IT948555B - Impianto alimentatore di combusti bile per motori a turbina a gas - Google Patents

Impianto alimentatore di combusti bile per motori a turbina a gas

Info

Publication number
IT948555B
IT948555B IT4826372A IT4826372A IT948555B IT 948555 B IT948555 B IT 948555B IT 4826372 A IT4826372 A IT 4826372A IT 4826372 A IT4826372 A IT 4826372A IT 948555 B IT948555 B IT 948555B
Authority
IT
Italy
Prior art keywords
gas turbine
supply system
fuel supply
turbine engines
engines
Prior art date
Application number
IT4826372A
Other languages
English (en)
Original Assignee
Lucas Industries 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 Lucas Industries Ltd filed Critical Lucas Industries Ltd
Application granted granted Critical
Publication of IT948555B publication Critical patent/IT948555B/it

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
    • F02C7/26—Starting; Ignition
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00—Fluid handling
    • Y10T137/2496—Self-proportioning or correlating systems
    • Y10T137/2559—Self-controlled branched flow systems
    • Y10T137/2574—Bypass or relief controlled by main line fluid condition
    • Y10T137/2579—Flow rate responsive

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fuel-Injection Apparatus (AREA)
  • High-Pressure Fuel Injection Pump Control (AREA)
  • Reciprocating Pumps (AREA)
IT4826372A 1971-02-15 1972-02-11 Impianto alimentatore di combusti bile per motori a turbina a gas IT948555B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB462471A GB1374813A (en) 1971-02-15 1971-02-15 Fuel supply systems for gas turbine engines

Publications (1)

Publication Number Publication Date
IT948555B true IT948555B (it) 1973-06-11

Family

ID=9780690

Family Applications (1)

Application Number Title Priority Date Filing Date
IT4826372A IT948555B (it) 1971-02-15 1972-02-11 Impianto alimentatore di combusti bile per motori a turbina a gas

Country Status (5)

Country Link
US (1) US3768249A (it)
JP (1) JPS5134927B1 (it)
FR (1) FR2125461B1 (it)
GB (1) GB1374813A (it)
IT (1) IT948555B (it)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1426281A (en) * 1973-02-15 1976-02-25 Plessey Co Ltd Devices for the metered supply of liquid fuel to combustion engines especially to aircraft gas-turbine engines
US3909159A (en) * 1973-03-05 1975-09-30 Garrett Corp Variable displacement pump for gas turbine fuel management system
GB1465476A (en) * 1973-07-18 1977-02-23 Lucas Industries Ltd Fuel control system for gas turbine engine
FR2238044B1 (it) * 1973-07-18 1976-12-24 Lucas Industries Ltd
US3930365A (en) * 1974-07-18 1976-01-06 Joseph Lucas (Industries) Limited Fuel control system for gas turbine engine
US4444008A (en) * 1981-03-04 1984-04-24 Rolls-Royce Limited Fuel control system for a gas turbine engine
US5062171A (en) * 1986-09-09 1991-11-05 Kinetic Concepts, Inc. Patient support air bags and related system with connectors for detachable mounting of the bags
GB2202904B (en) * 1987-03-23 1991-09-11 Rolls Royce Plc A method and apparatus for evaluating the working line characteristics of a compressor of a gas turbine engine
US4802334A (en) * 1987-10-05 1989-02-07 United Technologies Corporation Augmentor fuel system
US5694764A (en) * 1995-09-18 1997-12-09 Sundstrand Corporation Fuel pump assist for engine starting

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB624345A (en) * 1947-07-04 1949-06-02 David Havelock Ballantyne Improvements relating to fuel-and starting-systems for gas-turbine-engines
US2986881A (en) * 1958-04-23 1961-06-06 United Aircraft Corp Fuel accumulator for aircraft jet engine starter
US3078670A (en) * 1958-07-16 1963-02-26 Bmw Triebwerkbau Gmbh Fuel control system responsive to ambient conditions for combustion turbine power plants
US3151452A (en) * 1962-10-22 1964-10-06 Bendix Corp Electro-mechanical control for air breathing starter
US3282323A (en) * 1965-04-14 1966-11-01 Gen Electric Viscosity responsive devices
FR2040938A5 (it) * 1969-04-24 1971-01-22 Snecma
US3593736A (en) * 1969-05-19 1971-07-20 Chandler Evans Inc Slug pump and pressurizing valve for fuel control system

Also Published As

Publication number Publication date
GB1374813A (en) 1974-11-20
US3768249A (en) 1973-10-30
FR2125461B1 (it) 1974-08-02
DE2206716B2 (de) 1976-12-23
JPS5134927B1 (it) 1976-09-29
DE2206716A1 (de) 1972-08-24
FR2125461A1 (it) 1972-09-29

Similar Documents

Publication Publication Date Title
IT998522B (it) Apparato di combustione per motori a turbina a gas
IL33996A (en) Combustion chamber for a gas turbine engine
IT989653B (it) Camera di combustione per motori a turbina a gas
IT962232B (it) Paletta per l impiego in motori a turbina a gas
IT1060778B (it) Impianto di alimentazione di combustibile per un motore a turbina a gas
IT948122B (it) Impianto di regolazione di combu stibile in particolare per un mo tore a turbina a gas
IT948555B (it) Impianto alimentatore di combusti bile per motori a turbina a gas
IT1008488B (it) Impianto per regolare l alimentazio ne di combustibile in motori a turbina a gas
IT961051B (it) Apparecchiatura per nebulizzazione dei combustibile con sovralimenta zione d aria per un motore di tur bine a gas
IT961721B (it) Pompa di combustibile per motori a turbina a gas
IT982969B (it) Apparecchiatura di regolazione di combustibile per un impianto di postcombustione di un motore a turbina a gas
IT948358B (it) Regolatore di carburante parti colarmente per motori a turbina
IT982970B (it) Apparecchiatura di regolazione di combustibile per un impianto di postcombustione di un motore a turbina a gas
IT1002533B (it) Dispositivo di alimentazione di combustibile per un motore a turbina a gas
IT977086B (it) Dispositivo di alimentazione di combustibile per turbine a gas
IT956447B (it) Camera anulare di combustione per motori a turbina a gas
IT948121B (it) Impianto di regolazione di combusti bile in particolare per un motore a turbina a gas
IT1016434B (it) Regolatore di combustibile per motori a turbina a gas
IT1008747B (it) Apparecchio per la regolazione di carburante per motori a turbina
IT983725B (it) Reattore depuratore per gas di scarico di motori a combustione
IT942541B (it) Cappottatura per motori a turbina a gas
IT1047561B (it) Apparecchio per regolare l alimentazione di combustibile per motori a turbina a gas
IT948123B (it) Impianto di regolazione di com bustibile in particolare per un motore a turbina a gas
IT1013162B (it) Impianto di regolazione di combusti bile per un motore a turbina a gas
CH556511A (de) Brennkammer fuer eine gasturbine.