|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/102.R; 244/100.0R; 244/102.0A; 244/102.0SS; 244/103.0R|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 16 인용 특허 : 9|
In an aircraft having an aircraft landing gear, the aircraft landing gear includes an arm, a leg and a bogie at the lower end of the leg. The bogie is moveable in a direction along the length of the leg and pivotable between a trimmed deployed position and a stowable position. The arm is mounted on the landing gear and is rotatable between a first position in which the bogie is positioned in the trimmed deployed position, and a second position in which the bogie is positioned in the stowable position. Movement of the arm can be effected by a positioning ...
The invention claimed is: 1. An aircraft, comprising an aircraft landing gear, the aircraft landing gear comprising: an arm, an actuator arranged to rotate the arm, a stop for limiting rotary movement of the arm during takeoff and landing of the aircraft, a leg on which the arm is rotatably mounted, and a bogie at a lower end of the leg, the bogie being moveable in a direction along a length of the leg and pivotable between a trimmed deployed position and a stowable position, wherein movement of the bogie between the trimmed deployed position and the st...