Mounting device for an aircraft engine comprising two thrust...

Details Mounting device for an aircraft engine comprising two thrust... Mounting device for an aircraft engine comprising two thrust...

2007-06-27

2009-10-27

Eldred, J. Woodrow (Department: 3641)

Aeronautics and astronautics

Aircraft power plants

Mounting

C248S554000, C060S797000

Reexamination Certificate

active

07607609

ABSTRACT:
A mounting device for an aircraft engine includes a rigid structure and a device for mounting the engine on the rigid structure, the mounting device including a thrust load recovery device with two lateral thrust load recovery rods each having a rear end mounted on a crossbar of the recovery device with a first mechanical connection. At the rear end of each of the two rods, there is also provided a second mechanical connection with play between the rear end and a support fitting integral with the rigid structure. The first mechanical connection is implemented using a pin provided on the crossbar, passing through an orifice provided in the rear end of the rod.

REFERENCES:
patent: 6494403 (2002-12-01), Jule et al.
patent: 6758438 (2004-07-01), Brefort et al.
patent: 7108224 (2006-09-01), Pasquer et al.
patent: 1 136 355 (2001-09-01), None
patent: 1 300 337 (2003-04-01), None
patent: 1 481 897 (2004-12-01), None

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