F - Mech Eng,Light,Heat,Weapons – 02 – C
Patent
F - Mech Eng,Light,Heat,Weapons
02
C
F02C 7/20 (2006.01) B64D 27/20 (2006.01) B64D 27/26 (2006.01) B64D 29/00 (2006.01) F01D 25/28 (2006.01) F02C 7/32 (2006.01)
Patent
CA 2485242
The turbojet according to the invention is designed to be fixed onto the upper part of the aft section of the fuselage (1) of an aircraft using at least one davit ((28, 128), (28', 128')); the turbojet (10) comprising a fan, a forward casing, an aft casing, accessories (22, 23, 24, 25) arranged around the periphery of the forward casing, the forward casing comprising attachment points ((31, 32, 33), (31', 32', 38')), for the davit (28, 28'). The attachment points are arranged so that the turbojet (10) can be installed on either side of the aircraft fuselage (1) , accessories (22, 23. 24, 25) being arranged on the casing so that they are accessible from the outside of the fuselage (1) regardless of which side the installation is done.
Le turboréacteur de l'invention est destiné à être fixé sur la partie arrière du fuselage (1) d'un avion, en position supérieure, par le biais d'au moins un portemanteau ((28, 128), (28', 128')), le turboréacteur (10) comprenant une soufflante, un carter avant, un carter arrière, des accessoires (22, 23, 24, 25) disposés à la périphérie du carter avant, le carter avant comprenant des points ((31, 32, 33), (31', 32', 38')) de fixation du portemanteau (28, 28'). Les points de fixation sont disposés dé façon à permettre un montage du turboréacteur (10) indifféremment d'un côté ou de l'autre du fuselage (1), les accessoires (22, 23, 24, 25) étant disposés sur le carter de façon à être accessibles depuis (extérieur du fuselage (1) quel que doit le côté du montage.
Beutin Bruno
Burdin Fabien
Mazeaud Georges
Yvon Didier
Goudreau Gage Dubuc
Snecma
Snecma Moteurs
LandOfFree
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