Abstract:
A method that is provided that the at least one section of the flow engine includes at least a part of a combustion chamber of a gas turbine and is treated with at least a component with at least a biocatalytic activity, wherein the least one component with at least a biocatalytic activity is used for degradation of at least a substance with high hydrocarbon content, which is a carbonization arising during a combustion process. The invention further relates to a use of the at least one component with the at least one a biocatalytic activity for the treatment of the at least one section of the flow engine.

Description:
CROSS REFERENCE TO RELATED APPLICATIONS 
       [0001]    The present application claims priority to European Patent Office application No. 12164296 EP filed Apr. 16, 2012, the entire content of which is hereby incorporated herein by reference. 
       FIELD OF INVENTION 
       [0002]    The present invention relates to a method for a treatment of at least a section of a flow engine. 
       ART BACKGROUND 
       [0003]    In combustion chambers of gas turbines fuel is burned for generating thermal energy. The combustion chamber comprises a burner body with a pilot burner face, wherein the latter comprises a liquid fuel lance having a conduit for guiding the liquid fuel to a tip provided for injecting pilot fuel into the combustion chamber. Holes are provided in the tip for injecting cooling medium, which cools the lance tip and interacts with the fuel injected from the lance tip to create a homogeneous air/fuel mixture. 
         [0004]    In order to achieve a combustion with low emissions, it is a need to achieve a high degree of atomization of the fuel in a main operating range. During a start-up phase and during low load operation of the gas turbine, a less distributed fuel spray with large droplets is generated, due to the reduced mass flow and pressure. This increases the tendency of the fuel for splashing and smearing and especially to deposit on the lance tip and the adjacent areas. During operation the fuel covered surfaces on the pilot burner surface may coke and carbonize, such that a hard and adhesive coating is generated. This process is driven by the heat from the combustion process. The coke and carbonization onto the pilot burner face may lead to a blockage of the holes for injecting the cooling medium. Hence, the temperature of the lance tip may increase and the fuel flow through the lance tip may ultimately stop if the fuel orifice of the lance tip is blocked by carbonized fuel. All this leads to poor start reliability and requires additional maintenance. 
         [0005]    In order for the combustion system to regain its optimal performance the coke or carbonized deposits will need to be removed with regular intervals. Different methods are known and used in the removal process i.e. mechanical removal with mechanical tools such as rotating brushes, metal grinder or files, or liquid cleaning with various liquids such as acids. From US 2009/0293906 it is for example known to use an ultrasonic transducer in combination with a cleaning fluid to make the cleaning more effective. Disadvantageously, those methods either damage a base material of the burner body or the fuel nozzle or does not remove all of the deposits, which changes the spray characteristics and hence the combustion performance. 
         [0006]    In other approaches, the critical surfaces of the elements of a gas turbine that are in contact with fuel are coated with high temperature alloys with a coke inhibiting layer. 
       SUMMARY OF THE INVENTION 
       [0007]    It is a first objective of the present invention to provide a method for a treatment of at least a section of a flow engine which provides good treatment results and is quick in its performance. 
         [0008]    It is a further objective of the present invention to provide a use of at least a component with at least a biocatalytic activity for a treatment of at least the section of the flow engine. 
         [0009]    These objectives may be solved by a method and use according to the subject-matter of the independent claims 
         [0010]    According to a first aspect of the present invention, a method for a treatment of at least a section of a flow engine is presented. 
         [0011]    It is provided, that the at least one section of the flow engine comprises at least a part of a combustion chamber of a gas turbine and is treated with at least a component with at least a biocatalytic activity, wherein the least one component with at least a biocatalytic activity is used for degradation of at least a substance with high hydrocarbon content, which is a carbonization arising during a combustion process. Due to the inventive matter an environmental friendly method can be provided. Moreover, it operates independently, especially from an external source, e.g. an operator or an energy source. It should be noted, that a supplying of a specific environment, like an adjusted or applied temperature, pressure, humidity, pH-value, salt-concentration, radiation (IR-, UV-, VIS-, X- or radioactive radiation) or similar should not be understood as external source. Further, the inventive method performs without a damage of the at least one component or the base material of the at least one component. 
