Aeronautics and astronautics – Aircraft power plants – Mounting
Reexamination Certificate
2005-08-01
2009-12-01
Mansen, Michael R (Department: 3644)
Aeronautics and astronautics
Aircraft power plants
Mounting
C248S554000, C060S796000, C060S797000
Reexamination Certificate
active
07624945
ABSTRACT:
The invention relates to an engine assembly for an aircraft comprising a turbojet, a engine mount pylon, and a plurality of engine mounts inserted between the engine mount pylon and the turbojet. According to the invention, the plurality of engine mounts comprises a engine mount (6a) designed so as to uniquely resist forces applied along a direction (Y) transverse to the turbojet, this engine mount (6a) comprising an intermediate fitting (46) assembled onto a first fitting (40) fixed to the pylon through two swivel axes (48) oriented parallel along a vertical direction (Z), and a pin (56) oriented along a longitudinal direction (X) and fixed to the intermediate fitting, the pin being installed on a second fitting (58) fixed to the turbojet, with clearance along the longitudinal direction (X).
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Diochon Lionel
Seguin Guillaume
Airbus France
Bonzell Philip J
Mansen Michael R
Oblon, Spivak McClelland, Maier & Neustadt, L.L.P.
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