunities

environmental issues.

ofaeroengines

and

their

role

in

To begin, Mr. Yamaguchi from the Ministry of Land,

Mr. Tsukasa Yoshinaka, formerly of Pratt & Whitney, Canada,

Infrastructure, and Transport spoke from the perspective ofgave a presentation for students and young engineers.
Mr. Yoshinaka began his lecture by first showing

formulating environmental regulations. He requested a 2%

how to quantify expected increases in cycle and output

annual improvement in fuel efficiency for international aviation

efficiency by improving the efficiency of the compressor andand explained that the preparations for CO2 regulation are

turbine, thus increasing pressure ratio and turbine inlet

continuing to advance. Next, Dr. Epstein from Pratt & Whitney

temperature. He stated that this task is not simple, but it may be

spoke regarding the development of the geared turbofan engine

possible. To address these issues in the short term, one can learn(GTF) and its merits over previous engines, including low fuelfrom past successes and failures. In the long term, however,consumption and noise reduction. Dr. Weeks of Rolls-Royceoutside-the-box thinking is necessary. He then presented an

discussed two separate paths by discussing the trade-off

example of thermal energy conversion with boundary layer

between the two contradictory problems of CO2 and noise. In

control and semiconductors using ultrasonic waves. In addition,

the open rotor design, which is inferior in noise reduction, theMr. Yoshinaka explained that there are both grounds and context

reduction in fuel consumption drastically reduce CO2 emissions;for established design criteria, and it is necessary to improve

however, the turbofan engine design, which produces much lessand optimize on the basis of a good understanding of thosenoise, is inferior in reducing CO2 emissions. From the IHI, Dr.

underlying principles. In addition, he mentioned the following

Kodama spoke of the importance of reducing CO2 emissions by

example: Accurate loss estimates in light loads use current

reducing fuel consumption and outlined the status of technology

computational fluid dynamics (CFD), whereas heavy loads

development toward an optimization of turbine and fan parts

make such estimation difficult. That is, it is not sufficient toconstructed of lightweight composites such as carbon fiber

overly depend on CFD; a physical understanding of the basic

reinforced composites and ceramic matrix composites. Mr. Saitointernal flow of turbomachinery is also important.

from JAL reported on social activities regarding the

He also explained with an actual example of theenvironment by discussing the results of JAL’s biofuel flight test

Great East Japan Earthquake that a great number of people’s

results and the current status of biofuels. Mr. Noguchi of ANA

lives and livelihoods deeply connected to gas turbine technology,

discussed the progress of the ANA group’s ecology plan, which

as is global climate change. Mr. Yoshinaka ended his lecture

took place from 2008 to 2011 and set targets to reduce CO2

with the following plea to young technologists: “I want you toemissions. Following the discussions, Mr. Kanai from thetake up the challenge of solving these problems; they are both

Ministry of Economy, Trade, and Industry gave a shortdifficult and worthwhile.”

endorsement speech announcing the continued government
support for advanced technology development to reduce

3.4 Panel Discussions

environmental impacts.

Two panel discussions were also scheduled.

Panel Discussion 2: CO2 Reduction in Power Plants

Panel Discussion 1: Trends in Aeroengine Technology

On the final day of the convention, a panel discussion was held

Associated With Environmental Issues and CO2 Reduction:with the theme of low carbon from the power generation sector

Short- and Mid-Term Strategies

by three experts active in their own respective fields.

Six panelists were invited to partake in the first panel discussion,

To begin, discussion moderator Professor Nakata ofthe theme of which was a general overview of short- andTohoku University provided the audience with an introduction

8

to the topics to be discussed, which included a comparison of

Mr. Suzuki from Toshiba introduced the latest trends

energy and carbon flows between the United States and Japan,

in carbon dioxide capture and storage technology. He discussed

scenario analysis methodology, the significance of technicalthe features and future outlooks of three types of carbon capture

proficiency, and expectations for future innovation. Professor

technologies

Abharilong-term

pre-combustion capture, constant pressure combustion capture,

retrospective on the history of man’s environment and suggested

and oxygen combustion capture. The discussion prompted

future actions. Kepco’s Mr. Toyama discussed the expectations

listeners to recognize and consider the economic and socialof the efficiency of thermal power generation from an electric

aspects associated with the introduction of low carbon

utility industry perspective. He presented concrete examples oftechnologies after opinions were raised concerning thetechnology improvements and industry goals such as improving

management of advanced engineer training, financial aspects,

the thermal efficiency of gas-combined thermal power

thegeneration, upgrading pulverized coal thermal power generation,

environmental ethics and social acceptance for CO2 capture.

of

ETH

subsequently

presentedacurrently

importance

of

under

development:

governmental

policy,high-pressure

andensuredand implementing clean coal technologies such as IGCC.

Photo 3.3

Panel discussion 2

3.5 Forums

considerations, the fate of both will be decided by engine

Two forums were held during this conference.

improvements. The organization’s long-term plan is to examine

Forum 1: Trends in Aeroengine Technology Associated with

the introduction of electric-powered aircraft as well as

Environmental Issues and CO2 Reduction

high-temperature heat-resistant materials.

A forum on the long-term strategy for aviation engine

Dr.

Denos

from

the

EuropeanCommission

technology was held to introduce long-term plans of the United

represented Europe. It was stated that the EU’s efforts are to

States, Europe, and Japan.

realize an 80% reduction of NOx, a 50% reduction in noise, and

The American presentation was given by NASA’s

a 50% reduction in CO2, and that the commission is

Kenneth L. Suder. It was addressed as follows. The

endeavoring to introduce a new thrust mechanism moreorganization’s aviation sector has already set targets for noise,technologically advanced than the GTF, in addition toNOx, and fuel consumption and has begun a number of studies

technologies,

to realize those goals. With respect to airframe and wings,

three-dimensional wing design, etc., which are likely to bealthough both the advanced and integrated formats are underrealized in the short to medium term.

9

such

as

the

control/preventionofstalls,Dr. Nishizawa from Japan’s JAXA presented fornatural gas, would remain for the foreseeable future. In addition,

Japan. He stated that realization of the high bypass ratio that

the EU representative commented that 30 years would be

would contribute to an improvement in engine performancenecessary for the integration of hydrogen-related technologies

would necessitate considering, at the research level, ideas suchand that the installation of hydrogen supply systems to airports,

as a new form of an elliptically shaped engine.

for example, would be a lengthy process. On the contrary, theAn audience member raised a question on the

JAXA representative offered encouraging remarks. He said thepossibility of using hydrogen as a fuel. In response, the NASAagency’s rocket department has a proven history of handling

representative said although this concept would be challenging,hydrogen and that the long-term outlook of hydrogen as fuel ishydrogen is the only viable long-term solution. However, hepossible.

added that the current usage of hydrocarbon fuels, particularly

Photo 3.4 Forum 1

that began in the late 1970s and early 1980s.
South Korea’s Professor Kim from Inha University

Forum 2: Asian Energy and Environmental Strategy
In recent years, the energy situation in Asian regions has

discussed his country’s energy status and outlined strategies forbecome unclear due to China’s rapid economic development.

the future. South Korea depends almost entirely on imported

Energy issues have become significant topics worldwide due toenergy sources. Security is a top priority, and the country andsoaring energy prices, the securing of resources, andhas established future strategies from a variety of sources.

environmental conservation. Under these difficult circumstances,

Starting in 2006 and scheduled to conclude in 2014, a national

the three countries of Japan, China, and South Korea gathered

IGCC project is under way that uses a 300 MW model plant tofor this information exchange forum to discuss such issues andseek a 42% rise in gas turbine efficiency.

future outlooks.