         [0012]    Further, due to the inventive matter a section which is highly affected by the treatment and/or habitually causes problems due to its high contamination during the combustion process can be treated efficiently and properly. Moreover, due to the ability of the at least one component with the at least one biocatalytic activity for degradation of at least a substance with high hydrocarbon content, an easy and effective method for disposing of a contaminating, surplus and/or undesired processing material, post-production material, such as lubricant residues, coating residues, fuel and/or deposited reaction products can be provided. 
         [0013]    In this context a flow engine is intended to mean any engine or machine suitable for a person skilled in the art, e.g. a thermal heating plant, a gas turbine or an internal combustion engine. Furthermore, the phrase “for a treatment” should be understood as any possible treatment which is employable for a person skilled in the art, like a coating, finishing, deburring, dyeing, stripping, polishing, cleaning etc. 
         [0014]    A “biocatalytic activity” is intended to mean the ability to transform, convert, process, digest, catabolise, metabolise or any other action suitable for a person skilled in the art, at least one material or substance by means of a biological mechanism or process. In this context a biological process is intended to mean a process which contributes to a function of a living unit, like a cell, a tissue, an organ or an organism. The effected material or substance could be any material suitable for a person skilled in the art, like a gas, a fluid or a solid material e.g. a ceramic, a polymer, a rubber, grease, an oil, an organic compound or composition etc. 
         [0015]    A “component with at least a biocatalytic activity” may be a substance, a mixture of at least two substances, at least one organism and/or a combination of at least a substance and at least one organism, which possesses the at least one biocatalytic activity. Advantageously, the component is chosen from the group comprising of DNA, RNA, mRNA, siRNA, a peptide, a protein or an active fragment thereof, an enzyme or an active fragment thereof, an antibody or an active fragment thereof, a cell, a cell culture, a tissue, an organ, an organism, a prokaryote, an eukaryote, a protozoa, a metazoan, a microbe, a virus, a bacterium, an archaea, a fungus, an alga, an animal, a plant or the like. Moreover, the component may have more than one biocatalytic activity. Hence, at least two functions or even treatments could be facilitated with one component. In this context “degradation” is intended to mean a chemical decomposition or breakdown, where a separation of a chemical compound into elements or simpler compounds occurs. 
         [0016]    In a preferred embodiment the at least one component with at least one biocatalytic activity is provided from at least a living organism. With this realisation the at least one component is easy to obtain. Furthermore, the living mechanism is able to operate the method self-acting and automatic. The term “provide” should be understood as “build, make, compose, generate and/or secrete”. The living organism may provide the at least one component with at least one biocatalytic activity in situ or beforehand of the treatment and in the latter case may be obtained, harvested or recovered in laboratory scale. Further, the living organism may be any living organism known to a person skilled in the art and can be e.g. , a prokaryote, an eukaryote, a protozoa, a metazoan, a microbe, a virus, a bacterium, an archaea, a fungus, an alga, an animal or a plant. It should be noted, that despite a virus is an infectious particle that can&#39;t live autarkic they are deliberately included in the scope of the invention for example due to their effects in combination with e.g. living organisms. 
         [0017]    Advantageously, the at least one component with the at least one biocatalytic activity is provided from at least a microbe. Due to the easy breeding and harvesting of microbes the at least one component with the at least one biocatalytic activity can be obtained in large quantity in a big scale approach. The microbe may be any microbe known to a person skilled in the art and can be e.g. a virus, a bacterium, an archaea, a fungus, an alga, a protist, and microscopic plant, like green algae, or an animal, like plankton or planarian. 
         [0018]    According to a further preferred embodiment the at least one component with the at least one biocatalytic activity is at least a living organism, like a microbe, a virus, a bacterium, an archaea, a fungus, an alga, an animal or a plant. Hence, the method for a treatment can be applied easily just by bringing together the living organism and the at least one section of the flow engine. Moreover, all characteristics of a living organism, like a capability of a response to stimuli, reproduction, growth, development and maintenance of homeostasis, can be advantageously exploited. 
