Invention Grant
- Patent Title: Device for limiting the loosening of a nut in a turbine engine
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Application No.: US15779584Application Date: 2016-12-01
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Publication No.: US11022241B2Publication Date: 2021-06-01
- Inventor: Mathieu Cladiere , Cedric Roger Zordan , Stephane Vergez
- Applicant: Safran Helicopter Engines
- Applicant Address: FR Bordes
- Assignee: Safran Helicopter Engines
- Current Assignee: Safran Helicopter Engines
- Current Assignee Address: FR Bordes
- Agency: Oblon, McClelland, Maier & Neustadt, L.L.P.
- Priority: FR1561809 20151203
- International Application: PCT/FR2016/053163 WO 20161201
- International Announcement: WO2017/093671 WO 20170608
- Main IPC: F16L19/00
- IPC: F16L19/00

Abstract:
An assembly for a turbine engine. The assembly includes a mount, a nut clamping around the male portion of the mount, a member projecting from the mount and a device for limiting loosening of the nut. The loosening limitation device includes a member for locking the nut against rotation relative to the mount. The rotation locking member includes an inner surface designed to limit rotation of the nut with shape engagement with an outer surface of the nut. The rotation locking member includes a first anti-rotation abutment designed to rotatably abut against the projecting member. The loosening limitation device includes a translation locking member designed to limit translation of the rotation locking member relative to the nut.
Public/Granted literature
- US20190271421A1 DEVICE FOR LIMITING THE LOOSENING OF A NUT IN A TURBINE ENGINE Public/Granted day:2019-09-05
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