发明授权
US07494094B2 Aircraft wing systems for providing differential motion to deployable lift devices
有权
飞机机翼系统,用于为可部署升降机提供差速运动
- 专利标题: Aircraft wing systems for providing differential motion to deployable lift devices
- 专利标题(中): 飞机机翼系统,用于为可部署升降机提供差速运动
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申请号: US10935846申请日: 2004-09-08
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公开(公告)号: US07494094B2公开(公告)日: 2009-02-24
- 发明人: Mark S. Good , Paul M. Viigen , Seth E. Gitnes , Glynn Michael Thomas
- 申请人: Mark S. Good , Paul M. Viigen , Seth E. Gitnes , Glynn Michael Thomas
- 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: B64C3/50
- IPC分类号: B64C3/50 ; B64C9/00
摘要:
Systems and methods for providing differential motion to wing high lift devices are disclosed. A system in accordance with one embodiment of the invention includes a wing having a leading edge, a trailing edge, a first deployable lift device with a first spanwise location, and a second deployable lift device with a second spanwise location different than the first. The wing system can further include a drive system having a drive link operatively coupleable to both the first and second deployable lift devices, and a control system operatively coupled to the drive system. The control system can have a first configuration for which the drive link is operatively coupled to the first and second deployable lift devices, and activation of at least a portion of the drive link moves the first and second deployable lift devices together. In a second configuration, the drive link is operatively coupled to at least the first deployable lift device and operatively decoupled from the second deployable lift device, so that actuation of at least a portion of the drive link moves the first deployable lift device relative to the second deployable lift device.
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