|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/215 ; 241/213 ; 241/217|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 12 인용 특허 : 4|
Flap carriers fold spanwise (about chordwise axes) into the wing but are moved down together through pivotal linkage; the flaps are protracted and retracted through pivoting of the carriers relative to each other on spanwise axes. On retraction, the entire assembly fits into the wing so that the flow determining contour thereof remains undisturbed.
Flap arrangement with adjustment devices along the trailing edge of an aircraft wing, having a plurality of wing flaps, comprising: a first flap carrier, pivotably mounted to the wing, on shaft means which extend in chord direction of the wing, said shaft means being slidably mounted in a recess on the underside of the wing, for sliding in spanwise direction, said first carrier thus being provided for pivoting and down extension as well as sliding, in and retraction into the recess in the wing, while undergoing a combined sliding and pivot motion for dow...