Suspension part of a turbojet engine

Details Suspension part of a turbojet engine Suspension part of a turbojet engine

2006-01-17

2006-01-17

King, Anita M. (Department: 3632)

Aeronautics and astronautics

Aircraft power plants

Mounting

C248S554000, C248S557000, C060S797000

Reexamination Certificate

active

06986482

ABSTRACT:
A suspension part for mounting a turbojet engine includes two ends equipped with two elements, juxtaposed in a widthwise direction of the suspension part, for fixing the suspension part to the fixed structure. The ends are shaped into pairs of yokes respectively flanking connecting rods and each including fixing elements and a bearing of a journal of a connecting rod which bearing is situated underneath a fixing element. The suspension part also includes slots passing through the two ends of the suspension part and running between the yokes without running over a central portion of the suspension part. Each of the yokes has an upper portion with an additional thickness located on an inside of each of the yokes.

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