|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/216 ; 244/215 ; 464/160|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 8 인용 특허 : 5|
A wing gap closure flap is positioned in an aircraft wing so that a gap between the wing structure and the leading edge of a landing flap can be closed during normal cruising positions of the landing flap and opened when the landing flap is in a starting position or in a landing position. The gap is formed on the underside of the aircraft wing and the gap closure flap is operated by a positioning shaft which itself is driven through a drive lever linkage by the drive shaft for the landing flap. The wing gap closure flap is connected through a lever mecha...
An apparatus for controlling a wing gap in an aircraft wing having landing flaps (3) forming said wing gap, comprising at least one wing gap closure flap (1), at least one rotational positioning shaft (4) for operating said wing gap closure flap (1), bearings rotatably mounting said positioning shaft (4) in said aircraft wing, at least one lever mechanism (5) operatively connecting said positioning shaft (4) with said wing gap closure flap (1), at least one landing flap drive (7) and a drive coupling for transmitting power from said landing flap drive to...