         [0019]    An especially easy to perform and applied method can be obtained, when the at least one component with the at least one biocatalytic activity is at least a microbe. Thus, due to for example an incubation of the at least one section of the flow engine with the microbe or advantageously a plurality of the same microbe the treatment can be easily implemented. The microbe may be a microbe that is known to ingest chemical energy from minerals or ancient carbon found for example in carbon-rich sources, like shale, rocks or volcanic rocks, respectively. These sources are e.g. sediments at the present the sea floor or at former ocean floors transformed now to formation above or slightly beneath (approx. 100 cm) the ground. Preferably, the microbe is a bacterium or an archaea. Due to the quick self-reproduction of these organisms, a sufficient quantity of treatment substance or the at least one component with the at least one biocatalytic activity may be gained or produced. Furthermore, these organisms have a modest need in maintenance and the space per organism they occupy is minimal, thus saving place during treatment or storage. 
         [0020]    Growth, harvest, incubation, treatment conditions and/or the like beforehand and/or during the treatment of the at least one section of the flow engine, such as temperature, pressure, humidity, pH-value, salt-concentration or radiation, of all the aforementioned substances and/or organisms may be adjusted due to the used substance, organism and/or treatment. This will be accomplished by a person skilled in the art due to his knowledge independently. 
         [0021]    In an advantageously embodiment of the invention just at least one active part/component of the at least one component with the at least one biocatalytic activity is use for the treatment of the at least one section of the flow engine. This may advantageously be a protein, a peptide, an enzyme and/or antibody or an active fragment thereof. Thus, by using only the at least one active part/component complex affords for live maintenance of the living organism may be omitted. Moreover, storage and handling of the at least one component with the at least one biocatalytic activity may be simplified. 
         [0022]    Furthermore, preferably the at least one substance with high hydrocarbon content is built from at least a kerogen. Thus, during the combustion process arising contaminations, especially carbonization of the at least one section of the flow engine, can be eliminated efficiently with the inventive method. A kerogen is intended to mean any type of mixture of organic material (type I to type IV kerogen) of sapropelic, planktonic or humic origin. 
         [0023]    In a further advantageous embodiment the at least one component with at least one biocatalytic activity is used for cleaning of the at least one section of the flow engine. Thus, contaminant can be removed easily as well as uncomplicated. Moreover, a polluted part of the flow engine needn&#39;t to be replaced by a new and clean one. Thus also is cost saving. 
         [0024]    The problem of high contamination during the combustion process is particularly accentuated for gas turbines using dry low emissions (DLE). Furthermore, coking can also be experienced in other than DLE combustion systems operating with poor quality liquid fuels, e.g. specific types of diesel or heating oils. Problems potentially could also be experienced with gas fuels, i.e. coke oven gas or with heavy hydrocarbons. Thus, a reliability of a combustion chamber of such flow engines may be improved. 
         [0025]    It is further provided, that the part of the combustion chamber of the gas turbine is a wall or face e.g. a side wall of a pre-chamber volume. Hence, a surface exposed to a volume or operation environment of the combustion chamber may be advantageously treaded or cleaned, respectively, with the inventive method. 
         [0026]    Alternatively and/or additionally, the part of the combustion chamber of the gas turbine is advantageously a fuel injection device, thus the inventive method provides a treatment of a part of the combustion chamber which is highly affected and/or operationally subjected to high contamination during operation of the flow engine. Preferably, the fuel injection device is embodied as a fuel injection aperture. 
         [0027]    In addition and/or alternatively the part of the combustion chamber of the gas turbine is an igniter device and/or at least advantageously comprises an igniter in a burner body. By means of the inventive method, a treatment of the part of the combustion chamber including an igniter tip of the igniter device is homogenous, because the inventive method provides equally access to all surfaces, even in angled configurations. Preferably, the igniter device is embodied as an igniter. The igniter device may use a fuel in a torch like embodiment e.g. a spark or plasma or laser to ignite the fuel air mixture. During operation the igniter may also over time experience build up of deposits requiring a treatment to regain its performance to reliably ignite the flame in the combustion chamber during the start sequence of the gas turbine. 