Japan’s representative, Mr. Kurosawa from the Institute of

To begin, Mr. Wen of China introduced recent topics

Applied Energy, was the last speaker in this forum. He statedon the country’s energy status. Because coal is a major source ofthat 30% of the electrical generation capacity of Tohoku Electricenergy in China, IGCC research and development in this sector

Power and Tokyo Electric Power Company (Tepco) was lost due

is robust. In addition, CCS research and development is also

to the Great East Japan Earthquake and subsequent tsunami;

vigorous due to the need for environmental support. Similarly,

however, Japan was able to handle the summer season with noMr. Lin of China speculated on the impact of man-made heat

serious issues. In addition, he mentioned the country’s intent torelease on regional warming, citing the rapidly rising trends ofdecommission a number of older nuclear power generating

CO2 increases as well as rising temperatures in cities of China

stations in the future. Mr. Kurosawa also stated that Cool Earth10

21 is currently being maintained with the goal of a 50%

for the introduction of new sources of energy such as offshore

reduction in CO2 emissions by 2050. To achieve this goal, cleanwind, solar cells, and biomass.

coal and safe large-scale nuclear power technologies are underconsideration. In addition, Japan is currently promoting plans

Photo 3.5 Forum 2

by Toshinori Watanabe (The University of Tokyo),Experiments and CFD Concerning Unsteady Flow Fields of

Yoshinobu Tsujimoto (Osaka University), Makoto Yamamoto

High Flow Windmill Operations; No. 056, Impact of Wing Tip(Tokyo University of Science), Toshihiko Nakada (Tohoku

Vortex Collapse Occurring in the Vicinity of Stall Point on Wide

University), Kuniyuki Imanari (IHI) and Atsushi Makino (JAXA)

Wing Tip Gap; No. 106, Influence and Profile Drag Reductionof Flow Field Due to Libretto on the Blade Surface; No. 220,
Experiments and CFD on the Secondary Flow Loss Caused by

4. Technical Sessions
4.1 Aerodynamics

Interference with the Mainstream Flow and Leakage from theOf the 37 papers presented in the field of aerodynamics, 9, held

Seal Portion of the Stationary Blade; and No. 108, Verificationin 3 sessions, concerned axial flow compressors; 4 papers in 2

Usingsessions related to centrifugal compressors; 15 papers in 5

Temperature/Absolute

sessions related to turbines; 6 papers in 2 sessions related to

Measurements. The four papers presented in the centrifugal

CFD; and 3 papers in 1 session concerned aerodynamic design.

compressor field included No. 035, Surges in Two-Stage

The axial flow compressor field attracted a large audience, andCompressors, Their Detection and Characteristics; No. 040, The

papers presented on design optimization and design method

Difference in Distance between the Diffuser and the Impeller

proposals induced a lively debate. These papers included No.

and Its Impact on Performance and Noise; No.165, Design064, 11th Stage Compressor Optimization and OGV Design

Optimization of the Low Solidity Diffuser Using GA; and No.

Methods Using CFD; No. 055, Proposal for Optimal Wing

174, Proposal for Design Optimization Methodologies for

Design Methodology Oriented to Reduce Losses in the

Vortex Chambers Using CFD. Unfortunately, the centrifugal

Transonic Stage; No. 136, Development of High Loadcompressor sessions had relatively weak attendance, and theCompressors Aimed at Reducing the Number of Stages; and No.

subsequent question-and-answer sessions were anemic likely

046,

because this session was offered in smaller rooms on the final

Mixed

Span

Direction

Predictions

inTransonic

Compressors. In addition, presentations on improving the

CFD

and

Development
PressureofanAbsolute

Probe

for

Entropy

Thursday of the conference.

understanding and performance of unsteady flow structures

In the fields related to turbines, most of the

between blades included the following papers: No. 030,

presentations concerned axial flow turbines. Only two radial11

turbine-themed papers were presented: No. 162, Optimization of

Lattice Formation and Calculation Schemes, which evoked a

Small Radial Turbine Inlet Flow; and No. 007, Proposals forlively discussion with many questions asked from the large

Basic Design and Development. In these presentations, theaudience in attendance.

radial turbine was considered only as an application example.

Threepresentations

were

made

regarding

The axial flow turbine presentations mainly concerned unsteady

aerodynamic design: No. 135, Proposal for the Basic Design offlow structures between blades and included the following

a Wide-Chord Blade Row; No. 201, Experiments and CFD of apapers: No. 020, Analysis of Combustion Gas in the Passage

Tesla Compressor Diffuser Design; and No. 127, Effects of

between Blades; No. 194, Interface Problems with Measurement

Forward and Rearward Wing Sweep on Transonic Fan

Probes; No. 113, Secondary Flow Losses and Detailed Internal

Performance.

Flow

Measurements

for

Its

Optimization;

No.

117,

In this conference, a change was made forExperimental Study on the Impact of Unsteady Flow Structures

presentations in the field of aerodynamic design in that stabilityof Stationary Blades Brought on by Wing Tip Vortex Leakage;enhancement and turbocharger technology were combined.

and No. 248, CFD Analysis of Moving/Stationary Blade

Hence, fewer papers were presented than those offered inInterference on the Supersonic Turbine Blade Row. The

previous conferences.

following papers were also presented: No. 063, The
Relationship between Performance and Secondary Flow Lossby Yutaka Ohta (Waseda University), Takanori Shibata (Hitachi)

Resulting from Changes in Blade Loading; No. 076, Reduction

and Eisaku Ito (Mitsubishi Heavy Industries)

of Secondary Flow and Performance Improvements Due to WallContouring and Non-Axisymmetric End Walls; No. 175,

4.2 Heat Transfer

Circumferential CFD Analysis of Non-Uniform Inlet Flow

In the field of heat transfer, 34 papers and 1 keynote lecture

Influence; No. 215, Thermal and Aerodynamic Wing Design

were presented in 13 sessions, which was a significant increase

Methodology in the Development of the 1700 °C Class Gas

over the number of sessions in previous conferences. Of these,

Turbine; and No. 152, Interference with the Film Cooling

12 papers in 5 sessions concerned Heat Transfer on Film

Airflow and Secondary Flow Between Blades. In addition, three

Cooling I-V; 5 papers in 2 sessions concerned Heat Transfer

specialty

125,

with Impinging Jet I, II; 5 papers in 2 sessions were presented

Development of CFD Methodologies Using Mixed Gas Models

on Numerical Simulation of Heat Transfer I, II; 6 papers in 2

and Examples of Their Applications to Axial Flow Turbines;

sessions concerned Internal Cooling I, II; 3 papers in 1 session

and Nos. 254 and 255, The Influence of Unsteady Mainstreams

concerned Conjugate Heat Transfer; and 2 papers in 1 sessionof Laminar Boundary Layer Transition Mechanisms.

were presented on Heat Transfer Measurement.

paperswere

presented,

includingNo.

