IT8120586A0 - Apparato e metodo per migliorare il rendimento del carburante di un turbomotore a gas. - Google Patents

Apparato e metodo per migliorare il rendimento del carburante di un turbomotore a gas.

Info

Publication number
IT8120586A0
IT8120586A0 IT8120586A IT2058681A IT8120586A0 IT 8120586 A0 IT8120586 A0 IT 8120586A0 IT 8120586 A IT8120586 A IT 8120586A IT 2058681 A IT2058681 A IT 2058681A IT 8120586 A0 IT8120586 A0 IT 8120586A0
Authority
IT
Italy
Prior art keywords
improving
turbo engine
gas turbo
fuel performance
fuel
Prior art date
Application number
IT8120586A
Other languages
English (en)
Other versions
IT1139325B (it
Inventor
George Albert Coffinberry
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of IT8120586A0 publication Critical patent/IT8120586A0/it
Application granted granted Critical
Publication of IT1139325B publication Critical patent/IT1139325B/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
    • F02C7/12—Cooling of plants
    • F02C7/14—Cooling of plants of fluids in the plant, e.g. lubricant or fuel
    • 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
    • F02C7/224—Heating fuel before feeding to the burner
    • 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
    • F05D2220/00—Application
    • F05D2220/50—Application for auxiliary power units (APU's)
    • 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
IT20586/81A 1980-03-20 1981-03-19 Apparato e metodo per migliorare il rendimento del carburante di un turbomotore a gas IT1139325B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/132,364 US4404793A (en) 1980-03-20 1980-03-20 Apparatus for improving the fuel efficiency of a gas turbine engine

Publications (2)

Publication Number Publication Date
IT8120586A0 true IT8120586A0 (it) 1981-03-19
IT1139325B IT1139325B (it) 1986-09-24

Family

ID=22453677

Family Applications (1)

Application Number Title Priority Date Filing Date
IT20586/81A IT1139325B (it) 1980-03-20 1981-03-19 Apparato e metodo per migliorare il rendimento del carburante di un turbomotore a gas

Country Status (6)

Country Link
US (1) US4404793A (it)
JP (1) JPS56154130A (it)
DE (1) DE3110179A1 (it)
FR (1) FR2478742B1 (it)
GB (1) GB2072268B (it)
IT (1) IT1139325B (it)

