Invention Grant
- Patent Title: Speed reducer of a turbomachine
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Application No.: US17603655Application Date: 2020-04-17
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Publication No.: US11643975B2Publication Date: 2023-05-09
- Inventor: Julien Fabien Patrick Becoulet , Emmanuel Fabrice Marie Baret , Franck Emmanuel Bosco , Michel Gilbert Roland Brault , Paul Ghislain Albert Levisse
- Applicant: SAFRAN AIRCRAFT ENGINES
- Applicant Address: FR Paris
- Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee Address: FR Paris
- Agency: Christensen O'Connor Johnson Kindness PLLC
- Priority: FR 04224 2019.04.19
- International Application: PCT/FR2020/000136 2020.04.17
- International Announcement: WO2020/212666A 2020.10.22
- Date entered country: 2021-10-14
- Main IPC: F16H57/04
- IPC: F16H57/04 ; F02C7/36 ; F01D25/18 ; F02C7/06 ; F16H57/08

Abstract:
A speed reducer, particularly of an aircraft, includes a central sun gear mounted to rotate with a drive shaft about a rotation axis X, an annular ring gear coaxial with the X axis, and a plurality of planet gears arranged about the X axis and mounted to be movable on a planet carrier. The planet gears engages the sun gear and the annular ring gear, which extends around the planet gears. The speed reducer further includes a lubricant recovery device having a pipe for recovering lubricant discharged from the reducer by centrifuging. The recovery device has scoops mounted to pivot about a pivot axis P on a movable member of the speed reducer that rotates about the X axis between a deployed state and a rest state.
Public/Granted literature
- US20220235711A1 SPEED REDUCER OF A TURBOMACHINE Public/Granted day:2022-07-28
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