The following papers were presented concerning

The number of principal authors presenting from

CFD: No. 114, Analysis of Labyrinth Seal Leakage Flow; No.

each country were Japan, 15; China, 6; Thailand, 2; Europe, 5;205, Analysis of Mixed-Flow Compressor Windmill Operation

United States, 5; and South Korea, 1. (The number of presenters

When Turbo Engine Precooling Is Used; No. 239, Analysis offrom South Korea was affected by earthquake complications.)

the Variable Turbine Nozzle Section of Vehicle Turbochargers;

The large number of international presenters and the versatileand No. 241, Analysis of Ice Accretion under Moving/Stationary

and high-level variety of research activities combined to create a

Blade Interference in Aircraft Engines. In addition, Professor

successful international conference.

W.N. Dawes of Cambridge University presented No. 072,

The following is a brief list of noteworthy items

Examples Introducing the Proposal for a Faster Method of

included in the presentations: In the heat transfer on film

12

cooling session, Professor Ligrani presented his keynote lecture

Performance in High-Temperature Wind Tunnels Using a Test

titled “A Case Study on the Aerodynamic Loss Due to Film

Model Subjected to Three Types of Surface Roughening on

Cooling.” In addition, the following papers were presented: No.

Opposing Jet Flow Surfaces, As Well As the Effect of the Jet

138, The Effect of Bubbles and the Resulting Changes in the

Flow Passage Configuration, Determining the Most Effective to

Incidence of Film Cooling Characteristics on Positive Pressure

Be a Roughened Concave Surface.

Wing Surface Using Cascade Test Equipment and PSP

The internal cooling sessions consisted of Nos. 216

Technology; No. 148, Cooling Efficiency Determined by

and 226, A Detailed Investigation of a Projection on the FlowExperiments Using Temperature Sensitive Paint (TSP) Film on

Path; No. 007, Its Optimization; Nos. 103 and 149, Research on

Four

a

Flow Paths Outfitted with Comparatively New Types of Heat

Transpiration Type; No. 057, LDV Measurements Used toTransfer Enhancement Mechanisms, Such As Dimples; and No.

Examine Detailed Structure and Flow Measurements of the203, Investigations of the Effective Pin Fin Tilt Angle.

Different

Film

Hole

Configurations

Including

Cooling Efficiency of Film Cooling Panels With Multi-Rows of

The numerical simulation of heat transfer andHoles, and a detailed report on the Relationship between the

conjugate heat transfer section consisted of the following

Cooling Efficiency and Vortex Structure of Film Airflow; No.

presentations: Predictions Made by Conjugate Analysis of the227, The Influence of Film Cooling from the End Wall Given by

Following; No. 086, Temperature Distribution of Leading Wing

Horseshoe Vortices Formed at the Wing Leading Edge Using

Edge with Film Cooling; No. 164, Temperature Distribution of

PIV/LIF Methodology; No. 122, LES Analysis Considering

the Cooling Blade Used in the Stream Cooling System; No. 204,

Upstream Fluctuation Components Using Random Flow

Blade Surface Temperature Distribution in Boundary Layer

Generation Methodology on Thermal-Fluid Characteristics ofTransition; No. 198, RANS Analysis Predictions Using

Cooling Air from the Cooling Holes Situated on the Upstream

Experimental Heat Transfer Coefficient Distribution Data of aSide of the End Wall Turbine Blade Row; and No. 234, LES

Blade Surface with Film Cooling, Which Showed, As a

Analysis of Unsteady Flow of Cooling Air from the Cooling

Turbulence Model, the SST Model with the Transition Model

Holes Using Open FOAM; No. 085, a presentation regarding

Has Comparatively Better Results; and Nos. 016 and 060,

Double Jet Film Cooling and a promising configuration ofIntroduced Examples of Conducting DES and LES Analyses of

RANS Analysis of Thermal Fluid Properties of NEKOMIMI

Complex Flow Fields.

Geometry in the Cooling Hole Exit; No. 058, A Detailed
InvestigationofTemperature

Sensitive

LiquidMoreover, presentations were offered on Annular

CrystalCascade Test Results on HP Cooled Turbine Blade Materials

Methodology and Unsteady RANS Analysis of the Effect Given

Produced in CMC, in addition to The Durability of Trip andto Mainstream Turbulence and Cooling Air in the Mixing

Adequacy of Cooling Performance.

Process, and the Efficiency of Film Cooling on the Blade
Surface in a Turbulent Mainstream; and No. 195, An Evaluation

4.3 Combustionof Transient Response Methodology Using an IR Camera to

4.3.1 Outline

Study the Film Cooling Distribution and Heat Transfer

General combustion-related lectures included the following: CB

Efficiency of a Cooling Side (Cutback) Dimpled Model on the(1) (fuel), three presentations; CB (2) (combustion emissions I ),Cooling Air Outlet in the Trailing Wing Edge.

three presentations; CB (3) (combustion emissions II ), two

In the impinging jet cooling sessions, two papers

presentations; CB (4) (combustion phenomenon I), twowere presented: No. 257, Investigations into the Heat Transfer

presentations; CB (5) (combustion phenomenon II), three

Characteristics in a Gyrating Jet Flow; and No. 003, Coolingpresentations; CB (6) (combustor development I), three13

presentations; CB (7) (combustor development II), three

metal at or below 1800 K to suppress the generation of thermalpresentations; CB (8) (atomization of fuel and ignition), threeNOx. For verification, numerical analysis was reported on thepresentations; CB (9) (numerical analysis of combustion I),

results of one-dimensional flame propagation undergoing

three presentations; CB (10) (numerical analysis of combustion

detailed elementary reactions. In No. 232, with respect to ECOII), three presentations. Of these 28 presentations, 21 wereengines, experimental results on a low-NOx combustor using adomestic, and seven were foreign. Although we were concerned

new jet swirler to achieve rapid mixing of fuel and air werethat complications from the Great East Japan Earthquake would

reported.

result in fewer lectures, the number in this series was only one

In session CB (3) (combustion emissions II), twofewer than the 29 lectures offered at the last conference in 2007.

presentations related to emission were given. No. 101 reported

It would appear that interest remains high in environmental

the combustion characteristics of methylated ester biodiesel oil

issues associated with combustion and fuel diversification.

synthesized from waste cooking oil for aircraft and industrial
gas turbines, and No. 84 reported on Large-Eddy Simulation

4.3.2 Fuel

(LES) using the two-scalar flamelet approach targeting

In session CB (1) (fuel), three presentations were made relative

industrial gas turbines that use lean premixed combustion of theto biofuel. No. 013, together with a comparison of fuel

18 MW class.

properties of liquid fuel synthesized from natural gas or biomass
with that of jet fuel, reported its impact on transport efficiency

4.3.4 Combustion Phenomena

and range when used in large-, medium-, and small-sized

In session CB (4) (combustion phenomena I), two presentations

aircraft. No. 092 reported the burning characteristics of bio-gas

related to combustion phenomena were given. No. 059 reported

generated by microbial fermentation as fuel for a small gas

the combustion characteristics of fuel spray droplets for theturbine. No. 171 reported the burning characteristics of a gas

rich-fuel combustion area of a double-swirling, prefilming-typeturbine when methyl ester synthesized from cooking waste oil

fuel injection nozzle with a 1/2 scale RQL combustor using thewas used as gas turbine fuel. Commonly questioned was theresults of simultaneous measurements of fuel droplet velocity

price of biofuel compared with that of traditional fuels; however,and particle size measured by a phase Doppler anemometerit was believed that this issue was politically motivated.

