Engine suspension pylon for aircraft

Aeronautics and astronautics – Aircraft power plants – Mounting

Reexamination Certificate

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C248S554000

Reexamination Certificate

active

07448573

ABSTRACT:
The invention refers to a suspension pylon (4) for an aircraft engine (2), the pylon including a rigid structure (10) forming a box provided with a lower spar (28) and an upper spar (26), and an engine mounting system (11) installed fixed on the structure (10) and in particular including a forward attachment (6) with an attachment body provided with a horizontal fixing surface (40) held in contact with a horizontal fixing surface (38) of the structure (10). According to the invention, the attachment body is arranged such that its horizontal fixing surface (40) is located along a vertical direction (Z) of the pylon, upwards from a forward end (28a) of the lower spar and downwards from a forward end (26a) of the upper spar. Furthermore, the structure (10) includes at least one forward fitting (42a,42b) making up a forward closing rib (36) of the box, this fitting (42a,42b) defining said horizontal fixing surface (38).

REFERENCES:
patent: 4013246 (1977-03-01), Nightingale
patent: 4132069 (1979-01-01), Adamson et al.
patent: 2007/0069068 (2007-03-01), Lafont et al.
patent: 0 583 158 (1994-02-01), None
patent: 0 805 108 (1997-11-01), None
patent: 1 053 937 (2000-11-01), None
patent: 1 574 429 (2005-09-01), 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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