- 专利标题: Flap actuator mechanism
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申请号: US16573417申请日: 2019-09-17
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公开(公告)号: US11091248B2公开(公告)日: 2021-08-17
- 发明人: Kevin R. Tsai
- 申请人: THE BOEING COMPANY
- 申请人地址: US IL Chicago
- 专利权人: THE BOEING COMPANY
- 当前专利权人: THE BOEING COMPANY
- 当前专利权人地址: US IL Chicago
- 代理机构: Armstrong Teasdale LLP
- 主分类号: B64C13/28
- IPC分类号: B64C13/28 ; B64C3/28 ; B64C9/04
摘要:
An actuator mechanism for a flap includes a first link having a rotary-driven end and a free end, and a second link having a forward end, a mid-portion, and an aft end. The rotary-driven end is pivotally connected to a base structure, the forward end is pivotally connected to the free end, and the aft end is connected to the flap. The actuator mechanism also includes a third link that includes a fixed end, an intermediate connector, and an end connector. The fixed end is pivotally connected to the base structure, and the intermediate connector is pivotally connected to the mid-portion of the second link. The actuator mechanism further includes a flap link including a first end pivotally connected to the end connector, and a second end pivotally connected to the flap. Rotation of the first link causes the flap to transition from a stowed to a fully deployed position.
公开/授权文献
- US20210078694A1 FLAP ACTUATOR MECHANISM 公开/授权日:2021-03-18
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