Invention Grant
- Patent Title: Blade pivot of adjustable orientation and of reduced bulk for a turbomachine fan hub
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Application No.: US17432682Application Date: 2020-01-31
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Publication No.: US11572889B2Publication Date: 2023-02-07
- Inventor: Vincent François Georges Millier , Caroline Marie Frantz , Gilles Alain Marie Charier , Olivier Belmonte
- 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: FR1901823 20190222
- International Application: PCT/FR2020/050164 WO 20200131
- International Announcement: WO2020/169896 WO 20200827
- Main IPC: F04D29/32
- IPC: F04D29/32 ; F01D7/00 ; F04D29/36 ; B64C11/06 ; B64C11/36

Abstract:
A blade pivot of adjustable orientation for a turbomachine fan hub includes: a block having a retaining device configured to retain a fan blade root and a coupling device for the transmission of a torque; a ball type rolling bearing for taking up centrifugal forces having an inner ring; a clamping nut screwed onto an external thread of the block in order to clamp the inner ring of the ball type rolling bearing for taking up centrifugal forces to the block; a rolling bearing for taking up transverse forces; a pitch setting transmission ring positioned inside the inner radial end of the block and equipped with a coupling device cooperating with the coupling device of the block, and a device for locking the pitch setting transmission ring on the block.
Public/Granted literature
- US20220018357A1 BLADE PIVOT OF ADJUSTABLE ORIENTATION AND OF REDUCED BULK FOR A TURBOMACHINE FAN HUB Public/Granted day:2022-01-20
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