Invention Grant
- Patent Title: Shock absorber assembly for hydraulically and electrically connecting an unducted fan
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Application No.: US15761327Application Date: 2016-09-20
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Publication No.: US10221772B2Publication Date: 2019-03-05
- Inventor: Laurent Cedric Zamai , Matthieu Etienne Joachim Palis
- Applicant: SAFRAN AIRCRAFT ENGINES
- Applicant Address: FR Paris
- Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee Address: FR Paris
- Agency: Pillsbury Winthrop Shaw Pittman LLP
- Priority: FR1558881 20150921
- International Application: PCT/FR2016/052381 WO 20160920
- International Announcement: WO2017/051111 WO 20170330
- Main IPC: F16M13/00
- IPC: F16M13/00 ; F02C7/36 ; B64C11/44 ; B64C11/48 ; F01D25/04 ; F01D25/28 ; B64D27/00 ; B64C11/38 ; B64D27/10

Abstract:
A shock absorber assembly for a non-streamlined blower includes an extension collar having a first interface suitable for being rigidly attached on a first module of the blower; a connector support housing including a third interface suitable for being rigidly attached on a second module of the blower; and a fourth interface allowing a mechanical connection to be made between the housing and a second interface of the collar; a plurality of elastic devices arranged between the collar and the housing; a flange element rigidly attached on the third interface of the housing comprising a stop bearing on the collar in such a way as to define a space between the collar and the flange element; the elastic means are arranged so that a residual clearance exists between the flange element and the housing.
Public/Granted literature
- US20180274450A1 SHOCK ABSORBER ASSEMBLY FOR HYDRAULICALLY AND ELECTRICALLY CONNECTING AN UNDUCTED FAN Public/Granted day:2018-09-27
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