|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/134B ; 60/39093|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 45 인용 특허 : 0|
Thermal anti-icing systems for aircraft and methods for fabricating such systems. The anti-icing systems have an integrated one-piece skin with passageways formed therein to supply a heated fluid to that portion of an aircraft structure where anti-icing is desired. The anti-icing system also has an integrated or separately supplied manifold for routing heating fluid to the anti-icing system flow passages. The anti-icing system can be used in the leading edges of such aircraft structures as wings, horizontal and vertical stabilizers, inboard and outboard ...
The combination of an aircraft structure having a leading edge and a system for heating said structure to inhibit the formation of ice on said leading edge, said structure having an outer skin with spaced apart, exposed surface defining segments and said heating system including: a. an inner skin with a segment of complementary configuration adjacent a segment of said outer skin and cooperating therewith to form a series of flow passages which: are disposed in side-by-side relationship, extend from the leading edge of said structure toward the rear there...