|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||B64D-015/02 B64D-015/08 B64C-001/12|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 0 인용 특허 : 6|
A combination of liquid-to-air and air-to-liquid heat exchangers is employed in an aircraft anti-icing system configured to avoid ice buildup on exterior leading edges of wings and engine inlets of aircraft during flight under known or anticipated icing conditions. The anti-icing system may be utilized in lieu of traditionally employed air-to-air heat exchangers. In one embodiment, a heated anti-icing liquid is conveyed through tubes juxtaposed against interior surfaces of the leading edges of the wings and engine inlets. The liquid is heated by engine c...
1. An aircraft wing anti-icing system comprising: a liquid-to-air heat exchanger including a plurality of heated anti-icing liquid-conveying tubes secured directly to an interior surface of a leading edge of a wing; andan air-to-liquid heat exchanger located at a fuselage of an associated aircraft, spaced away from wings and engines supported on the aircraft, the air-to-liquid heat exchanger configured to transfer heat of engine core bleed air between at least one of the engines and the air-to-liquid heat exchanger, to the liquid-to air heat exchanger;wh...