发明授权
- 专利标题: Aircraft shock strut having a fluid level monitor
- 专利标题(中): 飞机冲击支柱具有液位监视器
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申请号: US13963705申请日: 2013-08-09
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公开(公告)号: US08919182B2公开(公告)日: 2014-12-30
- 发明人: William E. Luce
- 申请人: Goodrich Corporation
- 申请人地址: US NC Charlotte
- 专利权人: Goodrich Corporation
- 当前专利权人: Goodrich Corporation
- 当前专利权人地址: US NC Charlotte
- 代理机构: Snell & Wilmer L.L.P.
- 主分类号: G01F25/00
- IPC分类号: G01F25/00 ; B64C25/60 ; G01F23/292 ; G01M3/32 ; G01M11/00
摘要:
A system for monitoring a liquid level in an aircraft shock strut includes a cylinder having an internal chamber sealed by a piston telescopically movable within the cylinder. The chamber contains a gas and a liquid, and a sensor assembly is provided for monitoring a condition of a level of the liquid in the chamber. The sensor assembly includes at least one probe within the chamber, and a fitting assembly allows one or more leads from the probe to pass through the wall of the strut while maintaining pressure in the chamber. The fitting assembly includes a plug molded to the one or more leads extending from the probe. The fitting assembly also includes a retainer for holding the plug in sealed relationship with a through passage in the strut.
公开/授权文献
- US20130342828A1 AIRCRAFT SHOCK STRUT HAVING A FLUID LEVEL MONITOR 公开/授权日:2013-12-26
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