|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/054 ; 244/055 ; 244/120 ; 244/248 ; 244/554|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 30 인용 특허 : 1|
The present invention provides a tailcone and power assembly mountable to the body of an aircraft using a height adjustable dolly. The tailcone assembly comprises a longitudinal support member, a gas turbine engine mounted to the support member; a firewall; two curved rotatable casings hingeably connected to the support member; an inlet duct extending from an aperture in one of the rotatable casings to the engine inlet; an integral exhaust casing, and interface means for making necessary engine accessory connections to the aircraft. The tailcone is insta...
[ What is claimed is:] [1.]1. An aircraft tailcone assembly comprising:a longitudinal support member having forward and aft axial ends;a gas turbine engine mounted within said tailcone to said support member, said engine having an inlet and an exhaust;a firewall extending from said support member forward of said engine;at least one curved rotatable casing hingeably connected to said support member and rotatable from a closed position to an open position thereby exposing said engine;an inlet duct extending from an aperture in one of said rotatable casings...