|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||60/226.1 ; 60/039.07|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 42 인용 특허 : 6|
According to the invention, said heat exchanger (18) is arranged at the forward part (13A) of the engine (1) support pylon (13), being traversed by said air stream (21) which leaves the fan (6) and is not directed toward the compressors (3).
[ I claim:] [1.] A device for bleeding off and cooling hot air in an engine of an aircraft, the aircraft having a body, said engine comprising:an engine body having a compressor, a combustion chamber and a turbine, the engine defining an upstream direction and a downstream direction;a fan arranged in the upstream direction from the engine body, for causing a flow of cold air in the downstream direction;a fairing assembly comprising an air intake, a fan shroud and outer and inner fairings;linking means for connecting the engine body and the fan shroud; an...