FR2173143A1 - - Google Patents

Info

Publication number
FR2173143A1
FR2173143A1 FR7306172A FR7306172A FR2173143A1 FR 2173143 A1 FR2173143 A1 FR 2173143A1 FR 7306172 A FR7306172 A FR 7306172A FR 7306172 A FR7306172 A FR 7306172A FR 2173143 A1 FR2173143 A1 FR 2173143A1
Authority
FR
France
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.)
Granted
Application number
FR7306172A
Other versions
FR2173143B3 (fr
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.)
Robert Bosch GmbH
Original Assignee
Robert Bosch GmbH
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 Robert Bosch GmbH filed Critical Robert Bosch GmbH
Publication of FR2173143A1 publication Critical patent/FR2173143A1/fr
Application granted granted Critical
Publication of FR2173143B3 publication Critical patent/FR2173143B3/fr
Expired legal-status Critical Current

Links

Classifications

    • 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
    • F02C6/00Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/20Adaptations of gas-turbine plants for driving vehicles
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Control Of Eletrric Generators (AREA)
  • Control Of Velocity Or Acceleration (AREA)
  • Supercharger (AREA)
  • Feedback Control In General (AREA)
FR7306172A 1972-02-21 1973-02-21 Expired FR2173143B3 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE2208040A DE2208040C3 (de) 1972-02-21 1972-02-21 Regelschaltung für die Prozeßtemperatur einer Gasturbine

Publications (2)

Publication Number Publication Date
FR2173143A1 true FR2173143A1 (fr) 1973-10-05
FR2173143B3 FR2173143B3 (fr) 1976-02-20

Family

ID=5836587

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7306172A Expired FR2173143B3 (fr) 1972-02-21 1973-02-21

Country Status (8)

Country Link
US (1) US3844114A (fr)
JP (1) JPS5532893B2 (fr)
CH (1) CH552132A (fr)
DE (1) DE2208040C3 (fr)
FR (1) FR2173143B3 (fr)
GB (1) GB1424138A (fr)
IT (1) IT973278B (fr)
SE (1) SE384901B (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0471623A1 (fr) * 1990-08-16 1992-02-19 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Dispositif compensateur de température devant la turbine d'une turbomachine d'aviation

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2241363B2 (de) * 1972-08-23 1975-01-09 Motoren- Und Turbinen-Union Muenchen Gmbh, 8000 Muenchen Regeleinrichtung für ein Gasturbinentriebwerk, insbesondere eines Kraftfahrzeugs
US3938321A (en) * 1974-03-04 1976-02-17 General Motors Corporation Gas turbine control
US3952502A (en) * 1974-03-04 1976-04-27 General Motors Corporation Gas turbine control
US4134258A (en) * 1974-06-10 1979-01-16 Nippondenso Co., Ltd. Fuel control system
GB1520412A (en) * 1974-07-09 1978-08-09 Lucas Industries Ltd Gas turbine engine fuel control systems
US4016717A (en) * 1975-02-19 1977-04-12 Westinghouse Electric Corporation Matching response of a blade path temperature limit signal to characteristics of a gas turbine
JPS598653B2 (ja) * 1975-10-11 1984-02-25 三菱重工業株式会社 ジドウシヤヨウ 2 ジクガスタ−ビンノセイギヨソウチ
US4206597A (en) * 1976-04-23 1980-06-10 The Boeing Company Fan R.P.M. control loop stabilization using high rotor speed
US4314441A (en) * 1977-07-22 1982-02-09 Westinghouse Electric Corp. Gas turbine power plant control apparatus including an ambient temperature responsive control system
US4197699A (en) * 1977-12-22 1980-04-15 The Garrett Corporation Free turbine type gas turbine engine with variable free turbine guide vane control system
US4543782A (en) * 1982-05-21 1985-10-01 Lucas Industries Gas turbine engine fuel control systems
JPS5910742A (ja) * 1982-07-08 1984-01-20 Toyota Motor Corp ガスタ−ビン機関の制御装置
JP2743516B2 (ja) * 1989-10-05 1998-04-22 トヨタ自動車株式会社 二軸式ガスタービン機関
US5379584A (en) * 1992-08-18 1995-01-10 Alliedsignal Inc. Synthesis of critical temperature of a turbine engine
JP5725817B2 (ja) * 2010-11-30 2015-05-27 三菱日立パワーシステムズ株式会社 ガスタービン制御装置および発電システム
CN102890517B (zh) * 2011-07-20 2015-01-07 烟台杰瑞石油装备技术有限公司 一种直燃式液氮蒸发器的控制设备

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1090143A (en) * 1965-04-07 1967-11-08 Hawker Siddeley Dynamics Ltd Improvements in or relating to electrical control systems for engines
GB1215931A (en) * 1967-03-11 1970-12-16 Rolls Royce Improvements in or relating to gas turbine engines
GB1205323A (en) * 1968-01-22 1970-09-16 Mini Of Technology Engine fuel supply servo systems
US3470691A (en) * 1968-06-17 1969-10-07 Avco Corp Automatic starting and protection system for a gas turbine
US3606754A (en) * 1969-05-19 1971-09-21 Chandler Evans Inc Hybrid fuel control
US3601984A (en) * 1969-10-27 1971-08-31 Gen Electric Temperature rate control system
US3780527A (en) * 1971-04-21 1973-12-25 Lucas Industries Ltd Control apparatus for a gas turbine engine

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0471623A1 (fr) * 1990-08-16 1992-02-19 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Dispositif compensateur de température devant la turbine d'une turbomachine d'aviation
FR2665927A1 (fr) * 1990-08-16 1992-02-21 Snecma Dispositif compensateur de temperature devant la turbine d'une turbomachine d'aviation.
US5157918A (en) * 1990-08-16 1992-10-27 Societe Nationale D'etude Et De Construction De Motors D'aviation Temperature compensating device for turboshaft aero-engines

Also Published As

Publication number Publication date
DE2208040B2 (de) 1978-10-05
FR2173143B3 (fr) 1976-02-20
US3844114A (en) 1974-10-29
JPS5532893B2 (fr) 1980-08-27
DE2208040C3 (de) 1979-05-23
GB1424138A (en) 1976-02-11
IT973278B (it) 1974-06-10
CH552132A (de) 1974-07-31
DE2208040A1 (de) 1973-09-06
SE384901B (sv) 1976-05-24
JPS4896909A (fr) 1973-12-11

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