Turbojet
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High Quality Content by WIKIPEDIA articles! Turbojets are the oldest kind of general purpose jet engines. Two engineers, Frank Whittle in the United Kingdom and Hans von Ohain in Germany, developed the concept independently into practical engines during the late 1930s, although credit for the first turbojet is given to Whittle who submitted the first proposal and held a UK patent that was widely read. Turbojets consist of an air inlet, an air compressor, a combustion chamber, a gas turbine (that drives the air compressor) and a nozzle. The air is compressed into the chamber, heated and expanded by the fuel combustion and then allowed to expand out through the turbine into the nozzle where it is accelerated to high speed to provide propulsion.
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GarantieWeitere Informationen
- Allgemeine Informationen
- GTIN 09786130321048
- Genre Technik
- Editor Lambert M. Surhone, Miriam T. Timpledon, Susan F. Marseken
- Sprache Englisch
- Anzahl Seiten 160
- Herausgeber VDM Verlag Dr. Müller e.K.
- Größe H220mm x B150mm x T10mm
- Jahr 2009
- EAN 9786130321048
- Format Fachbuch
- ISBN 978-613-0-32104-8
- Titel Turbojet
- Untertitel Jet Engine, Cruise Missile, Flame Holder, General Electric CF6, Rolls-Royce/Snecma Olympus 593, Messerschmitt Me 262, De Havilland Comet, Concorde, Thrust2, Jet Dragster
- Gewicht 256g
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