Turbofan engine | Wikipedia audio article
Channel: wikipedia tts
Date: 2019-07-10

This is an audio version of the Wikipedia Article:
https://en.wikipedia.org/wiki/Turbofan


00:01:34 1 Principles
00:03:47 1.1 Bypass ratio
00:06:14 1.2 Efficiency
00:08:18 1.3 Thrust
00:09:36 1.4 Nozzles
00:10:23 1.5 Noise
00:12:55 2 Common types
00:13:04 2.1 Low-bypass turbofan
00:14:47 2.2 Afterburning turbofan
00:17:24 2.3 High-bypass turbofan
00:21:23 3 Turbofan configurations
00:23:17 3.1 Single-shaft turbofan
00:23:55 3.2 Aft-fan turbofan
00:24:46 3.3 Basic two-spool
00:25:33 3.4 Boosted two-spool
00:26:39 3.5 Three-spool
00:27:36 3.6 Geared fan
00:28:20 3.7 Military turbofans
00:28:40 3.8 High-pressure turbine
00:29:39 3.9 Low-pressure turbine
00:30:19 4 Overall performance
00:30:29 4.1 Cycle improvements
00:32:59 4.2 Thrust growth
00:34:26 4.3 Technical discussion
00:40:15 5 Early turbofans
00:43:05 6 Recent developments
00:43:14 6.1 Aerodynamic modelling
00:44:10 6.2 Blade technology
00:46:04 6.3 Fan blades
00:47:13 6.4 Future progress
00:53:06 7 Manufacturers
00:54:40 7.1 Gallery
00:54:49 7.2 Commercial turbofans in production
00:54:58 8 Extreme bypass jet engines
00:55:57 9 Terminology
00:59:56 10 See also



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SUMMARY
=======
The turbofan or fanjet is a type of airbreathing jet engine that is widely used in aircraft propulsion. The word "turbofan" is a portmanteau of "turbine" and "fan": the turbo portion refers to a gas turbine engine which achieves mechanical energy from combustion, and the fan, a ducted fan that uses the mechanical energy from the gas turbine to accelerate air rearwards. Thus, whereas all the air taken in by a turbojet passes through the turbine (through the combustion chamber), in a turbofan some of that air bypasses the turbine. A turbofan thus can be thought of as a turbojet being used to drive a ducted fan, with both of these contributing to the thrust.
The ratio of the mass-flow of air bypassing the engine core divided by the mass-flow of air passing through the core is referred to as the bypass ratio.  The engine produces thrust through a combination of these two portions working together; engines that use more jet thrust relative to fan thrust are known as low-bypass turbofans, conversely those that have considerably more fan thrust than jet thrust are known as high-bypass. Most commercial aviation jet engines in use today are of the high-bypass type, and most modern military fighter engines are low-bypass. Afterburners are not used on high-bypass turbofan engines but may be used on either low-bypass turbofan or turbojet engines.
Modern turbofans have either a large single-stage fan or a smaller fan with several stages. An early configuration combined a low-pressure turbine and fan in a single rear-mounted unit.