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Gas turbine fuel control including timing device for scheduling acceleration

  • US 3,075,350 A
  • Filed: 12/19/1958
  • Issued: 01/29/1963
  • Est. Priority Date: 12/19/1958
  • Status: Expired due to Term
First Claim
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1. A FUEL CONTROL FOR AN ENGINE HAVING A COMPRESSOR INCLUDING A FUEL CONDUIT TO SAID ENGINE, A METERING VALVE IN SAID CONDUIT, A BYPASS VALVE FOR CONTROLLING THE PRESSURE DROP ACROSS SAID METERING VALVE, A MULTIPLYING DEVICE OPERATIVELY CONNECTED TO SAID METERING VALVE, AN ALL-SPEED GOVERNOR INCLUDING A GOVERNOR SPRING OPERABLY CONNECTED TO SAID MULTIPLYING DEVICE, MEANS RESPONSIVE TO A COMPRESSOR GENERATED PRESSURE OPERATIVELY CONNECTED TO SAID MULTIPLYING DEVICE, A CYLINDER, A PISTON IN SAID CYLINDER, MEANS MOVABLE IN RESPONSE TO MOVEMENT OF SAID PISTON FOR VARYING THE EFFECTIVE FORCE OF SAID GOVERNOR SPRING, A PILOT VALVE CONNECTED TO SAID CYLINDER AND OPERATIVE WHEN IN A FIRST POSITION TO PROVIDE COMMUNICATION BETWEEN SAID CYLINDER AND A SOURCE OF HIGH PRESSURE FUEL UPSTREAM OF SAID METERING VALVE, WHEN IN A SECOND POSITION TO PROVIDE COMMUNICATION BETWEEN SAID CYLINDER AND A PASSAGE COMMUNICATING WITH A LOW FLUID PRESSURE SOURCE, AND WHEN IN A THIRD POSITION TO BLOCK COMMUNICATION BETWEEN SAID CYLINDER AND SAID SOURCES, OPERATOR OPERATED MEANS FOR CAUSING SAID PILOT VALVE TO ASSUME EITHER OF SAID FIRST OR SECOND POSITIONS AND FOLLOW-UP MEANS RESPONSIVE TO MOVEMENT OF SAID PISTON TO CAUSE SAID PILOT VALVE TO SEEK SAID THIRD POSITION, A TIMING BLEED IN SAID PASSAGE, MEANS CONTINUOUSLY RESPONSIVE TO A VARIABLE INPUT SIGNAL INDICATIVE OF A DESIRED SCHEDULE OF ENGINE OPERATION OPERATIVELY CONNECTED TO SAID TIMING BLEED FOR VARYING THE EFFECTIVE AREA THEREOF AS A FUNCTION OF SAID VARIABLE INPUT SIGNAL DURING OPERATION OF THE ENGINE AND REGULATING MEANS FOR MAINTAINING A DESIRED PRESSURE DROP ACROSS SAID BLEED.

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