发明授权
US07954769B2 Deployable aerodynamic devices with reduced actuator loads, and related systems and methods 有权
减少执行器负载的可部署空气动力装置,以及相关系统和方法

  • 专利标题: Deployable aerodynamic devices with reduced actuator loads, and related systems and methods
  • 专利标题(中): 减少执行器负载的可部署空气动力装置,以及相关系统和方法
  • 申请号: US11953672
    申请日: 2007-12-10
  • 公开(公告)号: US07954769B2
    公开(公告)日: 2011-06-07
  • 发明人: Glenn S. Bushnell
  • 申请人: Glenn S. Bushnell
  • 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: Perkins Coie LLP
  • 主分类号: B64C3/58
  • IPC分类号: B64C3/58 B64C9/00
Deployable aerodynamic devices with reduced actuator loads, and related systems and methods
摘要:
Deployable aerodynamic devices with reduced actuator loads, and related systems and methods are disclosed. An external flow system in accordance with a particular embodiment includes an external flow body, a deployable device carried by and movable relative to the external flow body, and a coupling connected between the external flow body and the deployable device. The system can further include an actuator device operatively coupled between the external flow body and the deployable device, with the actuator device positioned to move the deployable device along a motion path between a stowed position and the deployed position. The motion path can have a first portion over which the load delivered by the actuator device increases as the deployed device moves toward the deployed position, and a second portion over which the load delivered by the actuator device decreases as the deployed device moves toward the deployed position.
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