|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/42D ; 244/130|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 52 인용 특허 : 0|
An extendable fairing for use between two aerodynamic surfaces (e.g., the engine nacelle and wing leading edge flap) of an aircraft is disclosed. The illustrated embodiment of the invention comprises a fixed fairing section, extending outwardly from an engine nacelle, and an extendable fairing section, housed within the fixed fairing section. During cruise, when the flaps are withdrawn, the extendable fairing section is withdrawn. During takeoff and landing, or other conditions when the leading edge flaps are extended, the extendable fairing section is e...
An extendable aerodynamic fairing suitable for use between an engine nacelle and a wing leading edge flap for filling the gap between said engine nacelle and said wing leading edge flap when said wing leading edge flap is extended, said extendable aerodynamic fairing comprising: a fixed fairing section attached to said engine nacelle in an aerodynamic manner, said fixed fairing section starting at a point on the outer surface of said nacelle substantially forwardly of the leading edge of the wing with which said leading edge flap is associated and flairi...