|국가/구분||United States(US) Patent 등록|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 2 인용 특허 : 12|
A hatch-actuating mechanism, particularly for aircraft landing gear. The mechanism includes a lateral closing panel (1) and a secondary closing panel (4) articulated to one another. A lateral pivoting fitting (5) is joined to the lateral panel (1) and pivots about a fixed point on the structure (7). A secondary pivoting fitting (8) is joined to the secondary panel (4). A lateral actuating cylinder (10) controls the movement of the lateral panel. An intermediate actuating cylinder controls the movement of the secondary panel, the intermediate actuating cy...
The invention claimed is: 1. A hatch-actuating mechanism, for an aircraft landing gear, comprising a lateral closing panel dimensioned to cover, in hatch-closed position, a first lateral area of an access opening to an interior space, leaving free a first strip neighboring said first lateral area; a secondary closing panel dimensioned to cover, in hatch-closed position, at least part of the first strip, which is not covered by the lateral panel; a lateral pivoting fitting rotatably connected via a first lateral articulation to a first fixed structure wh...