Aircraft engine rear mount with thrust links and...

Details Aircraft engine rear mount with thrust links and... Aircraft engine rear mount with thrust links and...

2006-04-04

2006-04-04

Carone, Michael (Department: 3641)

Aeronautics and astronautics

Aircraft power plants

Mounting

C248S554000, C060S796000, C060S797000

Reexamination Certificate

active

07021585

ABSTRACT:
A turbine engine mount to a pylon of an aircraft includes a bracket arranged to be attached to the pylon, and a lever attached in its central part to the bracket via a first connection and two thrust links each joined aft to the lever by a second connection. The lever includes a central part with two arms, and the bracket includes an integral attachment lug placed between the two arms and connected to the arms via a pivot pin to form the first connection. The lever is laterally connected to the bracket via pivot pins passing through the lever and mounted with a clearance to form connections on standby.

REFERENCES:
patent: 5320307 (1994-06-01), Spofford et al.
patent: 5725181 (1998-03-01), Hey
patent: 6059227 (2000-05-01), Le Blaye et al.
patent: 6494403 (2002-12-01), Jule et al.
patent: 6758438 (2004-07-01), Brefort et al.
patent: 0 564 126 (1993-10-01), None
patent: 0 879 759 (1998-11-01), None
patent: 1 136 355 (2001-09-01), None
patent: 2 830 515 (2001-10-01), None

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