Aeronautics and astronautics – Aircraft power plants – Mounting
Reexamination Certificate
2006-03-07
2006-03-07
Barefoot, Galen (Department: 3644)
Aeronautics and astronautics
Aircraft power plants
Mounting
C060S226100, C060S796000, C248S555000, C244S055000
Reexamination Certificate
active
07007890
ABSTRACT:
The turbojet according to the invention is designed to be fixed onto the upper part of the aft section of the fuselage of an aircraft using at least one coat hanger, the turbojet comprising a fan, a forward casing, an aft casing, accessories arranged around the periphery of the forward casing, the forward casing comprising attachment points, for the coat hanger. The attachment points are arranged so that the turbojet can be installed indifferently on either side of the aircraft fuselage, accessories being arranged on the casing so that they are accessible from the outside of the fuselage regardless of which side the installation is done.
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patent: 2003/0102405 (2003-06-01), McEvoy
Beutin Bruno
Burdin Fabien
Mazeaud Georges
Yvon Didier
Barefoot Galen
Snecma Moteurs
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