Air compression aeroengine

Details Air compression aeroengine Air compression aeroengine

F - Mech Eng,Light,Heat,Weapons

02

K

F02K 1/54 (2006.01)

Patent

CA 2606525

The invention relates to an air compression aeroengine that uses turbine supercharged air compressor to produce high temperature and high pressure gas, then uses the counteractive thrust caused by compressed gas sprayed from the rear jet nozzle or the lower jet nozzle to realize vertical lift and fly forward. The simple structure would decrease the cost. The noise is low. The invention is suited in civil aviation, cargo liner, fighter plane, bomber, and other aircrafts.

L~invention concerne un moteur d~avion à compression d~air qui utilise le compresseur d~air de la turbine suralimentée pour produire un gaz à haute température et sous haute pression, puis utilise la poussée contre réactive provoquée par le gaz compressé vaporisé depuis la tuyère d~éjection arrière ou la tuyère d~éjection inférieure pour réaliser une portance verticale et voler vers l~avant. La structure simple diminue le coût. Le bruit est faible. L~invention est adaptée à l~aviation civile, aux cargos de ligne, aux avions de combat, aux bombardiers, et autres avions.

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