Turbojet engine mounting structure for aircraft

Details Turbojet engine mounting structure for aircraft Turbojet engine mounting structure for aircraft

2006-06-29

2011-12-06

Dinh, Tien (Department: 3644)

Aeronautics and astronautics

Aircraft power plants

Mounting

Reexamination Certificate

active

08070093

ABSTRACT:
A mount for an aircraft turbojet engine. The mount includes a central box formed by an assembly of two side panels joined via transverse ribs and two side boxes secured to a forward part of the box and arranged either side thereof, each side box including an aft closure frame. One of the ribs forming the box includes two side extensions made in a single piece with the rib and respectively projecting from the two side panels outwardly from the box, the two extensions being fixedly mounted on the frame of each of the two side boxes, respectively.

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patent: 1 053 937 (2000-11-01), None
U.S. Appl. No. 11/915,223, filed May 1, 2008, Diochon, et al.

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