         [0028]    According to a further exemplary embodiment the part of the combustion chamber of the gas turbine may be a pilot burner face of a burner body. Hence, clean result without damage of a base material of the burner body can be obtained. 
         [0029]    Alternatively and/or additionally, the part of the combustion chamber of the gas turbine is advantageously a fluid nozzle and/or at least comprises a fluid nozzle in a burner body. Due to the inventive method, a treatment of the fluid nozzle and/or of the part of the combustion chamber including the fluid nozzle is homogenous, because the inventive method provides equally access to all surfaces, even in angled configurations. The term “fluid nozzle” should be understood as any injection device or aperture of the combustion chamber for any fluid feasible for a person skilled in the art, like a fuel and/or a cooling medium. 
         [0030]    According to a further aspect of the present invention, a use of at least a component with at least a biocatalytic activity for a treatment of at least a section of a flow engine comprising at least a part of a combustion chamber of a gas turbine, wherein the at least one component with at least a biocatalytic activity is used for degradation of at least a substance with high hydrocarbon content, which is a carbonization arising during a combustion process is presented. Due to the inventive matter a use of an environmental friendly component can be applied. Furthermore, the use is independent, especially from an external source, e.g. an operator or an energy source. Further, the at least one component with at least one biocatalytic activity performs without a damage of the at least one component or the base material of the at least one component. Further, due to the inventive matter a section which is highly affected by the treatment and/or habitually causes problems due to its high contamination during the combustion process can be treated efficiently and properly. Furthermore, due to the ability of the at least one component with the at least one biocatalytic activity for degradation of at least a substance with high hydrocarbon content, an easy and effective method for disposing of a contaminating, surplus and/or undesired processing material, post-production material, such as lubricant residues, coating residues, fuel and/or deposited reaction products can be provided. 
         [0031]    Moreover, the at least one component with the at least one biocatalytic activity may be applied to the at least one section of the flow engine with any method feasible for a person skilled in the art, e.g. exposing, coating, spraying or incubating/submerging in particular with/in a solution. 
         [0032]    In a further advantageous realisation the at least one section of the flow engine is incubated in at least a solution containing at least the at least one component with the at least one biocatalytic activity. This action does favourably not require supervision. Moreover, due to the incubation in this solution the active component may have equally access to all surfaces, even in angled configurations, ensuring a homogenous treatment result. The treatment of the at least one section may include full submersion of the at least one section or partial submersion i.e. only exposing the surfaces showing the carbonization to the solution. In general, it would be also possible that the at least one section of the flow engine may be exposed in another way than (partly) submersion in the solution, like applying or spraying the at least one solution containing at least the at least one component with the at least one biocatalytic activity i.e. as a coating on the at least one section or on the carbonization. 
         [0033]    In the following section the invention relevant main features of the flow engine or the gas turbine are briefly summarised. 
         [0034]    The combustion chamber comprises at least a main combustion volume and a swirler device. A swirler of the swirler device is located upstream of the combustion volume. In an exemplary embodiment a pre-chamber guides the flow between the swirler and the main combustion volume. 
         [0035]    Further, the combustion chamber comprises at least an injection device or aperture, respectively, such that fuel is injectable into the combustion chamber. In particular, a fuel injection aperture or hole is arranged in a pilot burner face of a burner body and injects the pilot fuel stream into the combustion chamber. The injection aperture may be arranged at a pilot tip of a fuel lance and may be provided with the fuel via a fuel conduit. Depending on the actual size or configuration of the pilot tip it may be preferable to have more than one fuel injection aperture and/or fuel conduit in the same pilot tip. The pilot tip may has a width (diameter) of more than approximately 3 mm, preferably more than approximately 5 mm and less than approximately 25 mm (Millimetres). 
         [0036]    In addition, the combustion chamber comprises at least an igniter device such that the fuel air mixture is ignitable during start up. The ignition device may be an igniter or a conduit providing hot combustion gases from a neighbouring combustion chamber via a so-called cross ignition or cross lightning tube. 
