|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||F02K-003/02 F02K-099/00 F02C-006/08 F02K-003/06 F02C-007/14 F02C-007/18 B64D-033/10 B64D-027/18 F02C-007/224 F02K-003/115 B64D-029/00|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 0 인용 특허 : 33|
A thermal management system includes at least one heat exchanger in communication with a bypass flow of a gas turbine engine. The placement of the heat exchanger(s) minimizes weight and aerodynamic losses and contributes to overall performance increase over traditional ducted heat exchanger placement schemes.
1. A thermal management system for a gas turbine engine comprising: a bifurcation area;at least one heat exchanger mounted within said bifurcation area in communication with a bypass flow from the gas turbine engine, said at least one heat exchanger positioned downstream of a fan strut, said fan strut spanning between a core nacelle of said gas turbine engine and a fan nacelle of said gas turbine engine;wherein said at least one heat exchanger includes first and second heat exchangers, said first and second heat exchangers mounted within a common plenum ...