|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/215 ; 244/090A ; 244/090R ; 416/131 ; 416/135|
|발명자 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 14 인용 특허 : 4|
An automatic flap that uses on each wing two adjacent fins, one of which is smaller and is located on the middle or front of the wing, the other, which is larger, on the bottom rear of the wing, with a shaft in the common eccentric zone linking the two fins, said shaft being parallel to the axis of the wing, having the fins different resistance to the ram air, creating a rotation torque as a function of the aircraft's speed, when retracted, they are shaped so that the front or top fin adapts to the upper surface of the wing and the rear or bottom fin ada...
[ What is claimed is:] [1.] An automatic flap on an airplane wings subject to ram air in flight as while moving, characterized by using two adjacent and connected fins, the first is smaller and is located on the top middle portion of said wing, the second is larger than said first fin and is located on the bottom rear of the wing, with a shaft in a common eccentric zone linking said two fins, said shaft being parallel to the an axis of said wing, having said fins with different resistance to said ram air, creating a rotation torque as a function of the a...