GB983831A - Improved liquid pressure supply system - Google Patents

Improved liquid pressure supply system

Info

Publication number
GB983831A
GB983831A GB2105560A GB2105560A GB983831A GB 983831 A GB983831 A GB 983831A GB 2105560 A GB2105560 A GB 2105560A GB 2105560 A GB2105560 A GB 2105560A GB 983831 A GB983831 A GB 983831A
Authority
GB
United Kingdom
Prior art keywords
valve
servo
piston
conduit
pump
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
GB2105560A
Inventor
Stanley Ralph Tyler
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Dowty Fuel Systems Ltd
Original Assignee
Dowty Fuel Systems Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Dowty Fuel Systems Ltd filed Critical Dowty Fuel Systems Ltd
Priority to GB2105560A priority Critical patent/GB983831A/en
Publication of GB983831A publication Critical patent/GB983831A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D15/00Control, e.g. regulation, of pumps, pumping installations or systems
    • F04D15/0027Varying behaviour or the very pump
    • F04D15/0038Varying behaviour or the very pump by varying the effective cross-sectional area of flow through the rotor

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Jet Pumps And Other Pumps (AREA)

Abstract

983,831. Centrifugal pumps; gas turbine jet propulsion plant. DOWTY FUEL SYSTEMS Ltd. June 6, 1961 [June 15, 1960(2)], Nos. 21055/60 and 21056/60. Headings F1C and F1J. [Also in Division G3] A centrifugal pump 3 supplies fuel through a conduit 9, a metering orifice 43 and a port 47 to the afterburners of an aircraft gas turbine engine and its delivery is controlled by an inlet valve 7 actuated by a servo-piston 12 under the control of a valve 21 which is actuated by a diaphragm 26 subject to the pressure difference across the metering orifice so that the pressure difference is maintained constant. The degree of opening of the metering orifice is determined by a servo-piston 48 under the control of a valve 54 subject to the action of a feedback spring 58 and gas pressures in the engine applied to bellows 56, 57. Alternatively the valve 54 may be manually operated. To stop the flow of afterburning fuel an electrically operated pilot's control valve 69 is closed to cause depression of a servopiston 64 which interrupts communication between conduits 39, 41 and vents the conduit 41 and pump inlet to a port 73, thereby causing a second pump inlet valve 34 to be closed by a spring 38. The servo-piston 64 also vents the delivery conduit 9 of the pump through passages 61, 77, 79.
GB2105560A 1960-06-15 1960-06-15 Improved liquid pressure supply system Expired GB983831A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2105560A GB983831A (en) 1960-06-15 1960-06-15 Improved liquid pressure supply system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2105560A GB983831A (en) 1960-06-15 1960-06-15 Improved liquid pressure supply system

Publications (1)

Publication Number Publication Date
GB983831A true GB983831A (en) 1965-02-17

Family

ID=10156437

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2105560A Expired GB983831A (en) 1960-06-15 1960-06-15 Improved liquid pressure supply system

Country Status (1)

Country Link
GB (1) GB983831A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2011098126A1 (en) * 2010-02-11 2011-08-18 Pierburg Pump Technology Gmbh Mechanical coolant pump
ITBS20110150A1 (en) * 2011-10-27 2013-04-28 Ind Saleri Italo Spa ADJUSTABLE COOLING PUMP FOR INTERNAL COMBUSTION ENGINE
ITBS20130100A1 (en) * 2013-07-09 2015-01-10 Ind Saleri Italo Spa ADJUSTABLE COOLING PUMP FOR INTERNAL COMBUSTION ENGINE

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2011098126A1 (en) * 2010-02-11 2011-08-18 Pierburg Pump Technology Gmbh Mechanical coolant pump
CN102792029A (en) * 2010-02-11 2012-11-21 皮尔伯格泵技术有限责任公司 Mechanical coolant pump
US8967982B2 (en) 2010-02-11 2015-03-03 Pierburg Pump Technology Gmbh Mechanical coolant pump
CN102792029B (en) * 2010-02-11 2015-10-21 皮尔伯格泵技术有限责任公司 Mechanical type coolant pump
ITBS20110150A1 (en) * 2011-10-27 2013-04-28 Ind Saleri Italo Spa ADJUSTABLE COOLING PUMP FOR INTERNAL COMBUSTION ENGINE
ITBS20130100A1 (en) * 2013-07-09 2015-01-10 Ind Saleri Italo Spa ADJUSTABLE COOLING PUMP FOR INTERNAL COMBUSTION ENGINE
WO2015004548A1 (en) * 2013-07-09 2015-01-15 Industrie Saleri Italo S.P.A. Adjustable cooling pump for internal combustion engine
CN105408633A (en) * 2013-07-09 2016-03-16 萨乐锐伊塔洛工业有限公司 Adjustable cooling pump for internal combustion engine

Similar Documents

Publication Publication Date Title
GB1032511A (en) Improvements in or relating to engine crankcase ventilating systems
GB1161574A (en) Improvements in Fuel Delivery Systems for Gas Turbine Engines
GB1369653A (en) Fuel control system for gas turbine engine
GB983831A (en) Improved liquid pressure supply system
GB1032767A (en) Improvements in or relating to control systems for liquid-fuel supply for engines
GB1036403A (en) Improvements in tachometric carburettors for internal combustion engines
GB730647A (en) Means for supplying liquid fuel to prime movers of the jet propulsion and gas turbine types
GB696452A (en) Improvements in fuel supply systems for gas turbine engines
GB758679A (en) Improvements in or relating to fuel systems for aviation gas turbine power plants
GB1369652A (en) Fuel control system for gas turbine engine
GB1464369A (en) Hydraulic systems
GB773148A (en) Improvements relating to fuel systems for gas turbine engine installations
GB731524A (en) Liquid fuel control system for aircraft jet-propulsion plant
ES396983A1 (en) Fuel supply systems for gas turbine engines
GB1022446A (en) Liquid supply system
GB802923A (en) Improvements in or relating to fuel supply systems for gas turbine engines
GB644212A (en) Improvements in or relating to gas turbine fuel systems
GB762194A (en) Improvements in apparatus for feeding liquid fuel to the burners of continuous combustion turbine engines
GB734301A (en) Contact carriers for electric switches
GB1198982A (en) Fuel Systems for Gas Turbine Engines
GB902523A (en) Improvements in fuel flow proportioners
GB1254612A (en) An improved fuel control system for a gas turbine engine
GB887780A (en) Improvements in or relating to fuel control systems for internal combustion engines
GB654256A (en) Improvements in liquid fuel supply systems
GB638325A (en) Improvements in and relating to hydraulic governors