Aeronautics and astronautics – Aircraft power plants – Mounting
Reexamination Certificate
2006-09-22
2008-11-11
Collins, Timothy D (Department: 3643)
Aeronautics and astronautics
Aircraft power plants
Mounting
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:
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patent: 4132069 (1979-01-01), Adamson et al.
patent: 2007/0069068 (2007-03-01), Lafont et al.
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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.
Journade Frederic
Labarthe Christophe
Lafont Laurent
Airbus France
Collins Timothy D
Oblon & Spivak, McClelland, Maier & Neustadt P.C.
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