Invention Grant
- Patent Title: Aircraft engine intake arrangement comprising a mechanical decoupler
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Application No.: US16488858Application Date: 2018-02-28
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Publication No.: US11371432B2Publication Date: 2022-06-28
- Inventor: Serge Benyamin , Antoine Jean-Philippe Beaujard , Tewfik Boudebiza
- Applicant: SAFRAN AIRCRAFT ENGINES
- Applicant Address: FR Paris
- Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee Address: FR Paris
- Agency: Oblon, McClelland, Maier & Neustadt, L.L.P.
- Priority: FR1700201 20170228
- International Application: PCT/FR2018/050466 WO 20180228
- International Announcement: WO2018/158537 WO 20180907
- Main IPC: F02C7/04
- IPC: F02C7/04 ; F01D21/04 ; F01D25/16 ; F01D25/28 ; F02K3/06 ; F04D29/56 ; F23R3/04 ; F23R3/00

Abstract:
A mechanical decoupler (15) at the inlet to a turbomachine is positioned on the outside of an intake casing, where radiating arms (27) meet an external casing (13) so as to partially unload a low-pressure shaft when a significant out-of-balance appears. Because it is positioned a long way from the bearing, the decoupler (15) can be designed with a greater degree of freedom at a location where there is more space available and where layout constraints are less of an issue. More specifically, it is housed in a cavity (30) of the external casing (13) which opens onto the flow path (5).
Public/Granted literature
- US20190383216A1 AIRCRAFT ENGINE INTAKE ARRANGEMENT COMPRISING A MECHANICAL DECOUPLER Public/Granted day:2019-12-19
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