Patent ID: 11912399
Assignee: GOODRICH CORPORATION
Field: Mechanical elements (Mechanical engineering)
Classification: CPC B  F | IPC B  F

Claim 0:
1. An aircraft actuation system comprising:
a pinion;
a first cylinder;
a first piston movably disposed within said first cylinder;
a second cylinder disposed in non-collinear relation with said first cylinder;
a second piston movably disposed within said second cylinder;
a transfer member interconnected with each of said first piston and said second piston, wherein at least part of said transfer member is disposed out of each of said first and second cylinders and is engaged with said pinion; and
an outer race extending from a first end of said first cylinder, around a portion of said pinion and spaced from said pinion, and to a first end of said second cylinder,
wherein movement of said first piston and said second piston within said first cylinder and said second cylinder, respectively, moves said transfer member to rotate said pinion.