|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/054 ; 244/120 ; 181/212 ; 181/222 ; 248/554|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 62 인용 특허 : 2|
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 integrated muffler and exhaust cone for use in an aircraft tailcone having a gas turbine engine mounted therein, comprising:an exhaust cone portion of an aircraft tailcone extending from a forward end to and an aft end that opens to ambient, said exhaust cone portion defining an interior chamber, said exhaust cone portion further having a bulkhead at the forward end that fluidly isolates the interior chamber from the remainder of said tailcone; said bulkhead also having an aperture;a solid casing defining a conduit having...