GB749540A - Improvements in and relating to temperature responsive modulating valves - Google Patents

Improvements in and relating to temperature responsive modulating valves

Info

Publication number
GB749540A
GB749540A GB28325/53A GB2832553A GB749540A GB 749540 A GB749540 A GB 749540A GB 28325/53 A GB28325/53 A GB 28325/53A GB 2832553 A GB2832553 A GB 2832553A GB 749540 A GB749540 A GB 749540A
Authority
GB
United Kingdom
Prior art keywords
temperature
tubular element
spill
oct
combustion chamber
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
GB28325/53A
Inventor
John Oliver Philip Hughes
Roy Starmer
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.)
English Electric Co Ltd
Original Assignee
English Electric Co 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 English Electric Co Ltd filed Critical English Electric Co Ltd
Priority to GB28325/53A priority Critical patent/GB749540A/en
Publication of GB749540A publication Critical patent/GB749540A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/22—Fuel supply systems
    • F02C7/232—Fuel valves; Draining valves or systems
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00—Control
    • F05D2270/30—Control parameters, e.g. input parameters
    • F05D2270/301—Pressure
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00—Control
    • F05D2270/30—Control parameters, e.g. input parameters
    • F05D2270/303—Temperature

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Feeding And Controlling Fuel (AREA)
  • Supercharger (AREA)

Abstract

749,540. Gas turbine plant. ENGLISH ELECTRIC CO., Ltd. Oct. 8, 1954 [Oct. 14, 1953], No. 28325/53. Class 110(3) [Also in Group XXIX] A valve suitable for controlling a spill passage from the fuel supply to a gas turbine engine comprises a valve member 5 with an annular knife-edge co-acting with a tapered, tubular element 4 and carried by the free end of a Bourdon tube 7 whose interior is connected by a capillary tubing 10 to a mercury boiler which is exposed to the temperature at the inlet to the turbine. Up to a temperature of 300‹C. the mercury pressure is negligible and the spill flow is constant. From that temperature up to 760"C. the valve member is moved towards the smaller end of the tubular element 4 resulting in a progressively decreasing spill flow Any further increase of temperature causes the knife-edge to emerge from the tubular element and so rapidly to increase the spill flow. Englines having more than one combustion chamber may have a corresponding number of valve members arranged in parallel each controlled by a Bourdon tube sensitive to the temperature at the outlet of the respective combustion chamber.
GB28325/53A 1953-10-14 1953-10-14 Improvements in and relating to temperature responsive modulating valves Expired GB749540A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB28325/53A GB749540A (en) 1953-10-14 1953-10-14 Improvements in and relating to temperature responsive modulating valves

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB28325/53A GB749540A (en) 1953-10-14 1953-10-14 Improvements in and relating to temperature responsive modulating valves

Publications (1)

Publication Number Publication Date
GB749540A true GB749540A (en) 1956-05-30

Family

ID=10273884

Family Applications (1)

Application Number Title Priority Date Filing Date
GB28325/53A Expired GB749540A (en) 1953-10-14 1953-10-14 Improvements in and relating to temperature responsive modulating valves

Country Status (1)

Country Link
GB (1) GB749540A (en)

Similar Documents

Publication Publication Date Title
ES471533A1 (en) Valve control arrangements
US2861420A (en) Fuel regulator
GB749540A (en) Improvements in and relating to temperature responsive modulating valves
GB2014758A (en) Fuel control for a gas turbine engine reheat system
GB2014238A (en) Fuel Injection System for a Mixture Compressing I.C. Engine
US3029601A (en) Air mass flow computer
GB785803A (en) Arrangement for regulating the flow of after-burning fuel in jet propulsion engines having a two stage combustion system
US3327757A (en) Fuel control
GB781758A (en) Improvements in liquid fuel supply systems for gas turbine engines
GB831982A (en) Starting control for gas turbine engines
GB791062A (en) Improvements in or relating to gas turbine engine power plants
GB760406A (en) Liquid fuel burners
GB1066670A (en) Fuel control apparatus for a gas turbine engine
US3327756A (en) Fuel control
SU138690A1 (en) Odorant Automatic Dispenser
GB1037324A (en) Improved protective control system for gas turbine plant
GB776345A (en) Improvements in or relating to engine control arrangements
GB804702A (en) Improvements in a fuel flow control for engines
GB697137A (en) Improvements in gas turbine installations
GB496305A (en) Improvements in or relating to thermostatically-controlled gas-valves
GB969481A (en) Means for limiting the temperature of the jet pipe of a jet engine or gas turbine
GB837957A (en) Improvements in or relating to burners
GB749783A (en) Liquid fuel regulating means for prime movers
GB798472A (en) Improved method and apparatus for the flow control of fluids
GB850255A (en) Improvements in fluid flow valves