Families Citing this family (33)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2131094A (en) * 1982-11-29 1984-06-13 Gen Electric Engine oil heat recovery system
US4989403A (en) * 1988-05-23 1991-02-05 Sundstrand Corporation Surge protected gas turbine engine for providing variable bleed air flow
US4949544A (en) * 1988-12-06 1990-08-21 General Electric Company Series intercooler
US5241814A (en) * 1989-04-06 1993-09-07 Rolls-Royce Plc Management of heat generated by aircraft gas turbine installations
GB8907788D0 (en) * 1989-04-06 1989-05-17 Rolls Royce Plc Management of heat generated by aircraft gas turbine installations
US5177951A (en) * 1989-04-06 1993-01-12 Rolls-Royce Plc Method for management of heat generated by aircraft gas turbine installations
US5095693A (en) * 1989-08-04 1992-03-17 United Technologies Corporation High-efficiency gas turbine engine
US5036678A (en) * 1990-03-30 1991-08-06 General Electric Company Auxiliary refrigerated air system employing mixture of air bled from turbine engine compressor and air recirculated within auxiliary system
US5056335A (en) * 1990-04-02 1991-10-15 General Electric Company Auxiliary refrigerated air system employing input air from turbine engine compressor after bypassing and conditioning within auxiliary system
US5203163A (en) * 1990-08-01 1993-04-20 General Electric Company Heat exchange arrangement in a gas turbine engine fan duct for cooling hot bleed air
DE4131913A1 (de) * 1991-09-25 1993-04-08 Mtu Muenchen Gmbh Kuehlvorrichtung fuer hyperschall-luftstrahltriebwerke
US5255505A (en) * 1992-02-21 1993-10-26 Westinghouse Electric Corp. System for capturing heat transferred from compressed cooling air in a gas turbine
US5317877A (en) * 1992-08-03 1994-06-07 General Electric Company Intercooled turbine blade cooling air feed system
FR2705996B1 (fr) * 1993-06-03 1995-07-07 Snecma Système de dégivrage des parties avant d'une turbomachine.
US6578362B1 (en) * 1999-05-17 2003-06-17 General Electric Co. Methods and apparatus for supplying cooling air to turbine engines
US6584778B1 (en) * 2000-05-11 2003-07-01 General Electric Co. Methods and apparatus for supplying cooling air to turbine engines
US7185483B2 (en) 2003-01-21 2007-03-06 General Electric Company Methods and apparatus for exchanging heat
GB2421281A (en) * 2004-12-16 2006-06-21 Rolls Royce Plc Starting and anti-icing in a gas turbine engine
US7926290B2 (en) * 2006-12-18 2011-04-19 General Electric Company Turbine engine with modulated flow fan and method of operation
US20110171007A1 (en) * 2009-09-25 2011-07-14 James Edward Johnson Convertible fan system
US20110167792A1 (en) * 2009-09-25 2011-07-14 James Edward Johnson Adaptive engine
US20110179766A1 (en) * 2009-10-27 2011-07-28 Fly Steam, LLC Heat recovery system
US8397487B2 (en) * 2011-02-28 2013-03-19 General Electric Company Environmental control system supply precooler bypass
US9222411B2 (en) * 2011-12-21 2015-12-29 General Electric Company Bleed air and hot section component cooling air system and method
US9109842B2 (en) 2012-02-24 2015-08-18 Pratt & Whitney Canada Corp. Fuel air heat exchanger
US9057327B2 (en) * 2012-09-05 2015-06-16 General Electric Company Method and apparatus for heating liquid fuel supplied to a gas turbine combustor
EP2904231B1 (en) * 2012-10-01 2019-09-18 United Technologies Corporation Gas turbine engine including bleed system coupled to upstream and downstream locations of compressor and a corresponding method
FR3001260B1 (fr) * 2013-01-18 2017-04-21 Astrium Sas Dispositif de demarrage d'une turbopompe de moteur fusee
JP2016512862A (ja) * 2013-03-15 2016-05-09 ゼネラル・エレクトリック・カンパニイ 航空機エンジン向けのエネルギー効率のよい制御されたクライオ燃料の蒸発
FR3074533B1 (fr) * 2017-12-06 2020-11-06 Safran Aircraft Engines Circuit de commande hydraulique et pneumatique pour turboreacteur a echangeur de chaleur carburant/air
AR119134A1 (es) * 2019-06-10 2021-11-24 U S Well Services Llc Calentador integrado de gas de combustión para equipos móviles de acondicionamiento de combustible
US12196136B2 (en) * 2020-12-21 2025-01-14 General Electric Company Regenerative fuel heating system
EP4056475B1 (fr) * 2021-03-10 2023-04-26 Airbus Operations (S.A.S.) Aéronef comportant un moteur et un système de refroidissement

