SUSPENSION DEVICE FOR SUSPENDING TURBINE ENGINE FROM STRUCTURE OF AIRCRAFT

摘要

PROBLEM TO BE SOLVED: To provide a static type suspension device for suspending a turbine engine of a structure of an aircraft, in which a flexible vibration insulation device is incorporated and which is as compact as possible. SOLUTION: The present invention relates to the suspension of a turbine engine from the structure of an aircraft using a beam with a means of attachment to the above structure and at least one link rod articulated via one end to a journal secured to the beam and via the other end to an attachment fitting secured to the turbine engine. This suspension is one wherein the journal is mounted on the beam via a flexible coupling formed of two preloaded laminated cylinders of elastomer and metal. COPYRIGHT: (C)2009,JPO&INPIT