Invention Grant
- Patent Title: Fastening of an exhaust cone in a turbomachine nozzle
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Application No.: US18251798Application Date: 2021-11-03
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Publication No.: US11959437B2Publication Date: 2024-04-16
- Inventor: Jean-Philippe Joret , Vincent Devanlay , Fabien Bravin , Thomas Vandellos
- Applicant: SAFRAN NACELLES , SAFRAN CERAMICS
- Applicant Address: FR Gonfreville-L'Orcher
- Assignee: SAFRAN NACELLES,SAFRAN CERAMICS
- Current Assignee: SAFRAN NACELLES,SAFRAN CERAMICS
- Current Assignee Address: FR Gonfreville-l'Orcher; FR Le Haillan
- Agency: CHRISTENSEN O'CONNOR JOHNSON KINDNESS PLLC
- Priority: FR 11379 2020.11.05
- International Application: PCT/FR2021/051935 2021.11.03
- International Announcement: WO2022/096821A 2022.05.12
- Date entered country: 2023-05-04
- Main IPC: F02K1/04
- IPC: F02K1/04 ; F02K1/80

Abstract:
An assembly for a turbomachine nozzle having a longitudinal axis (X) includes an exhaust cone with an annular outer wall for guiding a primary air flow and an annular chamber placed radially inside said annular outer wall. The annular chamber includes an annular inner wall placed radially inside the annular outer wall of the exhaust cone. An exhaust case is placed upstream of the ejection cone. A connecting member is interposed longitudinally between the exhaust case and the exhaust cone and fastened to the exhaust case and to the annular inner wall. The assembly further includes elastic means configured to deform radially and prestressed radially between the annular outer wall and the connecting member.
Public/Granted literature
- US20240003315A1 FASTENING OF AN EXHAUST CONE IN A TURBOMACHINE NOZZLE Public/Granted day:2024-01-04
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