METHOD OF PRODUCING REVERSE-THRUST TURBINE ENGINE Russian patent published in 2008 - IPC F02K1/56 

Abstract RU 2331781 C2

FIELD: engines and pumps, transportation.

SUBSTANCE: invention relates to aviation, particularly, to the method of producing an aircraft reverse-thrust turbine engine. The proposed method consists in turning the reversing jets in the reversing device by means of flaps and a deflector grill. Here note that the deflector grill blades rear edges are set up at the angle equal to that of the reversing jets turning in the range of ϕ = 90°...135°, while the flaps are arranged so that the deflector grill front edge plane be at the angle of α = 20°...60° relative to the flaps plane.

EFFECT: higher efficiency thrust reverse, efficient protection of the engine of an ingress of foreign objects from the airfield surface attained by increased efficiency of deflector grill.

4 dwg

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RU 2 331 781 C2

Authors

Komov Aleksej Alekseevich

Dates

2008-08-20Published

2006-09-07Filed