Aircraft propulsion systems

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Referat, Hausaufgabe, Aircraft propulsion systems
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Referat
Aircraft propulsion systems This report treats the aircraft propulsion systems. It`s structured into four parts. 1st part: the turbojet engine 2nd part: the turbofan engine 3rd part: the turboprop engine 4th part: the ramjet engine 1st part: the turbojet engine: The first turbojet engine was flown in Germany in 1939. It was tested on a Heinkel He 178. The engines which now are in use, are in a great deal more complicated and are producing more thrust. A cutaway view of a three shaft turbojet engine with afterburner, as used at the supersonic fighter PANAVIA TORNADO, the Turbo Union RB 199-34R is shown here. The technical data from the RB199-34R are: max. thrust with afterburner........71 kN pressure-difference.....................23 rotation speed..............................12´000 ...

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Referat
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Englisch
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