Patent application number | Description | Published |
20080315064 | SUSPENSION FOR SUSPENDING A TURBINE ENGINE FROM THE STRUCTURE OF AN AIRCRAFT - The present invention relates to the suspending of a turbine engine from the structure of an aircraft using a beam with means of attachment to said structure and at least one link rod articulated via one end to a journal secured to the beam and via the other to a 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, elastomer and metal, cylinders. | 12-25-2008 |
20090032673 | FLEXIBLE SUSPENSION FOR TURBINE ENGINE - The present invention relates to a suspension for suspending a turbine engine from the structure of an aircraft, comprising a beam with a first element accepting means of attachment to said structure and a second element accepting means of attachment to the turbine engine. It is one wherein the beam comprises at least a first plate and a second plate, which plates are intended to be positioned transversely with respect to the axis of the engine and joined together by a layer of elastomer, the first plate being secured to the first element and the other plate to the second element. | 02-05-2009 |
20100096495 | AIRCRAFT WITH RECIPROCATING ENGINES PARTIALLY EMBEDDED IN THE FUSELAGE - Aircraft provided with turbojet engines of which the nacelles are partially embedded in the fuselage of the aircraft, characterised in that it comprises on engine nacelles an internal space comprising a platform capable of supporting personnel and maintenance equipment, with the portions of the nacelles located inside the aircraft comprising trapdoors or means for accessing inside the engines from the platform. | 04-22-2010 |