Method for fixing an engine strut to an airplane wing

Aeronautics and astronautics – Aircraft power plants – Mounting

Reexamination Certificate

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Reexamination Certificate

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07963479

ABSTRACT:
The inventive fixing system comprises a front attachment (6), a rear attachment (7) and an intermediate attachment (8) connecting a strut (1) to a wing (2), wherein the lower fitting (17) of the rear attachment (7) is fixedly connected to the transversal rear face (1G) of said strut on the extension thereof and said lower fitting (17) is substantially in flush with the top face of the strut.

REFERENCES:
patent: 4213585 (1980-07-01), Murphy
patent: 5806792 (1998-09-01), Brossier et al.
patent: 2004/0129832 (2004-07-01), Marche
patent: 2005/0082423 (2005-04-01), Whitmer et al.
patent: 2698068 (1994-05-01), None
patent: 1099538 (1996-10-01), None
XP-002335277 Derwent Abstract for foreign patent SU 1099538 A1, 1997.
PCT International Search Report dated Mar. 15, 2006.

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