(PDA). In No. 129, the alternate appearances of fuel spray andcombustion areas was reported for the instantaneous structure of

4.3.3 Combustion Emissions

a spray flame using a laboratory-scale spray combustion burner

In session CB (2) (combustion emissions I), three presentations

that considered detailed, two-dimensional plane measurement

were made relative to combustion emissions. No. 38, using a

results of the fuel spray and fuel area during boththoroughly stirred reactor combustion model and a combustion

noncombustion and combustion.

model that consolidates completely and partially stirred reactors,

In session CB (5) (combustion phenomena II), threereported estimates of NOx and CO emissions of a 250 MW

presentations related to combustion phenomena were given. No.

single-single shaft industrial gas turbine combustor when using

209 reported the phenomenon of flashback during leandifferent compositions of natural or synthetic gas as a fuel.

premixed combustion using a detailed velocity field of the flame

No. 142 reported experimental results of the

propagation surface obtained through high-speed time-series

formation mechanism of prompt NOx during lean premixed

PIV measurement. No. 235 reported the suppression of

combustion that used heat loss of the burner to keep the

combustion oscillation of a micro gas turbine combustor under

combustion temperature of the planar flame forming on sinteredhigh pressure. No. 224 reported PIV measurement of the14

velocity field of a gas turbine combustor model during

4.3.7 Numerical Analysis of Combustion

non-combustion.

In session CB (9) (numerical analysis of combustion I), threepresentations concerning numerical analysis of combustion were

4.3.5 Combustor Development

given. No. 27 reported numerical analysis of aircraft engines

In session CB (6) (combustor development I), three combustor

using

development-related presentations were given. No. 068 reported

formulation. No. 066 reported on LES for the rich-fuelthat a significant reduction of NOx emissions was possible for

combustion area of a double-swirling, prefilming-type fuelsmall aircraft engines. For the CAEP/4 NOx Standard, tests

injection nozzle with a 1/2 scale RQL combustor, which was

were conducted on five fuel-injection nozzles designed on thepreviously presented in No. 059. In No. 071, a visualizationbasis of the lean staged combustion concept. No. 179 reported

experiment of the atomization process though air flow of theon a 1500 °C-class industrial gas turbine that uses steam to cool

liquid film and detailed numerical analysis by using thethe turbine blade. #182 reported on a dry low emission (DLE)interface tracking method were reported.

thegas turbine combustor with very low concentrations of NOx andIn

CO emissions.

Reynolds-averaged

sessionCB

Navier–Stokes(10)(numerical(RANS)

analysisofcombustion II), three presentations related to combustion

In session CB (6) (combustor development II), threesimulation were given. No. 256 reported the usefulness ofpresentations on combustor development were given. No. 217

detailed elementary reaction analysis using equivalent reactor

reported research results using PIV and LES for combustors of

networks (ERN). No. 187 reported experimental results for aindustrial gas turbines with 1700 °C-class inlet temperature

two-stage combustor consisting of main and pilot that used PIV

using exhaust gas recirculation (EGR), which is currently being

measurement, Mie scattering measurement, and computational

promoted as a national project. No. 236 reported experimental

fluid dynamics (CFD) analysis. No. 043 reported LES results

results for a low NOx combustor for aircraft gas turbines thatfor spray combustion formed in a high-pressure field using theuses OH radicals chemiluminescence, Mie scattering from fuelflamelet model that applied the so-called new philosophy ofspray using a laser sheet, and PIV. In No. 184, experimental

determining the position of a lifted flame by solving theresults were reported on lean premixed, prevaporized (LPP)

G-equation.

combustors for ECO engines.
4.3.8 Miscellaneous Impressions
4.3.6 Atomization and Ignition

In this combustion-related general presentation, the application

In session CB (8) (atomization and ignition), three presentationsof complex optical measurement techniques for spray

concerning atomization and ignition were given. No. 081

combustion fields, detailed numerical analysis by the interface

reported on visualization experiments and numerical analysis

tracking

through interface-tracking methods concerning the liquid jet of a

atomization process of liquid fuel fulfilled both quantity andcoaxial-type fuel injection nozzle. No. 145 reported the results

quality; however, It was determined that a more activeof experiments concerning laser ignition of lean premixed gas

question-and-answer discussion session was necessary.

bylaser-induced

breakdown

using

a

methodconcerning

LES

of

combustionandpicosecond-orderultra-short pulse laser. No. 223 reported on the ignition of fuelby Fumiteru Akamatsu (Osaka University)

spray using a nanosecond-order short pulse laser.
4.4

Noise, Vibration, and Structure.

Ten papers and one keynote lecture were presented on structural

15

vibration. The keynote lecture was given by Professor Zoltan

Finally, a Japanese university introduced a design tool related to

Spakovszky, head of MIT’s gas turbine laboratory. Titled “Newfoil-bearing performance, thermal deformation, and stability.

Directions in Turbomachinery Aero-Acoustics,” the lectureThis meeting, concerning structural vibration,

provided a simple explanation of Dr. Spakovszky’s current

consisted of four sessions. Because of its diverse subject matter,

research and was composed of the following three sections: 1) a

which included structure, vibration, noise, and bearings, session

method for evaluating the shielding effect of noise generated byparticipation was limited. However, the smooth management by

new types of aircraft; 2) a method for evaluating fan rotor noise

the session chair, allowed questions to be drawn successfully

in an inlet at supersonic speeds; and 3) a noise design method

fromfor new low-noise, double inversion-type propeller fans. It wasquestion-and-answer session.

theparticipants,

resultinginasuccessful

concluded that the problem of aerodynamic noise associatedwith new propulsion systems and new types of aircraft requires

by Shigehiko Kaneko (The University of Tokyo)

alternative solutions to maintain aerodynamic performance.
Lecture No. 047 was a presentation from Japanese companies

4.5 Performance

related to noise evaluation in co-generation systems (CGS). No.

In the field of performance, a variety of gas turbines including

207, from Japanese research institutions, concerned a device toaero engines, aeroderivative gas turbines, micro-turbines, andreduce jet noise that was recently evaluated by the Japancombined-cycle gas turbines were chosen as topics, and nine

Aerospace Exploration Agency (JAXA). No. 065, from apresentations throughout three sessions were given.

Japanese university, was based on a theoretical study for

Presentation No. 010 concerned secondary air

improving the characteristics of blade vibration due todesign techniques in aero engines. With respect to unmanned

mistuning. The influence of this parameter on vibration

aerial vehicle (UAV) turbo-prop engines, numerical analysis

reduction effectiveness was evaluated through the Monte Carlofocusing on engine intake flow, exhaust flow, and pressure loss

method. No. 079, from a Japanese university, detailed

was calculated to conduct high-altitude performance analysis intheoretical and experimental research related to the reduction ofa test vessel (No. 087), and artificial intelligence methods for

aerodynamic noise generated by supersonic-speed jet engines.

fault diagnosis were considered (No. 107).

