Engine assembly for aircraft

Aeronautics and astronautics – Aircraft power plants – Mounting

Reexamination Certificate

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C248S554000

Reexamination Certificate

active

07445179

ABSTRACT:
The invention relates to an engine suspension pylon for an aircraft including a rigid structure provided with a box (24), this pylon also including an engine aft attachment (8) provided with an attachment body (38), and a thrust resistance device (9) generated by the engine. The rigid structure according to the invention includes an offset rib (35) for the attachment body (38), this rib (35) being mounted fixed on the box (24) between the box and the engine (2) and carrying the attachment body. Furthermore, the device (9) includes a thrust resistance spar (9b) of which the forward end is mounted fixed on the rib (35), and the aft end is mounted fixed on the box.

REFERENCES:
patent: 2007/0069069 (2007-03-01), Diochon et al.
patent: 0 147 878 (1985-07-01), None
patent: 2 676 707 (1992-11-01), None
patent: 2 010 969 (1979-07-01), None
U.S. Appl. No. 12/067,192, filed Mar. 18, 2008, Lafont, et al.
U.S. Appl. No. 12/066,916, filed Mar. 14, 2008, Lafont.

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