GB1604515A - Gas turbine engines - Google Patents

Gas turbine engines Download PDF

Info

Publication number
GB1604515A
GB1604515A GB21346/78A GB2134678A GB1604515A GB 1604515 A GB1604515 A GB 1604515A GB 21346/78 A GB21346/78 A GB 21346/78A GB 2134678 A GB2134678 A GB 2134678A GB 1604515 A GB1604515 A GB 1604515A
Authority
GB
United Kingdom
Prior art keywords
engine
input
speed
force
piston
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
GB21346/78A
Other languages
English (en)
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.)
Garrett Corp
Original Assignee
Garrett Corp
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 Garrett Corp filed Critical Garrett Corp
Publication of GB1604515A publication Critical patent/GB1604515A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D17/00Regulating or controlling by varying flow
    • F01D17/20Devices dealing with sensing elements or final actuators or transmitting means between them, e.g. power-assisted
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D17/00Regulating or controlling by varying flow
    • F01D17/10Final actuators
    • F01D17/12Final actuators arranged in stator parts
    • F01D17/14Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/16Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, 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
    • F02C7/36Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C9/00Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/16Control of working fluid flow
    • F02C9/20Control of working fluid flow by throttling; by adjusting vanes
    • F02C9/22Control of working fluid flow by throttling; by adjusting vanes by adjusting turbine vanes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B1/00Engines characterised by fuel-air mixture compression
    • F02B1/02Engines characterised by fuel-air mixture compression with positive ignition
    • F02B1/04Engines characterised by fuel-air mixture compression with positive ignition with fuel-air mixture admission into cylinder
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/40Transmission of power
    • F05D2260/402Transmission of power through friction drives
    • F05D2260/4023Transmission of power through friction drives through a friction clutch

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Control Of Turbines (AREA)
  • Supercharger (AREA)
GB21346/78A 1977-12-22 1978-05-23 Gas turbine engines Expired GB1604515A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/863,370 US4197699A (en) 1977-12-22 1977-12-22 Free turbine type gas turbine engine with variable free turbine guide vane control system

Publications (1)

Publication Number Publication Date
GB1604515A true GB1604515A (en) 1981-12-09

Family

ID=25340994

Family Applications (1)

Application Number Title Priority Date Filing Date
GB21346/78A Expired GB1604515A (en) 1977-12-22 1978-05-23 Gas turbine engines

Country Status (4)

Country Link
US (1) US4197699A (US20100223739A1-20100909-C00005.png)
CA (1) CA1134628A (US20100223739A1-20100909-C00005.png)
FR (1) FR2412702A1 (US20100223739A1-20100909-C00005.png)
GB (1) GB1604515A (US20100223739A1-20100909-C00005.png)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2119862A (en) * 1982-05-06 1983-11-23 Gen Electric Variable stator vane (VSV) closed loop control system of a compressor

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4299088A (en) * 1979-10-26 1981-11-10 General Electric Company Cyclic load duty control for gas turbine
US4406117A (en) * 1979-10-26 1983-09-27 General Electric Company Cyclic load duty control for gas turbine
EP0058158B1 (en) * 1980-08-21 1987-03-25 The Garrett Corporation Engine management system
US5497615A (en) * 1994-03-21 1996-03-12 Noe; James C. Gas turbine generator set
US7927067B2 (en) * 2007-05-01 2011-04-19 United Technologies Corporation System and method for controlling stator assemblies
US8090456B2 (en) * 2008-11-03 2012-01-03 United Technologies Corporation System and method for design and control of engineering systems utilizing component-level dynamic mathematical model
US8668434B2 (en) * 2009-09-02 2014-03-11 United Technologies Corporation Robust flow parameter model for component-level dynamic turbine system control
US8315741B2 (en) * 2009-09-02 2012-11-20 United Technologies Corporation High fidelity integrated heat transfer and clearance in component-level dynamic turbine system control
US9512784B2 (en) * 2010-01-29 2016-12-06 Pratt & Whitney Canada Corp. Free gas turbine with constant temperature-corrected gas generator speed
US9765702B2 (en) * 2013-03-15 2017-09-19 Ansaldo Energia Ip Uk Limited Ensuring non-excessive variation of gradients in auto-tuning a gas turbine engine
FR3082225B1 (fr) 2018-06-07 2020-06-05 Safran Helicopter Engines Systeme propulsif asymetrique a recuperation de chaleur
FR3120897A1 (fr) * 2021-03-17 2022-09-23 Airbus Operations (S.A.S.) Procédé de protection de la mise en rotation d’un moteur d’aéronef.
CN117267149B (zh) * 2023-11-17 2024-01-23 国网山西省电力公司电力科学研究院 一种大容量电力变压器油泵状态在线感知装置及评估方法

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3300966A (en) * 1963-06-04 1967-01-31 Chrysler Corp Control mechanism for adjustable gas turbine nozzle
US3362156A (en) * 1965-12-21 1968-01-09 Ford Motor Co Turbine nozzle actuator
US3508395A (en) * 1968-04-01 1970-04-28 Ford Motor Co Control system for motor vehicle type gas turbine engine
US3521446A (en) * 1968-04-16 1970-07-21 Chandler Evans Inc Fuel control having pressure referenced turbine overspeed device
US3621657A (en) * 1968-09-25 1971-11-23 Daimler Benz Ag Control installation for the automatic adjustment of the movable guide blades especially of the output turbine of a gas turbine drive unit
FR2057298A5 (US20100223739A1-20100909-C00005.png) * 1969-08-11 1971-05-21 Lucas Industries Ltd
US3719041A (en) * 1971-02-05 1973-03-06 Secr Defence Temperature-responsive control for gas turbine engines
DE2208040C3 (de) * 1972-02-21 1979-05-23 Robert Bosch Gmbh, 7000 Stuttgart Regelschaltung für die Prozeßtemperatur einer Gasturbine
US3858390A (en) * 1973-06-04 1975-01-07 Garrett Corp Power turbine nozzle control system

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2119862A (en) * 1982-05-06 1983-11-23 Gen Electric Variable stator vane (VSV) closed loop control system of a compressor

Also Published As

Publication number Publication date
US4197699A (en) 1980-04-15
FR2412702B1 (US20100223739A1-20100909-C00005.png) 1984-11-30
CA1134628A (en) 1982-11-02
FR2412702A1 (fr) 1979-07-20

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PCNP Patent ceased through non-payment of renewal fee

Effective date: 19920523