No. 186, from an American university, was based on theoretical

No. 259 presented installation examples of various

research concerning blade vibration due to mistuning and theflexible systems for aero-derivative gas turbines that can becharacteristics of applying an original technique known as theused as backup power sources to renewable energy installations.

modified modal domain approach（MMDA). No. 218, from a

For centrifugal compressors of micro-gas turbines, a newJapanese research university, analyzed a numerical calculation

technique using a one-dimensional model was proposed, inof three-dimensional, irregular aerodynamic forces acting on

addition to the examination of a performance benchmark in thewing vibration. No. 034, from Japanese companies, announced

same study. In addition, No. 0170 proposed a method of

the proposal of a flutter analysis tool based on the harmonic

estimating the simple thrust loads of radial turbines equippedbalance technique and included verification of its effectiveness.

with permanent magnet generators,

No. 093, from Korean companies, was based on a study that

For power generation in large gas turbines,

clarified countermeasures against the phenomenon whereby asafeguards against turbine blade overheating and its effect in thecentrifugal compressor impellor blade comes into contact withcase of gas fuel produced through gasification were studied in

the casing. No. 246 was an announcement from JapaneseF-class gas turbines (No. 020). No. 231 presented performancecompanies concerned with a new method of stacking fan blades.

estimates for oxygen combustion in the case of existing16

semi-closed combined-cycle gas turbines, and No. 190

streamline curvature method to result in a 3.1% performance

presented a state diagnosis of combined-cycle gas turbines

improvement for a 300 MW low-pressure turbine machine. No.

through remote monitoring center data.

173 presented the development of a new high-performancelabyrinth seal that reduces stream leakage through a vortex

by Norihiko Norihiko (AIST)

generated by a step set inside the seal; through experimentation
and analysis, an approximately 30% reduction in leakage

4.6 Steam Turbinesvolume flow was reported. No. 146 presented an analyticalAt the newly established IGTC’11 steam turbine session, 15

investigation on the effects on turbine performance of thepapers including two keynote lectures were presented in six

machining accuracy of turbine blade surfaces.

sessions(GS 2, OS 4). Four presentations were made in

In the organized session titled “Long Bladeorganized general sessions under the topic of Efficiency

Technology of Steam Turbine,” paper Nos.168, 211, and 249

Enhancement of Steam Turbines. Paper No. 002, based on new

were presented on the recent development of final-stage long

performance enhancement technologies that focus on unsteadyblades in the 1.2–1.3 m class (3600 rpm) by three domestic

phenomena, presented the results of a model turbine test to

steam turbine companies: Hitachi, Mitsubishi Heavy Industries,

control the mixture phenomenon of the mainstream and theand Toshiba. In general, a supersonic airfoil design is necessary

cavity flow that undergoes periodic variations from upstream

for the inlet of moving blades in this long blade class andstationary and downstream moving blades. By varying the axial

centrifugal stresses approach the limits of conventional material

and radial distances of the cavity-like shape of the peripheral

strength, each company employed confident design to ensureedge between stator and moving blades, a stage performancereliability and performance repeating analysis and model turbineenhancement of a maximum of 1.7% can be achieved. This

experiments including actual blade tests. This topic has attracted

presentation received significant attention for its substantial

the attention of a large global audience.

effects on performance enhancement.
.

Relating to the wet steam flows through steam

The keynote lecture, “Fluid Dynamic Efficiency

turbineblades,No.

104

presented

developmentof aOptimization of Steam Turbine Stages Considering Leakage

non-equilibrium wet steam flow RANS two-dimensional

Influences and Inter-Stage Reciprocal Interferences,” made byunsteady condensation analytical method using the quadrature

Professor Yuan, Tsinghua University, and concerned typicalmethod of moments (QMOM), which properly considers thetwo-stage high pressure turbines. The lecture presented ansize distribution of condensed water droplets. Regarding the

optimal design method to attempt performance enhancement

prediction of unsteady flow forces of steam turbine blades, No.

using CFD including steam leakage of the inner diameter side of053 considered the influence of the axial distance between stator

the stationary blade and the blade-tip seal fins to automaticallyblades and rotating blades on the unsteady fluid forces on thechange the shape of the three-dimensional design of first-stage

rotating blades separating the unsteady flow force applied to themoving blades in the optimal design system. Because suchmoving blades due to the potential interference effect of thechanges affect the down-stream stage, the two-stage efficiency

stationary and moving blades and the unsteady flow force

was employed as the objective function. Many engineers andapplied to the moving blades due to the interference effect of theresearches who study the related issues attended this session,

stator blade wakes and moving blades. This paper presented awhich allowed for detailed, extended questions and discussions.

study of two-dimensional analysis of the unsteady compressible

No. 155 presented an optimal design method for low-pressure

RANS and analysis of two-dimensional unsteadyturbine cascades that includes a quasi-three-dimensional

flow with an approximately zero-thickness trailing edge using

17

non-viscouscusps attached to the trailing edges of the stator blades at thesteam hotter than 700 °C, even when employing 12 Cr steel in asame time to separate the potential and wake unsteadymedium-pressure rotor. No. 176 introduced the development ofinteractions.

a new material in which the temperature change is regulated for

A large global audience gathered for the presentation

the phase-precipitation hardening that dominates the creepof the keynote lecture titled “Recent Technologies forstrength of the Ni-based alloy, which satisfies the reciprocal

Concentrated Solar Power Systems and Steam Turbines” by Mr.

relationship of forge ability and high temperature–high-strength

Okita from Toshiba Corporation. This seemed to show that theand can be expected for application to the 800 °C Class. These

technology trends in this field garnered significant attention.

papers presented advanced, original technologies in the

Regarding solar thermal energy power generation systems, ordevelopment of A-USC specific to Japan. No. 188 presented

concentrated solar power systems (CSP), in which steam

from Europe where the development of Advanced USC

turbines generating electricity are driven by steam generated bytechnologies had been launched first introduced the reason why

the exchange of heat gathered with a reflector that heats a

the Alloy 625 was recommended for casting material and theirmolten salt medium or oil, constructions have been performed in

manufacturing examples. In addition, the presentation on

regions such as North Africa, the Middle East, Southern Europe,

production verifications of l welding mockups from several

and North America, where solar thermal energy steam turbines

casting material left the impression that 700 °C-class steamof a 50 MW or more per-unit capacity are currently running.

turbine casings and high temperature valve boxes are becoming

The future prospects of CSP and characteristics required forto be ready for their practical applications.

solar steam turbines were introduced in detail, and we believethat along with geothermal turbines, the use of renewableby Tadashi Tanuma (Teikyo University) and Eiji Saito (Hitachi)energy for steam turbines has the potential for future importantresearch and development topics.

4.7 Materials

Four papers were presented in the ultra-supercritical

The materials sessions offered the newly-established topic ofpressure steam turbine session, three of which centered on thesteam turbine materials.

development of materials and design development of the

Although submissions related to the development

700 °C-class Advanced Ultra-Super Critical steam conditionand evaluation of advanced ultra-supercritical steam turbine(A-USC) through a Japanese national project. The remaining

project material development and evaluation were invited, these

paper was a report concerning developments in Europe of

related submissions were summarized as project reports fromapplications of welding and casting materials such those forthe topic of steam turbines, also newly established.

turbine casings. Paper No. 169 from Japan presented theTherefore, as usual, the program consisted of gas

development of Ni-based alloy for steam turbine rotors withturbinesimilar linear expansion coefficient to 12Cr steel and the“Maintenance/Lifetime

mock-up of dissimilar metal welding with the developed

Materials/Repair Technology,” and “Coating Technology.”

