|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/113 ; 244/53B|
|발명자 / 주소|
|인용정보||피인용 횟수 : 8 인용 특허 : 1|
A combination air brake and engine shield for a jet powered aircraft. A hydraulically operated, hinged shield member, shaped so as to conform to the surface of the aircraft fuselage when in its retracted position, may be swung outwardly therefrom so as to be disposed in front of the air intake of the jet engine powering the craft, to thereby divert any foreign objects from being drawn into the intake and damaging the engine. The same arrangement may also serve as an air brake to effect deceleration of the aircraft. Spring loaded louvers are provided in t...
A combination air brake and engine shield for a jet-type aircraft comprising, in combination: (a) an airframe having a fuselage with wing members structurally attached thereto along a line which is displaced downward and parallel to the longitudinal axis of said fuselage; (b) first and second jet-type engines, each having an air intake section and mounted on either side of said fuselage, Extending outwardly from the exterior surface thereof and disposed above said wing members; (c) first and second recesses formed in the exterior surface of said fuselage...