|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/216; 244/215; 244/099.3|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 12 인용 특허 : 11|
A trailing edge flap mechanism incorporates a support beam, a flap carrier beam supporting an aerodynamic flap, a first link interconnecting a first and second rotation points and a second link interconnecting third and fourth rotation points. The support beam has a ground connection on a first fixed axis of rotation. A connecting link has a ground connection on a second fixed axis of rotation and is connected to the first link intermediate the first and second rotation points. An actuator is connected with a drive link pivotally engaged to the first lin...
1. A trailing edge flap mechanism for an aircraft comprising: a support beam having a first portion with a first rotation axis and a fourth rotation axis aft of the first rotation axis;a flap carrier beam supporting an aerodynamic flap, said carrier beam having a second rotation axis at a forward end and a third rotation axis within a nose contour of the flap aft of the second rotation axis;a first link interconnecting the first rotation axis and second rotation axis;a second link interconnecting the third rotation axis and fourth rotation axis;said supp...