Ni-based alloy and the conventional 12Cr steel, while the

However,conventional Ni-based alloys have a limitation for large scale“Maintenance/Lifetime

rotor forgings. No. 210 introduced an example of a turbine“Damage/Lifetime Valuation” and “Crack Progression” sessions

structural

relatively

to be divided into five sessions, with the first part of

low-temperature steam of high-pressure turbine exhaust in thepresentations related to “Maintenance/Lifetime” made on thehigh-temperature section of a medium-pressure rotor, can use

first day and lectures concerning the development of materials

designthat, bycooling with the18

componentsaclassified

into

Evaluation,”numerousof“Advanced

submissions

Evaluation”

topicsforrequiredtheentirepresented on the second day. These 13 presentations weremachine case studies. Finally, No. 253, concerning a thermal

attended by approximately 30 participants on the first day andbarrier coating material attracting recent attention, reported theapproximately 50 on the second day, resulting in standing-room

research results of research on La2Zr2¬¬O7, SrZrO3, andonly and demonstrating the high level of interest in materials

LaLiAl11O18.5 ,which are systems of pyrochlore, perovskite,

technology.

and aluminates respectively; new segment structures; and new
The“Maintenance/Lifetime

Evaluation”

processes of suspension plasma thermal spraying and extreme

presentation was composed of three papers, Nos. 199, 185, andlow-temperature plasma thermal spraying.

075, a series of reports on research results on the analysis ofactual machine phenomena related to gas turbine disk damage,

By Yomei Yoshioka (Toshiba)clarification of phenomena based on reproducible laboratory
experiments, and the effectiveness of shot peening constructed

4.8 Turbochargers

as a measure, respectively. No. 069 presented evaluation andNine presentations, including the keynote lecture, were done inanalysis results for solving the problem of fretting fatigue in thethe turbocharger session, offered for the first time in IGTC’11.

fixings of the moving blade section of a gas turbine. Nos. 042

Five papers came from overseas. The session began with theand 031 introduced examples of gas turbine first-stage moving

keynote lecture by Dr. Ricard Martines–Botas of Imperial

blade damage and reported on material degradation and related

College, U.K, titled “Boosting and Turbocharger Needs fordamage analysis results, respectively. No. 061 reported

Highly Downsized Low Carbon Vehicles.” This lecture

fundamental evaluation results of the dependency of Ni-based

concerned the potential improvement in fuel consumption ofalloy fatigue crack propagation behavior on crystal orientation,passenger-car engines through the introduction of high-boost

targeting the static/moving blade damage that has become

systems, in addition to the effect of turbine characteristics under

problematic in actual machines.

flow pulsation on turbochargers and engine matching. An

Concerning“Advanced

Materials/Repair

attempt to to improve fuel consumption by significantly

Technology,” No. 181 reported the development and evaluation

reducing loss through heat and friction through downsizingof the recent trend of constraining the volume of Re added to anengines by high boost pressure generated by turbochargers andalloy, relative to an Ni-based single-crystal alloy, which has

to improve the response of the turbocharger at the low engine

become indispensable in changing gas turbines to highspeeds by an electric compressor are done. In addition to above

temperatures. No. 008 presented the development concept andattempts, the “Hyboost project” incorporates a system for

performance evaluation results of a burner-rig test machine

energy recovery through a power turbine into a gasoline engine.

developed as a corrosion-resistance evaluation technique in“Hyboost project” demonstrates the possibility of improving

alloy production. No. 074 reported the development of repair

further fuel consumption of internal combustion engines.

materials attached to a stationary blade diffusion row andGeneral issues and guidelines for the design of turbines withevaluated the results of actual applications.

efficient energy recovery of the engine exhaust gases were also

In the “Coating” session, No. 118 evaluated damage

presented.

to thermal barrier coatings, which is an interface strength

The following includes a summary of the eightassessment technique that applies the indentation method, heatgeneral presentations.

cycle testing, and actual damage to machine materials, in

No.

026,

a

paper

relatedtoturbocharger

addition to the development of coating materials. No. 180

development for an IMO-2 four-stroke marine engine, focused

examined low thermal conductivity thermal barriers and actualon the aerodynamic design of a turbine and a compressor. The

19

compressor employed a recirculating-flow-type casing treatment

stress is an indispensable technique in ensuring turbocharger

with counter swirl vanes at the aim of expanding the operating

reliability. No.109 presented a model for predicting the increase

range. The turbine achieved a high efficiency by optimizing theof vibrational stress through mistuning, and No. 112 examined

angle and the thickness of the impellor blade.

by CFD analysis the relationship among structure, flow field,

Three papers related to compressors were presented.

and aerodynamic performance of variable nozzles. A cylindricalTwo dealt with unstable phenomena and one dealt withspacer was placed in the upstream of the nozzle to preserve

performance. No. 121, related to unstable phenomena,

nozzle clearance. There were button-shaped cylindrical shaft

investigated the difference between the surge characteristics

seals, which connected the nozzle rotation axis to the nozzle

caused by a certain volume of plenum chamber downstream ofvane at both ends of the nozzle vane. The impacts of each of

the compressor and the same piping volume, defined by thethesevolume from the compressor outlet to the discharge valve, as theperformance were described in detail.

elementsandnozzleclearanceon

aerodynamic

volume of the plenum chamber. No. 080 presented a result of

The theme of the remaining two papers related to theunsteady CFD analysis to show the different performance/surge

keynote lecture. No. 052 presented the development process ofcharacteristics of two compressors. For a compressor impeller

low-pressure-ratio power turbines for turbo-compound engines.

with better surge characteristics without the existence of a stall

Turbine impellers targeted at 1 KW power generation turbine

cell, the entire circumferential shroud section in the inducer waswith an expansion ratio of 1.1 have a unique shape of (turbine

covered with the stable separation. The compressor impeller

impellor exit area)/(turbine impellor inlet area) = 0.35. It waswith worse surge characteristics showed that a localized

reported that the radial turbine demonstrated significantly higher

separation propagated in the direction of the circumference as aefficiency than conventional turbines with expansion ratio ofrotating stall. In No. 088, the effect of two types of vane shape,

between 1.05 and 1.3. No. 158 described the prediction ofstraight vane and curved vane set inside a cavity of aturbine performance under pulsating inlet flow. Unsteadyrecirculation-flow-typetheturbine performance was estimated through a mean-line model

performance/surge characteristic and impeller flow field wasand one dimensional CFD. Although prediction accuracy forinvestigated through CFD calculation. Particularly for theflow volume fluctuation was slightly lower, other obtained

curved vane, it was shown that the suppression of the positive

parameters were in good agreement. In addition, practical levelpre-swirl of the recirculating flow at the impeller inlet results inpredictions of average turbine performance were reported fora decrease in surge flow rate and an increase in pressure ratio.

one fluctuation per cycle.

casingtreatment,onRelative to compressor performance, No. 233 examined theeffect of clearance on compressor performance to obtain

by Hideaki Tamaki (IHI)

fundamental data used in a centrifugal compressor for an MGT.

and Seiichi Ibaraki (Mitsubishi Heavy Industries)

Numerical calculation was implemented for four types ofclearance and a case of non-clearance.

