|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||B64D-015/02 B64D-015/04 B64D-015/06|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 3 인용 특허 : 14|
An airplane leading edge de-icing apparatus having a heat diffuser for heating the leading edges of an airplane is provided. The heat diffuser has a first heat diffuser side having a concave shape and a second heat diffuser side having a convex shape. The heat diffuser is joined to the leading edge of an airplane. A counter current heat exchanger is provided and heats a heat transfer fluid with heat energy absorbed from hot gases. The heat transfer fluid is pumped in and out of a reservoir tank with a first pump. A second pump pumps the heat transfer flu...
1. An airplane de-icing apparatus for de-icing a leading edge of an airplane with a heat transfer fluid, the airplane deicing apparatus comprising: a counter current heat exchanger;a reservoir tank;a first pump;a first reservoir tube joined to the first pump and the reservoir tank, and a first pump tube and a check valve and wherein the first pump tube is joined to the check valve and the first pump;an inlet tube joined to the check valve and the counter current heat exchanger, and wherein a first reservoir inflow tube is joined to the countercurrent hea...