Engine assembly for aircraft

Details Engine assembly for aircraft Engine assembly for aircraft

2006-09-26

2011-10-18

Collins, Timothy D (Department: 3644)

Aeronautics and astronautics

Aircraft power plants

Mounting

Reexamination Certificate

active

08038092

ABSTRACT:
An aircraft engine assembly including a turbojet engine, an engine mount, and a plurality of engine attachments. The engine attachments include first and second forward attachments fixed to a fan case and located symmetrically in relation to a plane defined by a longitudinal axis of the turbojet engine and a vertical direction thereof, both forward attachments configured to transfer loads exerted in a longitudinal direction of the turbojet engine and in the vertical direction thereof. Moreover, each of the two forward attachments includes a shear pin mounted on the case and going through two walls of a clevis fixed on the engine mount.

REFERENCES:
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patent: 5746391 (1998-05-01), Rodgers et al.
patent: 7093996 (2006-08-01), Wallace et al.
patent: 7156343 (2007-01-01), Marche
patent: 2004/0108413 (2004-06-01), Thompson
U.S. Appl. No. 12/064,924, filed Feb. 26, 2008, Diochon, et al.

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