4.9 Development and Operation

Next, four papers were related to radial turbines, two

A total of eight papers were presented in three sessions in theof which presented as variable nozzles as the subject. Radial

field of Development and Operation: DO (1), DO (2), and DO

turbines used in turbochargers are operated at a variety of(3). In session DO (1), which concerned the retrofitting ofrotational speeds depending on engine operating conditions.

thermal plants, No. 005 reported changes and aging ofHence it is difficult to completely avoid impeller blade

combined cycle steam power units. In this paper, a scheme wasresonance caused by nozzle wake, and understanding vibrationalpresented to reduce costs and shorten the construction period by20

taking full advantage of existing facilities and to improve4.10 Systems and Control

environmental performance and thermal efficiency by updating

In the session on systems and control, the number of papers

equipment.

presented was twice that of the previous event; therefore, the six
In DO (2), three papers were presented relative topapers were divided into two sessions. Nos. 041, 200, 208, andMW-class gas turbine development. No. 51 announced the240 concerned research on reduction of fuel consumption anddevelopment of Kawasaki Heavy Industries Ltd. M1A-17,

lowering of NOx emissions, suggesting that the increased

which, through the application of CFD, demonstrated a 2.5 pointinterest in technology development meets the needs of society.

improvement in thermal efficiency and a 200 kW improvement

In addition, research on the control infrastructure of active

in output while clearing 15 ppm of NOx over the M1A-13 with

control stabilization and system identification, Nos. 159 and 251,

the same dimensions. From the MAN Company, element

respectively, is also relevant.

examination and unsteady CFD results on the 6 MW gas turbine

No. 041, which concerned aircraft engine fuelcurrently in development were presented in No. . No. 94, frompumps, was based on a case study conducted on fuelDoosan Heavy Industry and Construction, presented a summary

consumption improvement that introduced an electric fuelof performance test results and activation schedule optimization

system driven by an electric motor from a conventional

for the DGT-5 5 MW class gas turbine generator, which wasaccessory gear box (AGB). In this process, the heat balance candeveloped jointly with The Ukraine.

be improved by removing the air cooled oil cooler (ACOC). No.

Three papers were presented in DO (3). In a

200 introduced simulation results of controlling power loadpresentation on the flow of lubricating oil in the accessory

variations of the gas turbine and nuclear reactor cogeneration

gearbox,visualization

system aimed at developing countries. No. 208 concerned a gas

experiments and CFD simulation of the flow guide effect, which

turbine using catalytic combustion. This paper explained thewere in good agreement. No. 189 presented the Mitsubishi

concept of maintaining combustion performance against

Heavy Industries 1600 °C-class gas turbine. Improvements indeterioration of the catalyst whereby the main fuel is switched

thermal barrier coating (TBC) and cooling technologies tobetween activation and rotational acceleration control by fuzzyachieve the 1600 degree Centigrade TIT prevented damage tologic, and the precombustion fuel can be adjusted according to

the high-temperature parts, which was validated throughthe temperature difference between the front and the rear of thehundreds of hours of operating tests. In a presentation on

catalyst. In No. 240, for twin spool turbofan and single spool

1700 °C-class gas turbines (No. 197), simulation results on theturbojet engine, minimization control of SFC in a test engine

DLE combustor for exhaust gas recirculation system were

was implemented by estimating thrust and SFC using a

introduced as a technology for achieving both high temperature–

constant-gain Kalman filter and by manipulating fuel andhigh efficiency and low NOx, along with a variety of researchvariable mechanisms.

No.

214

introduced

resultsofresults on blade cooling technology, coating technology, andNo. 159 was a presentation on active stabilization

aerodynamic design. Numerous participants attended bothcontrol. By detecting compressor instability using the standard

sessions. In particular, DO (2) and DO (3) were standing-room

deviation of the shift in pressure rate change of the compressor

only.

wall, a method of adjusting the fuel start-up schedule using the
exponentially-weighted moving average of the pressure rate
by Eiichi Koda (CRIEPI)change in the wall was confirmed in simulation. No. 251

and Kazuhiko Tanimura (Kawasaki Heavy Industries)

concerned a twin spool turbofan engine, whereby system
identification of engine response was introduced for fuel and21

variable mechanisms, and comparative verification was

range by injection and clarified the inception mechanism of aperformed for models and engine tests.

stall. A method of expanding the operating range on the basis of

Session attendance was 20 to 30 per paper;

this concept is expected to be actively studied in the future.

numerous question-and-answer sessions and discussions wereactive; and time allocation was appropriately managed.

by Takahiro Nishioka (Hitachi Plant Technologies)

by Hiroyuki Furukawa (IHI)

5. Exhibition
5.1 Introduction

4.11 Stability Enhancement

From November 14 (Monday) to November 17 (Thursday), theIn the “Stability Enhancement” organized session, five papers

International Gas Turbine Congress 2011 (IGTC '11) exhibition

and two keynote lectures were presented in two sessions. Of thewas held on the 10th floor of the Osaka International

five, four papers concerned expansion of the operating range ofConvention Center (GCO) in the exhibition hall and exhibition

axial fans and axial flow compressors with the use of casing

room on the same floor, an area of approximately 1,000 square

treatment and air separators. The first keynote lecture (KL-01)

meters. Thirty-nine domestic and international companies andreported on optimization of the type of casing treatment oforganizations participated. In addition, 9 exhibiting companies

grooves along the circumference. In this presentation, for

conducted presentations on their products and technologies for

optimization of the groove depth based on surrogate modeling,

students and the general public during the exhibition period.

it was reported that the stall margin was larger than the casing

Fourteen laboratories from 10 universities displayed their

without treatment. In No. 014, the effects of the circumference

activities at the panel exhibits held in the exhibition room. As agroove using analysis of steady-state and unsteady-state RANS

special event, pupils from neighboring elementary schools were

were

the

invited to attend lectures and handicraft classes. A large number

performance type of casing treatment of the circumferenceof participants from the general public were also in attendance.

groove, and capturing this effect through unsteady RANS or

A photo exhibition for the 10th anniversary of IGTC

examined.

Unsteady flow

largely influenced

LES analysis proved important.

is reported in chapter 2.

The effect of a single circumference groove installedon the leading edge of rotor blade was reported in No. 082. CFD

5.2 Company Exhibitions

was used to study these effects on two types of rotor blades, andThe opening ceremony was conducted in front of the exhibition

the effect of the circumferential groove type casing treatment

hall at 11:30 a.m. November 14 (Monday), beginning withwas determined to be dependent on the inception mechanism of

opening remarks from the chairman of the IGTC '11 exhibit

the stall of a single rotor blade as well as the flow induced bycommittee. Approximately 100 attendees participated in thethe groove.

opening ceremony, which was conducted by the president of the
The second keynote lecture (KL-06) reported on theGas Turbine Society of Japan, the vice chairman of themechanism of the effect of the operating range expansion due to

IGTC ’11 organizing committee, and the chairman of thean air separator equipped with radial vanes. It was demonstrated

IGTC ’11 executive committee. Because the event was heldthat an air separator subject to stall suppression and operating

during a break between presentations, attendance was strong,

range expansion exhibits several features. Apart from these, No.

and the ceremony was considered successful.

