Jet Turbine engine cross section (UEB Uncontracted)

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Synopsis: In these diagrams of a jet engine, there is a cross section view through the length of the engine at the top of the page and in the bottom right of the page, a front view of the engine intake. There is a locator dot shown, which will be at the top left of the page when the image is the right way up. On the left of the page air is forced into the engine by the compressor which has many fan blades. The compressed air is fed into the combustion chamber in the middle of the page. Fuel is injected into the engine through a port in the lower centre part of the combustion chamber. This is where combustion and gas expansion takes place. On the right of the page the exhaust exits past the turbine producing the thrust of the engine. The front view shows the circular opening of the engine with lots of fan blades arranged around the central hub like a huge fan.