         [0037]    The fuel may be any fuel feasible for a person in the art, e.g. a gaseous fuel and/or a liquid fuel, like heating oil and/or diesel fuel, etc. 
         [0038]    The combustion chamber or the pilot burner face, respectively, may additionally comprise an inlet channel with at least an inlet hole or preferably a plurality of inlet holes for injecting a cooling medium into the combustion chamber. 
         [0039]    The inlet channel may have a width (diameter) of more than approximately 0.2 mm, preferably more than approximately 1 mm and less than approximately 10 mm (Millimetres). 
         [0040]    The combustion chamber or the pilot burner face, respectively, may in addition for example have at least an inlet hole or preferably a plurality of inlet holes for injecting an additional fuel e.g. different fuel into the combustion chamber. The inlet holes may have a width (diameter) of more than approximately 0.2 mm, preferably more than approximately 0.5 mm and less than approximately 5 mm (Millimetres). 
         [0041]    The inlet channel may be formed with a circular, elliptical, triangular, rectangular shape or a combination thereof, for example. Hence, the width may be defined by the hydraulic diameter i.e. the diameter of the circular shape, or the semiminor axis of an elliptical shape or the distance of opposed sides of a rectangular shape. The combination of the number of and dimension of the individual apertures can be selected to promote and control the fuel air mixing and the fuel distribution in the combustion chamber. The achievable time of operation between maintenance may depend on the location and dimension of the fluid aperture. Hence, by using such a larger inlet channel, the risk of completely blocking the inlet channel by coke or carbonized layers may be reduced. 
         [0042]    The cooling medium in the combustion chamber may be, for example, air, steam, a gas fuel e.g. natural gas, a fluid, such as water, or other cooling fluids, which are suitable for cooling e.g. the pilot burner face. Preferably, a cooling medium is applied that cools the pilot burner face and particularly any fuel injection devices and is additionally usable for supporting the combustion inside the combustion chamber, such as an oxidant, e.g. air. 
         [0043]    In particular, the inlet channel and the inlet holes, respectively, for injecting the cooling medium is/are placed close to the fuel injection aperture for generating a sufficient cooling energy for cooling the fuel injection aperture and the fuel lance. A plurality of injection channels for injecting the cooling medium is formed preferably around a circumferential direction along the fuel injection aperture. 
         [0044]    The pilot burner face or a surface exposed to carbonized fuel is preferably alloyed with titanium or a titanium compound. Hence, since titanium is lesser reactive than other metal materials, such as steel or nickel, a clogging and an adhesion of carbonized fuel may be reduced. 
         [0045]    The carbonization may have different causes. As described above, during start-up and low load operation fuel may carbonize onto surfaces of the combustion chamber. Moreover, most gas turbines are designed for so called dual fuel operation, wherein the main fuel is typically natural gas and a back up fuel, used when the main fuel is not available or low in supply, is typically a heating oil or kerosene. During operation it is possible to switch between the fuels without stopping the gas turbine. It may even be possible to continuously run on both fuels at the same time. In such a situation it may be an option to use natural gas instead of air to keep the lance tip cool. The gas fuel is cooler than the air from the compressor and would have a marginal impact on emissions particularly if traded off against the gas pilot fuel flow. 
         [0046]    It has to be noted that embodiments of the invention have been described with reference to different subject matters. In particular, some embodiments have been described with reference to apparatus type claims whereas other embodiments have been described with reference to method type claims. However, a person skilled in the art will gather from the above and the following description that, unless otherwise notified, in addition to any combination of features belonging to one type of subject matter also any combination between features relating to different subject matters, in particular between features of the apparatus type claims and features of the method type claims is considered as to be disclosed with this application. 
     
    
     
       BRIEF DESCRIPTION OF THE DRAWINGS 
         [0047]    The aspects defined above and further aspects of the present invention are apparent from the examples of embodiment to be described hereinafter and are explained with reference to the examples of embodiment. The invention will be described in more detail hereinafter with reference to examples of embodiment but to which the invention is not limited. 
