GB646780A - - Google Patents

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Publication number
GB646780A
GB646780A GB646780DA GB646780A GB 646780 A GB646780 A GB 646780A GB 646780D A GB646780D A GB 646780DA GB 646780 A GB646780 A GB 646780A
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GB
United Kingdom
Prior art keywords
valve
pressure
flow
fuel
diaphragm
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English (en)
Publication of GB646780A publication Critical patent/GB646780A/en
Active legal-status Critical Current

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  • Feeding And Controlling Fuel (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
GB646780D Active GB646780A (enrdf_load_stackoverflow)

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ID=1749942

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Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2808702A (en) * 1951-03-13 1957-10-08 Garrett Corp Gas turbine pneumatic governor fuel supply control
US2841957A (en) * 1955-08-09 1958-07-08 Robert J Thorpe Automatic compressor pressure limiter
US2846846A (en) * 1951-06-14 1958-08-12 Bendix Aviat Corp Fuel system for gas turbine engines having means for avoiding compressor instability
US2849862A (en) * 1954-12-01 1958-09-02 Gen Motors Corp Air density fuel control for jet engine
US2873578A (en) * 1951-03-13 1959-02-17 Garrett Corp Fuel-air ratio control apparatus for gas driven prime movers
US2925710A (en) * 1956-02-23 1960-02-23 John C Gavin Variable area jet nozzle control
US2960826A (en) * 1954-12-06 1960-11-22 Curtiss Wright Corp Coordinated fuel and speed scheduling control for gas turbine engines
US2963859A (en) * 1955-10-26 1960-12-13 Gen Electric Turbojet fuel regulating system with temperature compensation for preventing compressor stall
US3062007A (en) * 1957-02-20 1962-11-06 Szydlowski Joseph Fuel feed system for turbojet engines
US3085397A (en) * 1957-08-01 1963-04-16 Rolls Royce Gas turbine engine fuel system
US3091925A (en) * 1958-06-11 1963-06-04 Rolls Royce Gas turbine engine fuel control with plural sleeve valves
US3105354A (en) * 1960-08-08 1963-10-01 Bendix Corp Fuel control for combustion engines
US3205655A (en) * 1957-10-07 1965-09-14 Chandler Evans Inc Afterburner fuel regulator responsive to compressor discharge absolute pressure

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2873578A (en) * 1951-03-13 1959-02-17 Garrett Corp Fuel-air ratio control apparatus for gas driven prime movers
US2808702A (en) * 1951-03-13 1957-10-08 Garrett Corp Gas turbine pneumatic governor fuel supply control
US2846846A (en) * 1951-06-14 1958-08-12 Bendix Aviat Corp Fuel system for gas turbine engines having means for avoiding compressor instability
US2849862A (en) * 1954-12-01 1958-09-02 Gen Motors Corp Air density fuel control for jet engine
US2960826A (en) * 1954-12-06 1960-11-22 Curtiss Wright Corp Coordinated fuel and speed scheduling control for gas turbine engines
US2841957A (en) * 1955-08-09 1958-07-08 Robert J Thorpe Automatic compressor pressure limiter
US2963859A (en) * 1955-10-26 1960-12-13 Gen Electric Turbojet fuel regulating system with temperature compensation for preventing compressor stall
US2925710A (en) * 1956-02-23 1960-02-23 John C Gavin Variable area jet nozzle control
US3062007A (en) * 1957-02-20 1962-11-06 Szydlowski Joseph Fuel feed system for turbojet engines
US3085397A (en) * 1957-08-01 1963-04-16 Rolls Royce Gas turbine engine fuel system
US3205655A (en) * 1957-10-07 1965-09-14 Chandler Evans Inc Afterburner fuel regulator responsive to compressor discharge absolute pressure
US3091925A (en) * 1958-06-11 1963-06-04 Rolls Royce Gas turbine engine fuel control with plural sleeve valves
US3105354A (en) * 1960-08-08 1963-10-01 Bendix Corp Fuel control for combustion engines

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