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2637984A (en) * 1950-07-26 1953-05-12 Gen Electric Turbine
US2691274A (en) * 1951-04-11 1954-10-12 Fairchild Engine & Airplane Air conditioning system for aircraft cabins
GB741433A (en) 1953-03-27 1955-12-07 Rolls Royce Improvements relating to gas turbine engine fuel systems
GB742270A (en) 1953-03-27 1955-12-21 Rolls Royce Improvements relating to gas-turbine engine fuel systems
GB781758A (en) 1953-11-13 1957-08-28 Dowty Fuel Syst Ltd Improvements in liquid fuel supply systems for gas turbine engines
GB797360A (en) 1955-03-07 1958-07-02 Dowty Fuel Syst Ltd Improvements relating to fuel systems for use with gas turbine engines
US3080716A (en) * 1956-03-08 1963-03-12 Thompson Ramo Wooldridge Inc Engine lubricating oil cooling systems for turbojets or the like
GB859479A (en) 1958-04-25 1961-01-25 Rolls Royce Aircraft fuel system
GB1003590A (en) * 1960-09-01 1965-09-08 Hawker Siddeley Aviation Ltd Improvements in systems for and methods of heat exchange aboard aircraft
US3547380A (en) * 1967-09-18 1970-12-15 Gen Electric Aircraft nuclear propulsion system
US3537513A (en) * 1968-03-11 1970-11-03 Garrett Corp Three-fluid heat exchanger
US3623546A (en) * 1969-11-10 1971-11-30 Avco Corp Cooling system for an electronic assembly mounted on a gas turbine engine
JPS496311A (it) * 1972-05-11 1974-01-21
US4041697A (en) * 1975-07-17 1977-08-16 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Oil cooling system for a gas turbine engine
GB1559828A (en) 1975-09-12 1980-01-30 Rolls Royce Fuel system for gas turbine engines
JPS5351322A (en) * 1976-10-20 1978-05-10 Hitachi Ltd Gas turbine combustion system
JPS54130716A (en) * 1978-03-31 1979-10-11 Hitachi Ltd Gas turbine plant

Also Published As

Publication number Publication date
IT1139325B (it) 1986-09-24
US4404793A (en) 1983-09-20
DE3110179A1 (de) 1981-12-24
FR2478742B1 (fr) 1988-04-22
GB2072268A (en) 1981-09-30
JPS56154130A (en) 1981-11-28
GB2072268B (en) 1984-05-02
FR2478742A1 (fr) 1981-09-25

Similar Documents

Publication Publication Date Title
IT1139325B (it) Apparato e metodo per migliorare il rendimento del carburante di un turbomotore a gas
IT7927878A0 (it) Tenuta di turbomotore a gas emetodo per fare la medesima.
IT8321934A0 (it) Carburatore per turbomotore a gas.
ZA811056B (en) A method for the operation of an internal-combustion engine with homogenous gas
GB2098719B (en) Gas turbine engine combustion apparatus
IT8019221A0 (it) Separatore di particelle estranee per turbomotori a gas.
JPS5575535A (en) Fuel injection apparatus for gas turbine engine
JPS5720539A (en) Exhaust nozzle for gas turbine engine
IT1076576B (it) Metodo per la rimozione di contaminanti dalla superficie di pezzi,quali per esempio i componenti di un turbomotore a gas
JPS5751901A (en) Gas turbine engine
GB2075447B (en) Thrust deflectors for gas turbine engines
IT8119348A0 (it) Complesso di aspirazione per turbomotori a gas.
IT8423428A0 (it) Turbocompressore a gas di scarico per un motore endotermico.
IT7826244A0 (it) Apparato per prova di condizioni di turbomotori a gas.
IT1190953B (it) Processo per la regolazione del carico di un motore termico sovralimentato con un turbocompressore a gas di scarico
IT8321090A0 (it) Prediffusore per motori a turbina a gas.
IT8022694A0 (it) Diffusore particolarmente adattoper turbomotori a gas.
IT7925254A0 (it) Metodo ed apparato per sopprimere il rumore a bassa frequenza, generato internamente, di un turbomotore a gas.
IT8321087A0 (it) Struttura di diffusione per un motore a turbina a gas.
JPS57110723A (en) Method of generating gas pressure with internal combustion engine and apparatus for executing the same
FI813071A7 (fi) Menettelytapa ja laite polttomoottorin suorituskyvyn ja hyötysuhteen parantamiseksi.
FI802683A7 (fi) Menetelmä ja laitteisto polttomoottorin hyötysuhteen parantamiseksi.
IT8123606A0 (it) Ugello di combustibile per turbomotore a gas.
JPS5776230A (en) Gas turbine engine
IT8148453A0 (it) Metodo per condizionare gas di combustione