Invention Grant
- Patent Title: Assembly for attaching a nozzle to a structural element of a turbine engine
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Application No.: US16314431Application Date: 2017-06-22
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Publication No.: US10526978B2Publication Date: 2020-01-07
- Inventor: Axel Sylvain Loïc Thomas , Maurice Guy Judet , Gabrijel Radeljak
- Applicant: SAFRAN AIRCRAFT ENGINES
- Applicant Address: FR Paris
- Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee Address: FR Paris
- Agency: Lathrop Gage LLP
- Priority: FR1656235 20160630
- International Application: PCT/FR2017/051655 WO 20170622
- International Announcement: WO2018/002480 WO 20180104
- Main IPC: F02C7/20
- IPC: F02C7/20 ; F02C9/16 ; F01D25/24
Abstract:
The present invention relates to an assembly (10) comprising: an annular nozzle (4) of a turbine of a turbine engine, a structural annular element (6) of the turbine engine, the nozzle (4) and the structural annular element (6) each comprising a radial flange (16, 18), the flanges being applied axially onto one another, and at least one member (12) for axially retaining the flange (16) of the nozzle (4) with the flange (18) of the structural annular element (6), with the member being applied to one of the flanges and being able to axially retain the two flanges one on top of the other.
Public/Granted literature
- US20190203649A1 ASSEMBLY FOR ATTACHING A NOZZLE TO A STRUCTURAL ELEMENT OF A TURBINE ENGINE Public/Granted day:2019-07-04
Information query
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