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FR2405371A1 - Demarreur de turbomoteur - Google Patents

Demarreur de turbomoteur

Info

Publication number
FR2405371A1
FR2405371A1 FR7828395A FR7828395A FR2405371A1 FR 2405371 A1 FR2405371 A1 FR 2405371A1 FR 7828395 A FR7828395 A FR 7828395A FR 7828395 A FR7828395 A FR 7828395A FR 2405371 A1 FR2405371 A1 FR 2405371A1
Authority
FR
France
Prior art keywords
starter
turbomotor
turbine engine
auxiliary
turbine
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.)
Withdrawn
Application number
FR7828395A
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.)
TDY Industries LLC
Original Assignee
Teledyne Industries Inc
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 Teledyne Industries Inc filed Critical Teledyne Industries Inc
Publication of FR2405371A1 publication Critical patent/FR2405371A1/fr
Withdrawn legal-status Critical Current

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
    • F02C7/268—Starting drives for the rotor, acting directly on the rotor of the gas turbine to be started
    • F02C7/27—Fluid drives
    • 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)

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)
  • Output Control And Ontrol Of Special Type Engine (AREA)
  • Supercharger (AREA)

Abstract

Démarreur de turbomoteur auxiliaire. Ce démarreur est caractérisé en ce qu'une tuyauterie partant d'un générateur auxiliaire de gaz chauds amene ces derniers dans le turbomoteur pour lancer sa turbine. Application aux demarreurs de turbomoteurs.
FR7828395A 1977-10-05 1978-10-04 Demarreur de turbomoteur Withdrawn FR2405371A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/839,624 US4161102A (en) 1977-10-05 1977-10-05 Turbine engine starting system

Publications (1)

Publication Number Publication Date
FR2405371A1 true FR2405371A1 (fr) 1979-05-04

Family

ID=25280237

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7828395A Withdrawn FR2405371A1 (fr) 1977-10-05 1978-10-04 Demarreur de turbomoteur

Country Status (5)

Country Link
US (1) US4161102A (fr)
DE (1) DE2842860A1 (fr)
FR (1) FR2405371A1 (fr)
GB (1) GB2005354B (fr)
IT (1) IT7869296A0 (fr)

Families Citing this family (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE416224B (sv) * 1978-04-11 1980-12-08 Stal Laval Turbin Ab Gasturbinanleggning
DE3441509A1 (de) * 1984-11-14 1986-05-22 Klöckner-Humboldt-Deutz AG, 5000 Köln Verfahren und einrichtung zum anlassen einer gasturbine
US4815277A (en) * 1987-01-08 1989-03-28 Sundstrand Corporation Integrated power unit
US4819423A (en) * 1987-01-08 1989-04-11 Sundstrand Corporation Integrated power unit
US5003767A (en) * 1988-03-25 1991-04-02 Sundstrand Corporation Gas turbine starter system with power augmentation
US4947641A (en) * 1988-06-23 1990-08-14 Sundstrand Corporation Pulse accelerating turbine
US4899536A (en) * 1988-07-21 1990-02-13 Sundstrand Corporation Starting system for a turbine engine
WO1990001627A1 (fr) * 1988-07-29 1990-02-22 Sundstrand Corporation Demarreur pour un moteur a turbine comprenant une chambre de stockage d'oxydant et de combustion combines
US5131223A (en) * 1989-07-13 1992-07-21 Sundstrand Corporation Integrated booster and sustainer engine for a missile
US5136838A (en) * 1989-12-07 1992-08-11 Sundstrand Corporation Stored energy, wide energy range turbine starting system
US5115637A (en) * 1989-12-22 1992-05-26 Sundstrand Corporation External cartridge gas combustor ignitor
US5265407A (en) * 1990-06-22 1993-11-30 Sundstrand Corporation Oxidant blow down heater
US5179831A (en) * 1990-07-31 1993-01-19 Sundstrand Corporation Stored energy system for driving a turbine wheel
US5174106A (en) * 1990-08-24 1992-12-29 Talley Defense Systems, Inc. Secondary ignition system
SE467590B (sv) * 1990-12-05 1992-08-10 Abb Carbon Ab Startanordning vid kraftanlaeggning
US5150569A (en) * 1990-12-14 1992-09-29 Williams International Corporation Integrated propulsion system
US5161369A (en) * 1991-01-28 1992-11-10 Williams International Corporation Aft fan gas turbine engine
US6644033B2 (en) * 2002-01-17 2003-11-11 The Boeing Company Tip impingement turbine air starter for turbine engine
US6941760B1 (en) 2003-03-19 2005-09-13 Hamilton Sundstrand Corporation Start system for expendable gas turbine engine
IL179762A (en) 2006-11-30 2011-06-30 Rafael Advanced Defense Sys Starting turbine engines
IL190103A (en) * 2008-03-11 2014-02-27 Rafael Advanced Defense Sys METHOD AND SYSTEM FOR IMPROVING TURBINE ENGINE STARTING, AND IGNITION MODULE
FR3007459B1 (fr) * 2013-06-19 2016-10-14 Airbus Operations Sas Systeme et procede de mise en rotation d'un element rotatif d'un dispositif mecanique, en particulier d'une turbomachine.
US10247104B2 (en) 2015-04-23 2019-04-02 Rolls-Royce North American Technologies, Inc. Oxygen enhanced pneumatic starting
US20200182155A1 (en) * 2018-12-07 2020-06-11 United Technologies Corporation Casing with integral cavity

