Invention Grant
- Patent Title: Module of a turbomachine or of a combustion chamber test bench
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Application No.: US15778612Application Date: 2016-11-16
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Publication No.: US10914196B2Publication Date: 2021-02-09
- Inventor: Marc Bernard Blanrue , Jean-François Bernard Adnot
- Applicant: SAFRAN AIRCRAFT ENGINES
- Applicant Address: FR Paris
- Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee Address: FR Paris
- Agency: Christensen O'Connor Johnson Kindness PLLC
- Priority: FR1561444 20151127
- International Application: PCT/FR2016/052972 WO 20161116
- International Announcement: WO2017/089677 WO 20170601
- Main IPC: F01D25/24
- IPC: F01D25/24 ; F01D25/26

Abstract:
The present disclosure concerns an assembly of a turbomachine or of a combustion chamber test bench, generally including an annular outer housing, inside which a combustion chamber is housed, and a ferrule downstream from the housing. The ferrule may be attached to said housing by a connection comprising a radial flange rigidly connected to one of the housing and the ferrule, an annular groove being provided in the radial flange, and an axial tab rigidly connected to the ferrule or to the housing. The tab is generally housed in the groove, and the tab and the annular groove may be arranged relative to each other in such a way that, at assembly, they are in contact and centered relative to each another.
Public/Granted literature
- US20180291767A1 MODULE OF A TURBOMACHINE OR OF A COMBUSTION CHAMBER TEST BENCH Public/Granted day:2018-10-11
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