070 reported the first model of a three-dimensional wing shape

Exhibitors included companies from a variety ofthat considered stall. No. 099 concerned expansion of operating

technology fields related to gas turbines and jet engines such as

22

gas and steam turbines; gas turbine superchargers; materials,

Table 5.1 List of Company Exhibitors
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18

parts, and related equipment; machine tools; test equipment;
measurement and data processing equipment; computers andrelated software; and publications. In addition, special panels
were held, and presentations included actual products andmock-ups, as well as video features.
Booth demonstrations afforded each company theopportunity to demonstrate its respective products and software.
During the exhibition period, a special stage was set up in thecompany’s exhibition section of the main exhibition hall. Nine
companies introduced their products and latest technologies, andeach offered lectures for university students that were scheduled

19
20
21
22
23
24
25
26

to coincide with the open seminar for other students and generalaudiences, which were highly successful.
In addition, for the first time in congress history,
approximately 100 pupils from neighborhood elementary

27
28
29
30
31
32
33
34
35
36
37
38
39

schools were invited to a lecture titled “How Does an Airplane
Fly?” and were given handicraft lessons in a lecture titled“Build a Wind Car” to provide an understanding of gas turbines.
Including university students and elementary school pupils,
approximately 660 people attended the company exhibitor’s
events.

Tyco Thermal Controls Japan Co., Ltd.
Brüel & Kjær Japan
Japan Aerospace Exploration Agency
General Electric International Inc.
SHINWA CORPORATIONSHINKAWA Electric Co., Ltd.
DAIICHI SYSTEM ENGINEERING Co., Ltd.
OHTE GIKEN Inc.
B&B-AGEMA
Concurrent Nippon Corporation
UEMURA GIKEN Co., Ltd.
Softinway, Inc.
Spraying Systems Co., Japan
Maruyama Excell Co., Ltd.
VINAS Co., Ltd.
Atsuita Press Industry Co., Ltd.
Ohmura Seisakusho Co., Ltd
National Institute of Advanced Industrial Science andTechnology
IHI Castings Co., Ltd.
NIPPON MUKI Co., Ltd.
WOODWARD GOVERNOR (JAPAN), Ltd.
Fuji Techno Industries Corporation
Maruwa Electronic Inc.
Mitsubishi Heavy Industries, Ltd.
Kawasaki Heavy Industries, Ltd.
MITSUBISHI HEAVY INDUSTRIES PRECISIONCASTING Co., Ltd
Japanese Aero Engines Corporation
Honda
EAGLE INDUSTRY Co., Ltd.
TOSHIBA Corporation
AIKOKU ALPHA CORPORATION AP DIVISIONJAPAN AIR TECCo., Ltd.
WOOD GROUP
Rotadata, Ltd. (International Servo Data Corp.)
EVERLOY SHOJI Co., Ltd.
SANKYO INTERNATIONAL Corp.
Reaction Design Japan, KK
IHI Corporation
Hitachi Ltd. Power System Co.

5.3 Student Exhibitions
The student exhibitions began November 14 (Monday) andTable 5.2 Number of exhibition visitors

ended November 17 (Thursday). Each university presented the

DateOpening hours

contents of its latest research on panel displays, while someNovember 14 (Mon)
November 15 (Tue)November 16 (Wed)November 17 (Thu)
Cumulative total
number of visitors

11:30–17:00 (5.5h)
10:00–17:00 (7 h)
10:00–17:00 (7 h)
10:00–14:00 (4 h)universities distributed introductory fliers. The ability to observea summary of trends in gas turbine engine research atuniversities helped to make the event a great success.

23(Total: 23.5 h)

Number ofvisitors
1,013
874
1,155
910
3,952

Table 5.3 List of Student Exhibitors
Name of laboratories of university exhibitors
Kawada Laboratory, Osaka Institute of Technology
Watanabe Laboratory, University of Tokyo
Takeishi and Komiyama Laboratory, Osaka University
Ota Laboratory, Waseda University
Yamamoto Laboratory, Tokyo University of Science
Yuasa Laboratory, Tokyo Metropolitan University
Hayashi Laboratory/Tsujita Laboratory, Hosei University
Yamasaki Laboratory, Kyushu University
Tsujimoto Laboratory, Osaka University
Honami Laboratory, Tokyo University of Science
Funazaki Laboratory, Iwate University
Furukawa Laboratory, Kyushu University
Yamamoto/Sasao Laboratory, Tohoku University
Yoshida/Iwai/Saito Laboratory, Kyoto University

Photo 5.3

Student exhibition (exhibition room)

Photo 5.1 Opening ceremony
Photo 5.4

Exhibitor’s event

by Junichiro Masada (Mitsubishi Heavy Industries)

6. Plant Tours
On November 18, the final day of the congress, two different
plant tours were provided. Tour 1 visited the Senboku Gas Plant
of Osaka Gas Co., Ltd., and Sakaiko Power Plant of Kansai
Electric Power Co. Inc. Twenty-nine people attended the tour,
including two members of the event committee and 27
Photo 5.2

participants from three countries; 23 were from Japan. In the

Company exhibition space (exhibition hall)morning, the group visited the Senboku Gas Plant of Osaka Gas.
A video introduction to Osaka Gas and the Senboku Gas Plant
in the Gas Science Museum, and the tour continued by bus andon foot. In the turbine building, visitors were offered a closeview of the exterior of a steam turbine, generator, and 7EA+egas turbine. In the question-and-answer session, questions wereraised on earthquake and tsunami measures for power plants in24

coastal areas in light of the March 11 earthquake.
After lunch, the group visited Sakai City Hallobservation lobby for sightseeing. Although cloudy skies
persisted, the visitors were able to enjoy views of the tomb ofEmperor Nintoku and Osaka Bay.
The tour then arrived at the Sakaiko Power Plant of
Kansai Electric Power Co., Inc., and received a video
introduction to Kansai Electric Power Co., Inc., as well as
Sakaiko Power Plant in the company’s seminar room. After

Photo 6.1 Tour 1 at Senboku Gas Plant, Osaka Gas Co., Ltdinspecting the central control room, the tour continued withobservations of the power generation equipment, mainly frominside the bus. The interior of the power plant contained
abundant greenery, which demonstrated the company’s position
on environmental issues.
Tour2visitedTakasago

MachineryWorks,

Mitsubishi Heavy Industries, Ltd., and the Akashi and Seishin
plants of Kawasaki Heavy Industries Co., Ltd. Thirty-eightparticipants from five countries, including 19 from Japan andPhoto 6.2 Tour 2 at Takasago Machinery Works, Mitsubishi

two committee members, attended the tour.

Heavy Industries, Ltd

The bus departed from the Osaka International
Convention Center on time. In the morning, the group visitedby Yasuhiro Kinoshita (Kawasaki Heavy Industries)

Takasago Machinery Works, Mitsubishi Heavy Industries, Ltd.
A video introduction to the company’s gas turbine business wasshown, after which the group observed the manufacturing
process from element to assembly and the plant’s combined
cycle (T-point). The tour lasted less than two hours and was richin content. After lunch, the group visited the Seishin Plant of
Kawasaki Heavy Industries Co., Ltd., to observe the assemblyof medium-pressure compressors for large aircraft engines. The
tour then continued to the Akashi plant, where the group visitedthe industrial gas turbine overhaul shop and domestic private
power generation energy center. Both companies divided thevisitors into two groups to allow for plenty of questions andanswers. The tour ran later than the scheduled return time andwas forced to forgo a scheduled stop in Maiko Park on the way
back. However, they were fortunate enough to get a close viewof the Akashi Kaikyo Bridge from the bus windows, lit up in
rainbow-colors.

25