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|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||F01D-011/02 F01D-011/00 B64C-027/22 B64C-027/00|
|미국특허분류(USC)||244/012.4; 244/012.3; 244/012.5; 244/023.A; 244/023.B; 244/023.C; 277/307; 277/309; 277/355; 415/173.3; 415/174.2|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 2 인용 특허 : 10|
A high-speed vertical take-off and land aircraft includes a body with an engine supported by the body. A fan assembly is also carried by the body. The fan assembly includes a hub and a plurality of blades to provide vertical lift for the aircraft. A nozzle ring is provided on the fan assembly. The nozzle ring includes an annular nozzle array. Hot gases from the engine are fed to the nozzle array by a feed duct. A bearing mechanism supports the fan assembly on the body. The bearing mechanism is carried in a work space. A brush seal assembly thermally iso...
What is claimed: 1. A high-speed vertical take-off and land aircraft, comprising: a body; an engine supported by said body; a fan assembly carried by said body, said fan assembly including a hub and a plurality of blades to provide vertical lift for said aircraft; a nozzle ring on said fan assembly providing an annular nozzle array for ejecting hot exhaust gases at a temperature from said engine; a feed duct receiving said hot exhaust gases from said engine and directing said hot exhaust gases to said annular nozzle array; an interface between said feed...