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2457833A (en) * 1943-02-03 1949-01-04 Westinghouse Electric Corp Cartridge starter for combustion gas turbines
GB616695A (en) * 1944-04-21 1949-01-26 British Thomson Houston Co Ltd Improvements in and relating to gas turbine power plants
GB743809A (en) * 1953-08-01 1956-01-25 Armstrong Siddeley Motors Ltd Ignition means for use in starting gas turbine engines
FR1112882A (fr) * 1954-10-18 1956-03-20 Dispositif de démarrage pour turbo-machines: spécialement pour turbo-réacteurs etturbo-propulseurs
FR1204518A (fr) * 1958-04-09 1960-01-26 Snecma Procédé et dispositif de démarrage pour aérodynes équipés d'alternateurs
US2924935A (en) * 1956-04-09 1960-02-16 United Aireraft Corp Fuel supply for gas generator
GB938013A (en) * 1959-04-27 1963-09-25 Gen Electric Improvements in and relating to electric turbine-start control arrangements
FR1563248A (fr) * 1967-04-03 1969-04-11
FR2000233A1 (fr) * 1968-01-15 1969-09-05 Plessey Ltd
DE2500795A1 (de) * 1975-01-10 1976-07-15 Maschf Augsburg Nuernberg Ag Vorrichtung zum beschleunigen eines gaserzeugers einer mehrwelligen gasturbine, insbesondere kraftfahrzeug-gasturbine, aus dem stand

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2465092A (en) * 1947-05-29 1949-03-22 Gen Electric Ignition means for combustion chambers
GB881816A (en) * 1959-07-03 1961-11-08 Rolls Royce Improved gas turbine engine
US2982095A (en) * 1959-07-09 1961-05-02 Westinghouse Electric Corp Gas generating device
US3093968A (en) * 1960-05-05 1963-06-18 Cornell Aeronautical Labor Inc Method and apparatus for augmenting the drive of a gas turbine
US3439495A (en) * 1967-09-18 1969-04-22 Robert L Binsley Resonating combustor for directly starting turbine engine

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2457833A (en) * 1943-02-03 1949-01-04 Westinghouse Electric Corp Cartridge starter for combustion gas turbines
GB616695A (en) * 1944-04-21 1949-01-26 British Thomson Houston Co Ltd Improvements in and relating to gas turbine power plants
GB743809A (en) * 1953-08-01 1956-01-25 Armstrong Siddeley Motors Ltd Ignition means for use in starting gas turbine engines
FR1112882A (fr) * 1954-10-18 1956-03-20 Dispositif de démarrage pour turbo-machines: spécialement pour turbo-réacteurs etturbo-propulseurs
US2924935A (en) * 1956-04-09 1960-02-16 United Aireraft Corp Fuel supply for gas generator
FR1204518A (fr) * 1958-04-09 1960-01-26 Snecma Procédé et dispositif de démarrage pour aérodynes équipés d'alternateurs
GB938013A (en) * 1959-04-27 1963-09-25 Gen Electric Improvements in and relating to electric turbine-start control arrangements
FR1563248A (fr) * 1967-04-03 1969-04-11
FR2000233A1 (fr) * 1968-01-15 1969-09-05 Plessey Ltd
DE2500795A1 (de) * 1975-01-10 1976-07-15 Maschf Augsburg Nuernberg Ag Vorrichtung zum beschleunigen eines gaserzeugers einer mehrwelligen gasturbine, insbesondere kraftfahrzeug-gasturbine, aus dem stand

Also Published As

Publication number Publication date
IT7869296A0 (it) 1978-10-04
US4161102A (en) 1979-07-17
GB2005354A (en) 1979-04-19
GB2005354B (en) 1982-03-24
DE2842860A1 (de) 1979-04-26

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Legal Events

Date Code Title Description
ST Notification of lapse