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HYDRAULIC/PNEUMATIC CHARGING VALVE WITH INTEGRATED PRESSURE TRANSDUCER

  • US 20090293624A1
  • Filed: 08/24/2007
  • Published: 12/03/2009
  • Est. Priority Date: 08/30/2006
  • Status: Active Grant
First Claim
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1. A charging valve for use in a pressure vessel in an aircraft landing gear comprising:

  • a valve stem having a first and second end and a channel extending therebetween;

    a pressure-sensing device received within the channel at the first end and operable to measure the pressure of the pressure vessel; and

    a receptacle received within the channel between the pressure-sensing device and the second end and operable to be in communication with the pressure-sensing device and configured to allow fluid to flow through the valve.

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