           [0048]      FIG. 1 : shows a perspective schematic view of a section of a combustion chamber of a flow engine with a pilot burner face of a burner body which may be treated with a component with a biocatalytic activity according to the inventive method, 
           [0049]      FIG. 2 : shows a detailed schematic view of the pilot burner face from  FIG. 1  with a fuel injection conduit surrounded by cooling medium injection holes, 
           [0050]      FIG. 3 : shows schematically the pilot burner face of  FIG. 1  with carbonizations deposited in its surface, 
           [0051]      FIG. 4 : shows schematically and more detailed the carbonizations at an hole of an igniter of the pilot burner face and 
           [0052]      FIG. 5 : shows the pilot burner face from  FIG. 1  contaminated with carbonizations and disassembled from the flow engine during the treatment with the component with a biocatalytic activity according to the inventive method. 
       
    
    
     DETAILED DESCRIPTION 
       [0053]    The illustrations in the drawings are schematically. It is noted that in different figures, similar or identical elements are provided with the same reference signs. 
         [0054]      FIG. 1  shows a perspective view of a section  10  of a combustion chamber  18  of a not in detail shown flow engine  12  embodied as a gas turbine  22 . The combustion chamber  18  is formed with a tubular-like shape (not shown in detail) which extends in axial direction  38  and comprises a pre-chamber volume  26  and a main chamber  40 , wherein the latter extends in a circumferential direction  42  around the pre-chamber volume  26 . Moreover, the combustion chamber  18  comprises a side wall  24 , which extends basically in a direction  44  perpendicular to the axial direction  38  and is located axially adjacent to the pre-chamber volume  26 . The side wall  24  is a part of a burner body  34  of the combustion chamber  18 . 
         [0055]    Further, the burner body  34  comprises as a part  20  of the combustion chamber  18  and the side wall  24  a pilot burner face  46 , which is a section of a liquid fuel lance  48  that is inserted in the burner body  34 . The liquid fuel lance  48  has a fuel conduit  50  for guiding a liquid or pilot fuel, like No.  2  heating oil, also known as diesel fuel, to a pilot or liquid fuel tip  52  for injection of the liquid fuel. Therefore, the pilot burner face  46 , forming a part of the side wall  24 , and hence the combustion chamber  18  comprises as a further part  20  of the combustion chamber  18  a fluid nozzle  32 , which is embodied as the fuel injection device  28  or a fuel injection aperture. 
         [0056]    As shown in more detail in  FIG. 2 , the pilot burner face  46  or the liquid fuel tip  52 , respectively, comprises as further fluid nozzles  28  several inlet holes  54  for injecting a cooling medium, e.g. air, from a cooling channel  56  extending basically in parallel to and in circumferential direction  42  around the fuel conduit  50  into the combustion chamber  18 . The inlet holes  54  are formed circumferentially around the fuel injection device  28  or aperture as to promote the characteristics of the spray. The cooling medium is normally supplied from a compressor discharge of the gas turbine  22  utilizing the same available pressure drop as the main flow through the burner, however flowing in a parallel stream for the two flows to be joined in the burner cavity. Moreover, as a further part  20  of the combustion chamber  18  an igniter device comprising an igniter  30  is attached to the burner body  34  in order to ignite the injected fuel during start-up. 
         [0057]    Through the fuel injection device  28  or aperture the pilot fuel is injected into the combustion chamber  18  in a predefined direction  58 . The inlet holes  54  have a cross-section through which cooling medium is injected which interacts with the pilot fuel injected in the direction  58  through the fuel injection device  28  or aperture of the pilot burner face  46 . The pilot burner face  46  may locally reach temperatures between approximately 800° C.-1000 C (Celsius) during operation. The inlet holes  54  for injecting cooling air cool the lance tip  52  and the injected cooling medium interacts with the fuel injected from the lance tip  52  to create a homogeneous air/fuel mixture. 
         [0058]    An outer volume  60  of the combustion chamber  18 , which extends in circumferential direction  42 , comprises a swirler device, embodied as a swirler  62 , wherein the swirler  62  is adapted for injecting a main fuel/air stream in circumferential direction  42  into the main chamber  40 . The injected pilot liquid fuel and the injected cooling medium are injected for controlling the combustion of the main fuel/air mixture stream which flows through the swirler  62  of the combustion chamber  18 . 
