| 摘要 |
The present invention relates to a system for opening and closing, in a substantially longitudinal direction, at least one hatch (5) of a landing gear bay (3) of an aircraft (1), characterized in that said system includes: a proximal guide rod (7) and a distal guide rod (6), each having a first end pivotably attachable to the hatch (5), and a second end pivotably attachable to a stationary inner structure of the gear bay (3), and arranged such as to form a deformable parallelogram hinge; and at least one drive rod (8) having a first end that is pivotably attachable to the hatch (5), and a second end that is pivotably attachable to a landing gear leg (2). The invention also relates to a landing gear bay (3) comprising such a system. |
