Aircraft jet engine pylon suspension attachment

Details Aircraft jet engine pylon suspension attachment Aircraft jet engine pylon suspension attachment

2011-07-05

2011-07-05

Dinh, Tien (Department: 3644)

Aeronautics and astronautics

Aircraft power plants

Mounting

Reexamination Certificate

active

07971825

ABSTRACT:
The invention relates to a turbojet suspension pylon for an aircraft, the pylon being provided with a rigid structure (10) comprising a longitudinal central box (22). According to the invention, the rigid structure also comprises two lateral boxes (24a,24b) fixed to a forward part of said central box (22), the pylon also comprising a first (6a) and a second (6b) engine forward suspension designed to resist forces applied along the longitudinal direction (X) of the pylon, these first and second suspensions being arranged on the two lateral boxes respectively.

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U.S. Appl. No. 12/089,058, filed Apr. 3, 2008, Diochon, et al.

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