Invention Grant
- Patent Title: Stator support for a fan shaft driven by a reduction gearbox in a turbomachine
-
Application No.: US18029783Application Date: 2021-09-24
-
Publication No.: US11946381B2Publication Date: 2024-04-02
- Inventor: Christophe Marcel Lucien Perdrigeon , Didier Gabriel Bertrand Desombre , Régis Eugène Henri Servant
- Applicant: Safran Aircraft Engines
- Applicant Address: FR Paris
- Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee Address: FR Paris
- Agency: BIRCH, STEWART, KOLASCH & BIRCH, LLP
- Priority: FR 10071 2020.10.01
- International Application: PCT/FR2021/051656 2021.09.24
- International Announcement: WO2022/069824A 2022.04.07
- Date entered country: 2023-03-31
- Main IPC: F01D25/18
- IPC: F01D25/18 ; F02C7/06 ; F02C7/36

Abstract:
Stator structure (22) extending around an axis of the turbomachine and comprising: —a support (50) having an inner surface centred on the axis and—a flange (60) defining an air chamber (A2) and having an outer surface centred on the axis, the support (50) extending around the flange (60) such that the inner and outer surfaces are opposite to each other, the structure (22) defining an oil circuit and an air circuit which are formed by upstream channels (64, 65) and downstream channels (54, 55), —each upstream channel (64, 65) defining an outer opening in the outer surface, —each downstream channel (54, 55) defining an inner opening in the inner surface, each circuit being oriented between the outer and inner openings in a direction comprising a component radial to the axis.
Public/Granted literature
- US20230407763A1 STATOR SUPPORT FOR A FAN SHAFT DRIVEN BY A REDUCTION GEARBOX IN A TURBOMACHINE Public/Granted day:2023-12-21
Information query