Control valve of aircraft carrier ejector

Control valve of aircraft carrier ejector

  • CN 105,314,123 A
  • Filed: 06/20/2014
  • Published: 02/10/2016
  • Est. Priority Date: 06/20/2014
  • Status: Active Application
First Claim
Patent Images

1. a control cock, it is characterized in that given two annular grooves of plungers valve core or the twice annular groove of half moon breach spacing, width and the degree of depth or half moon breach move axially control given position and internal diameter each relevant gas port connection, short circuit and opening and closing, realize pressurizeing to the classification of control cylinder.

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