|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/213 ; 244/90R ; 244/215 ; 244/219|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 56 인용 특허 : 0|
A variable contour control surface (30a) and a transition section (30a) are designed to eliminate the discontinuities that exist between an aircraft wing control surface and the wing itself. The variable contour is provided by translating the top skin of the control surface relative to the top surface of the wing with the bottom surfaces of the wing and control surface being joined as a single surface. This movement results in a change in the camber of the control surface. The transition section (30a) is a flexible connection between the inboard and outb...
An aircraft wing assembly comprising: (a) a main wing portion having a top skin and a bottom skin; (b) a variable contour control surface having a top skin and a bottom skin, either said top skin of said variable contour control surface or said bottom skin of said variable contour control surface being attached to the corresponding top or bottom skin of the main wing portion and the other skin of said variable contour control surface being translatable relative to the corresponding other skin of the main wing portion; (c) means for translating said trans...