Patent 7296414 was granted and assigned to Rolls-Royce on November, 2007 by the United States Patent and Trademark Office.
A mounting assembly (10) for mounting a gas turbine engine on an aircraft. The assembly (10) comprising four equispaced hydraulic piston and cylinder thrust links (16) connecting between the engine fan case (12) and the air intake (14), which intake (14) is mounted to the airframe.