Aircraft engine assembly

Aeronautics and astronautics – Aircraft power plants – Mounting

Reexamination Certificate

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Details

C244S055000

Reexamination Certificate

active

07740200

ABSTRACT:
An engine assembly for aircraft including a turbojet, an attachment strut, and a plurality of engine mounts interposed between the attachment strut and the turbojet. Each of the engine mounts is attached to a fan casing of the turbojet.

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patent: 2 732 947 (1996-10-01), None
U.S. Appl. No. 11/914,327, filed Nov. 13, 2007, Diochon, et al.
U.S. Appl. No. 11/632,077, filed Jan. 10, 2007, Diochon, et al.
U.S. Appl. No. 11/572,003, filed Jan. 12, 2007, Diochon, et al.
U.S. Appl. No. 11/571,666, filed Jan. 5, 2007, Diochon, et al.

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