|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/215; 244/213; 244/214; 244/131; 277/644; 277/645; 277/647; 277/916|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 15 인용 특허 : 122|
Aerodynamic seals for use with control surfaces on aircraft are described herein. In one embodiment, a seal assembly for use with an aircraft includes a first seal member and a second seal member. The first seal member has a first proximal portion configured to be attached to a fixed airfoil portion of the aircraft, and a first distal portion configured to extend outwardly from the fixed airfoil portion toward a movable control surface. The second seal member has a second proximal portion configured to be attached to the movable control surface, and a se...
We claim: 1. A seal assembly for use with an aircraft, the aircraft having a movable control surface spaced apart from a fixed airfoil portion to define a gap therebetween, the seal assembly comprising: a first seal member having a first proximal portion and a first distal portion, wherein the first proximal portion is fixedly attached to the fixed airfoil portion and the first distal portion extends outwardly from the fixed airfoil portion toward the movable control surface; and a second seal member having a second proximal portion and a second distal ...