F - Mech Eng,Light,Heat,Weapons – 02 – C
Patent
F - Mech Eng,Light,Heat,Weapons
02
C
F02C 7/20 (2006.01) B64C 3/32 (2006.01) B64D 27/12 (2006.01) B64D 27/18 (2006.01) B64D 27/26 (2006.01)
Patent
CA 2487839
This invention relates to a structure (1) for mounting a turboprop (2) under an aircraft wing (4), comprising a rigid structure and means (10) of fastening the turboprop on the rigid structure. According to the invention, the rigid structure is composed of a box (8), and the mounting means comprise at least two lateral connecting rods (26) resisting the engine torque generated by the turboprop, the connecting rods (26) being arranged on each side of the box and each having a forward end (26a) connected to a gear box (24) of the turboprop (2), and an aft end (26b) connected to said box.
Cassagne Jerome
Chambreuil Arnaud
Del Blanco Anthony
Machado Stephane
Martin Yvon
Airbus France
Airbus Operations Sas
Goudreau Gage Dubuc
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