FR2960592B1 - Procede de demarrage d'un moteur d'aeronef - Google Patents

Procede de demarrage d'un moteur d'aeronef

Info

Publication number
FR2960592B1
FR2960592B1 FR1054054A FR1054054A FR2960592B1 FR 2960592 B1 FR2960592 B1 FR 2960592B1 FR 1054054 A FR1054054 A FR 1054054A FR 1054054 A FR1054054 A FR 1054054A FR 2960592 B1 FR2960592 B1 FR 2960592B1
Authority
FR
France
Prior art keywords
starting
aircraft engine
aircraft
engine
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.)
Active
Application number
FR1054054A
Other languages
English (en)
Other versions
FR2960592A1 (fr
Inventor
Djemouai Hadjidj
Franck Serge Jacques Liotte
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.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA SAS
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 SNECMA SAS filed Critical SNECMA SAS
Priority to FR1054054A priority Critical patent/FR2960592B1/fr
Publication of FR2960592A1 publication Critical patent/FR2960592A1/fr
Application granted granted Critical
Publication of FR2960592B1 publication Critical patent/FR2960592B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/18—Lubricating arrangements
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/08—Cooling; Heating; Heat-insulation
    • F01D25/10—Heating, e.g. warming-up before starting
    • 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
    • F02C7/275—Mechanical 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
    • F05D2270/00—Control
    • F05D2270/01—Purpose of the control system
    • F05D2270/05—Purpose of the control system to affect the output of the engine
    • F05D2270/052—Torque
    • 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
    • F05D2270/00—Control
    • F05D2270/30—Control parameters, e.g. input parameters
    • F05D2270/303—Temperature
    • 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
    • F05D2270/00—Control
    • F05D2270/30—Control parameters, e.g. input parameters
    • F05D2270/304—Spool rotational speed
    • 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)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Lubrication Of Internal Combustion Engines (AREA)
FR1054054A 2010-05-27 2010-05-27 Procede de demarrage d'un moteur d'aeronef Active FR2960592B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1054054A FR2960592B1 (fr) 2010-05-27 2010-05-27 Procede de demarrage d'un moteur d'aeronef

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1054054A FR2960592B1 (fr) 2010-05-27 2010-05-27 Procede de demarrage d'un moteur d'aeronef

Publications (2)

Publication Number Publication Date
FR2960592A1 FR2960592A1 (fr) 2011-12-02
FR2960592B1 true FR2960592B1 (fr) 2016-02-26

Family

ID=43415355

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1054054A Active FR2960592B1 (fr) 2010-05-27 2010-05-27 Procede de demarrage d'un moteur d'aeronef

Country Status (1)

Country Link
FR (1) FR2960592B1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2022008834A1 (fr) 2020-07-09 2022-01-13 Safran Helicopter Engines Procede de demarrage d'un moteur d'aeronef

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3062972B1 (fr) * 2017-02-10 2021-06-11 Safran Aircraft Engines Dispositif de generation d'energie electrique auxiliaire et turbomachine comportant un tel dispositif
EP3418505B1 (fr) * 2017-06-23 2022-04-13 HS Marston Aerospace Limited Circuit de lubrification chauffé

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA2157688A1 (fr) * 1993-03-03 1994-09-15 Robert L. Ii Simmons Systeme integre de regulation d'une turbomachine
US7204090B2 (en) * 2004-06-17 2007-04-17 Pratt & Whitney Canada Corp. Modulated current gas turbine engine starting system
US7690205B2 (en) * 2005-09-20 2010-04-06 Honeywell International Inc. Gas turbine engine cold start mechanization
US7448220B2 (en) * 2005-10-19 2008-11-11 Hamilton Sundstrand Corporation Torque control for starting system
FR2915238A1 (fr) * 2007-04-23 2008-10-24 Airbus France Sa Procede et systeme pour le demarrage d'un turbomoteur par temps froid.
FR2925110B1 (fr) * 2007-12-13 2014-06-27 Hispano Suiza Sa Dispositif d'alimentation en huile d'un moteur d'aeronef equipe d'au moins un demarreur-generateur.

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2022008834A1 (fr) 2020-07-09 2022-01-13 Safran Helicopter Engines Procede de demarrage d'un moteur d'aeronef
FR3112365A1 (fr) 2020-07-09 2022-01-14 Safran Helicopter Engines Procede de demarrage d’un moteur d’aeronef

Also Published As

Publication number Publication date
FR2960592A1 (fr) 2011-12-02

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