Patent ID: 9254914
Filing Date: 2016-02-09
CPC Classification: B64C,F16F

Claim Text:
1. An Aircraft transmission restraint system, wherein the restraint system comprising: a first strut having a first piston resiliently coupled to a first housing with a first elastomeric member, wherein the first housing, the first piston, and the first elastomeric member form a first fluid chamber; a second strut having a second piston resiliently coupled to a second housing with a second elastomeric member, wherein the second housing, the second piston, and the second elastomeric member form a second fluid chamber; a fluid line placing the first fluid chamber and the second fluid chamber in fluid communication; a fluid in the first fluid chamber, the second fluid chamber, and the fluid line; wherein an actuation of the first piston and the second piston in a first direction causes a portion of the fluid to move into one of the first fluid chamber and the second fluid chamber.