CH336645A - Gasturbinenanlage - Google Patents

Gasturbinenanlage

Info

Publication number
CH336645A
CH336645A CH336645DA CH336645A CH 336645 A CH336645 A CH 336645A CH 336645D A CH336645D A CH 336645DA CH 336645 A CH336645 A CH 336645A
Authority
CH
Switzerland
Prior art keywords
gas turbine
turbine plant
plant
gas
turbine
Prior art date
Application number
Other languages
English (en)
Inventor
Wark Hutchinson David
Original Assignee
Wark Hutchinson David
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 Wark Hutchinson David filed Critical Wark Hutchinson David
Publication of CH336645A publication Critical patent/CH336645A/de

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
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/26—Control of fuel supply
    • F02C9/28—Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed
    • 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
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/107—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor with two or more rotors connected by power transmission
    • F02C3/113—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor with two or more rotors connected by power transmission with variable power transmission between rotors
    • 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
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • 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
    • F02C7/08—Heating air supply before combustion, e.g. by exhaust gases
    • 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
    • F02C7/36—Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user
    • 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
    • F05D2220/30—Application in turbines
    • F05D2220/32—Application in turbines in gas turbines
    • F05D2220/324—Application in turbines in gas turbines to drive unshrouded, low solidity propeller

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
CH336645D 1950-09-13 1954-10-29 Gasturbinenanlage CH336645A (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US184543A US2693080A (en) 1950-09-13 1950-09-13 Differential gas turbine

Publications (1)

Publication Number Publication Date
CH336645A true CH336645A (de) 1959-02-28

Family

ID=22677335

Family Applications (1)

Application Number Title Priority Date Filing Date
CH336645D CH336645A (de) 1950-09-13 1954-10-29 Gasturbinenanlage

Country Status (4)

Country Link
US (1) US2693080A (de)
BE (1) BE532916A (de)
CH (1) CH336645A (de)
FR (1) FR1113920A (de)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB817591A (en) * 1954-11-08 1959-08-06 Parsons C A & Co Ltd Improvements in and relating to gas turbine plants
US2960825A (en) * 1955-10-19 1960-11-22 Thompson Ramo Wooldridge Inc Reexpansion gas turbine engine with differential compressor drive
US3056256A (en) * 1956-05-07 1962-10-02 United Aircraft Corp Afterburner control for a multispool gas turbine power plant
DE1127150B (de) * 1957-05-24 1962-04-05 Kronogard Sven Olof Gasturbinenanlage
US2908189A (en) * 1957-06-12 1959-10-13 Garrett Corp Combination engine starter and constant speed drive
US3280554A (en) * 1964-09-30 1966-10-25 Ford Motor Co Motor vehicle gas turbine drive
US3632222A (en) * 1970-10-21 1972-01-04 Avco Corp Damping means for differential gas turbine engine
US3848482A (en) * 1973-08-03 1974-11-19 Avco Corp Differential gearing for gas turbine engine
DE2525950A1 (de) * 1975-06-11 1976-12-16 Motoren Turbinen Union Gasturbinentriebwerk in baukastenbauweise
US4132064A (en) * 1977-05-26 1979-01-02 The Garrett Corporation Turbine engine with differential gearing between high pressure turbine and compressor
US4251987A (en) * 1979-08-22 1981-02-24 General Electric Company Differential geared engine
US6725644B2 (en) * 1999-05-18 2004-04-27 Arthur Vanmoor Combined input and output system for an internal combustion engine and turbine power plant
US20040159089A1 (en) * 1999-05-18 2004-08-19 Arthur Vanmoor Combined input and output system for a combustion engine and turbine power plant
EP1199445A1 (de) * 2000-10-17 2002-04-24 Siemens Aktiengesellschaft Vorrichtung und Verfahren zur Brennstoffvorwärmung in kombinierten Gas- und Dampfturbinenanlagen
US6895741B2 (en) * 2003-06-23 2005-05-24 Pratt & Whitney Canada Corp. Differential geared turbine engine with torque modulation capability
KR101603218B1 (ko) * 2010-03-16 2016-03-15 한화테크윈 주식회사 터빈 시스템
US9347373B2 (en) 2013-12-19 2016-05-24 Pratt & Whitney Canada Corp. Gas turbine engine with transmission
US11041444B2 (en) * 2018-11-02 2021-06-22 Pratt & Whitney Canada Corp. Gas turbine engine with differential gearbox

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB595357A (en) * 1944-04-08 1947-12-03 Power Jets Res & Dev Ltd Improvements in or relating to power plants
FR418794A (fr) * 1909-10-08 1910-12-19 Henri Royer Turbo-moteur pour torpilles automobiles
US2358815A (en) * 1935-03-28 1944-09-26 Jarvis C Marble Compressor apparatus
US2514513A (en) * 1942-03-06 1950-07-11 Lockheed Aircraft Corp Jet power plant with boundary layer control for aircraft
US2423183A (en) * 1944-07-13 1947-07-01 Fairey Aviat Co Ltd Turbine type jet propulsion
US2575683A (en) * 1947-01-13 1951-11-20 Lockheed Aircraft Corp Intercooler and control system for turbo power plants

Also Published As

Publication number Publication date
FR1113920A (fr) 1956-04-05
BE532916A (de) 1956-03-14
US2693080A (en) 1954-11-02

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