Patent ID: 8496202

Claim:
A force transmission system between a turboprop and an attachment device of the turboprop on an aircraft, the force transmission system comprising: a first force transmission device and a second force transmission device; and first means for fluid communication between the first force transmission device and the second force transmission device, wherein each of the first force transmission device and the second force transmission device includes a first hollow cylinder with an axis that is parallel to a first force transmission direction wherein each of the first hollow cylinders has a first space full of a first fluid and is closed off in a sealed manner at two opposite ends thereof by a first damping layer that bears in contact with a bearing element of the turboprop and by a second damping layer that bears in contact with a bearing element of the attachment device, respectively, wherein said first and second damping layers are positioned so as to be compressed by a pressure of said first fluid, and wherein the first means for fluid communication is disposed between said first spaces.