ENGINE SUSPENSION ASSEMBLY IN MOUNTING SYSTEM INSTALLED BETWEEN MOUNTING PILLAR AND ENGINE OF AIRCRAFT Russian patent published in 2010 - IPC B64D27/26 

Abstract RU 2387583 C2

FIELD: transport.

SUBSTANCE: suspension assembly contains body (130), cross member (146) pivotally installed on it by means of pivot axis (144), and two tie-rods for accepting traction forces each one of which contains end connected with cross member. The body consists of the first metal fastener (132a) and the second metal fastener (132b) superimposed on first metal fastener. The axis (144) contains the first section (144a) and the second section (144b), while the first section is made as integral part of the first metal fastener and the second section is made as integral part of the second metal fastener. Additionally, metal fasteners (132a, 132b) together form thrust surface (166) made capable to limit turning of cross member (146).

EFFECT: higher safety and reduction of dimensions and mass of engine suspension assembly.

11 cl, 7 dwg

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RU 2 387 583 C2

Authors

Bofor Zhak

Djumon Zhan-Fransua

Dates

2010-04-27Published

2006-03-15Filed