- 专利标题: PITCH CHANGE MECHANISM COMPRISING AN IMPROVED ELECTROHYDRAULIC ACTUATOR
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申请号: US18564493申请日: 2022-05-23
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公开(公告)号: US20240239474A1公开(公告)日: 2024-07-18
- 发明人: Huguette DE WERGIFOSSE
- 申请人: Safran Aircraft Engines
- 申请人地址: FR PARIS
- 专利权人: Safran Aircraft Engines
- 当前专利权人: Safran Aircraft Engines
- 当前专利权人地址: FR PARIS
- 优先权: FR 05562 2021.05.28
- 国际申请: PCT/FR2022/050971 2022.05.23
- 进入国家日期: 2023-11-27
- 主分类号: B64C11/38
- IPC分类号: B64C11/38 ; B64C11/44 ; F01D7/00
摘要:
The present invention relates to a pitch change mechanism for a turbine engine propeller (10) comprising: — an electric machine (29) fixedly mounted on a stator portion of the turbine engine and comprising an actuator shaft (21); — an axial piston hydraulic pump (20) suitable for pressurising a hydraulic fluid, the hydraulic pump comprising a body (22) driven by the propeller (10); a barrel (23) housing a set of pistons (24) each comprising a sliding block (25); and a plate (26) that is tilted with respect to the axis of rotation, each sliding block bearing on the plate, one of the plate (26) and the barrel (23) being fixedly connected to the stator portion of the turbine engine and the other of the plate (26) and the barrel (23) being fixed to the actuator shaft (21) for conjoint rotation.
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