- 专利标题: Noise-reducing aircraft landing gear tow bar fitting
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申请号: US16893028申请日: 2020-06-04
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公开(公告)号: US11530051B2公开(公告)日: 2022-12-20
- 发明人: Navid Daneshvaran , Takao Suzuki , Nicholas J. Moffitt , Nicholas Toon , Michael Lewis McGillivray
- 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: Alleman Hall Creasman & Tuttle LLP
- 主分类号: B64F1/22
- IPC分类号: B64F1/22 ; B64C25/60
摘要:
A tow bar fitting for towing an aircraft is disclosed. The tow bar fitting includes a mount, a pin support, and a tow pin. The mount includes an upper attachment and a lower attachment for affixing the tow bar fitting to a landing gear of the aircraft. The pin support extends from the mount away from the landing gear. The tow pin is positioned in the pin support such that a tow pin plane that horizontally bisects the tow pin is lower than a mount plane that horizontally bisects the upper attachment and the lower attachment when the aircraft is right-side-up on the ground.
公开/授权文献
- US20210380276A1 NOISE-REDUCING AIRCRAFT LANDING GEAR TOW BAR FITTING 公开/授权日:2021-12-09
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