Title:
SUSPENSION DEVICE OF AN AIRCRAFT TURBINE ENGINE
Document Type and Number:
WIPO Patent Application WO/2012/131233
Kind Code:
A3
Abstract:
The invention relates to a suspension device of a turbine engine casing, comprising a stepped shaft (26) that extends through aligned holes in two lugs (52, 54) of a clevis that is solidly connected to the casing. In addition, a wear-protection part (50) is mounted on each lug (52, 54) of the clevis and the stepped shaft (26) extends through said part. The wear-protection part (50) is rotatably fixed on the clevis (52, 54) in a form-fit manner.
Inventors:
DURAND DIDIER NOEL (FR)
EVAIN GAEL (FR)
LEUTARD FLORENCE IRENE NOELLE (FR)
MARTIN ARNAUD (FR)
EVAIN GAEL (FR)
LEUTARD FLORENCE IRENE NOELLE (FR)
MARTIN ARNAUD (FR)
Application Number:
PCT/FR2012/050589
Publication Date:
October 10, 2013
Filing Date:
March 21, 2012
Export Citation:
Assignee:
SNECMA (FR)
DURAND DIDIER NOEL (FR)
EVAIN GAEL (FR)
LEUTARD FLORENCE IRENE NOELLE (FR)
MARTIN ARNAUD (FR)
DURAND DIDIER NOEL (FR)
EVAIN GAEL (FR)
LEUTARD FLORENCE IRENE NOELLE (FR)
MARTIN ARNAUD (FR)
International Classes:
B64D27/26
Foreign References:
| US20080067286A1 | 2008-03-20 | |||
| EP0872418A2 | 1998-10-21 | |||
| US20050269445A1 | 2005-12-08 | |||
| EP0940337A1 | 1999-09-08 |
Attorney, Agent or Firm:
BARBE, Laurent (3 rue Auber, Paris, FR)
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