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Hydraulic distributor, especially for servo-control systems of aircraft and helicopters

  • US 4,335,745 A
  • Filed: 06/26/1980
  • Issued: 06/22/1982
  • Est. Priority Date: 07/03/1979
  • Status: Expired due to Term
First Claim
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1. A hydraulic distributor primarily intended to equip servo-control systems of aircraft and helicopters, comprising a plug rotatably mounted within a stationary sleeve housed within a casing and pierced by bores for admission of a hydraulic fluid under pressure and discharge of the fluid to the collector-tank, progressively-opening passages on the periphery of the rotary plug in order to ensure circulation of the hydraulic fluid from one bore of the sleeve to the next when the plug is caused to rotate, said hydraulic distributor comprising an annular element interposed between the sleeve and the rotary plug, said annular element being pierced by radial openings in the line of extension of the bores of the stationary sleeve, progressively-opening passages in the outer periphery of said annular element so as to permit progressive transfer of the hydraulic fluid from one bore of the stationary sleeve to the adjacent bore if said annular element is caused to rotate, and locking means for maintaining the annular element in a normally stationary position at the time of rotation of the plug and for permitting rotational displacement of the annular element by the plug in the event of seizure of this latter within said annular element in order that the circulation of the hydraulic fluid may then be permitted to circulate from one bore to another through the peripheral passages of said annular element.

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