Turbojet designed to be fixed onto the AFT part of the...

Aeronautics and astronautics – Aircraft power plants – Mounting

Reexamination Certificate

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Details

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.

REFERENCES:
patent: 2863620 (1958-12-01), Vautier
patent: 3543588 (1970-12-01), Richardson
patent: 3714779 (1973-02-01), Stein et al.
patent: 3735946 (1973-05-01), Mullins
patent: 3809340 (1974-05-01), Dolgy et al.
patent: 4044973 (1977-08-01), Moorehead
patent: 4585189 (1986-04-01), Buxton
patent: 5443229 (1995-08-01), O'Brien et al.
patent: 6357220 (2002-03-01), Snyder et al.
patent: 6401448 (2002-06-01), Manteiga et al.
patent: 2003/0102405 (2003-06-01), McEvoy

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