         [0059]    When the gas turbine  22  is running or during start up, i.e. when cooling air is delivered from a not shown compressor to the combustion chamber  18 , the main acting force on the liquid fuel droplets inside the combustion chamber  18  is the flow field created by the swirler  62  in the combustion chamber  18 . The flow field created by the swirler  62  forms a helical run of the fuel droplets along the axial direction  38  in the combustion chamber  18 . The main fuel i.e. fuel air mixture stream  64  of the flow field containing the fuel droplets is indicated by the arrows printed in  FIG. 1 . The entered fuel may be deposited as a substance  16  with a high hydrocarbon content or out of a kerogen, respectively, and/or may carbonize as a carbonization  66  on parts  20  of the combustion chamber  18  e.g. in the pre-chamber volume  26 , on the side wall  24 , on the igniter  30 , on the tip  52  and inside the inlet holes  54  or a hole  68  of the igniter  30  for the cooling medium due to the high temperature inside the combustion chamber  18  and thus may e.g. block the inlet holes  54 . The deposited substance  16  will reduce the start reliability of the gas turbine  22  as well as the emission performance. In areas  70  where the surface temperature reaches sufficiently high levels during operation the fuel residuals will burn off, e.g. in the centre portion of the pilot burner face  46 . This situation is schematically shown in  FIGS. 3 and 4 . 
         [0060]    This substance  16  and/or carbonisation  66  can be removed by degradation with an inventive method for a treatment or a cleaning, respectively, of the section  10  of the flow engine  12  or the side wall  24  or the part  20  (pilot burner face  46  or a fuel nozzle  28  or the igniter  30 ) of the combustion chamber  18  (in the following text the terms section  10  of the flow engine  12  is used synonymously for the term part  20  of the combustion chamber  18 ). According to this method the section  10  of the flow engine  12  is treated with a component  14  with a biocatalytic activity. The component  14  with the biocatalytic activity, which metabolises or removes by degradation the high hydrocarbon content and/or the kerogens of the substance  16  and/or carbonization  66 , is a microbe and thus a living organism. Generally, it is also possible, that the component  14  is provided from a microbe or a living organism, respectively, and may be, for example, an enzyme of the microbe metabolising or removing by degradation the high hydrocarbon content and/or the kerogens of the substance  16 . 
         [0061]    Therefore, the component  14  with the biocatalytic activity is used for the treatment of the section  10  of a flow engine  12  and specifically by incubating the section  10  in a solution  36 , which contains the component  14  with the biocatalytic activity. This can be seen in  FIG. 5  that shows schematically the pilot burner face  46  with the fluid nozzles  28  and the igniter  30  contaminated with the substance  16  and disassembled from the flow engine  12  during the treatment with the component  14  with a biocatalytic activity according to the inventive method. The incubation time t will be adjusted in a way so that the carbonization  66  will be completely removed. The treatment of the section  10  may include full submersion of the section  10  or partial submersion i.e. only exposing the surfaces showing the carbonization  66  to the solution  36 . 
         [0062]    In  FIG. 5  a dissembled burner face gets the treatment by the component  14 . In other arrangements component  14  may be injected into an assembled gas turbine combustion chamber such that it able to affect the carbonized surfaces in a still assembled burner within the combustion chamber. For this, for example, a cap is placed over the burner face such that the component  14  will be encapsuled by the burner face and surfaces of the cap. The component  14  then can affect the burner face. 
         [0063]    It should be noted that the term “comprising” does not exclude other elements or steps and “a” or “an” does not exclude a plurality. Also elements described in association with different embodiments may be combined. It should also be noted that reference signs in the claims should not be construed as limiting the scope of the claims. 
         [0064]    Although the invention is illustrated and described in detail by the preferred embodiments, the invention is not limited by the examples disclosed, and other variations can be derived therefrom by a person skilled in the art without departing from the scope of the invention.