FR3057029B1 - Turbopropulseur comprenant une generatrice d'electricite integree - Google Patents

Turbopropulseur comprenant une generatrice d'electricite integree Download PDF

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Publication number
FR3057029B1
FR3057029B1 FR1659512A FR1659512A FR3057029B1 FR 3057029 B1 FR3057029 B1 FR 3057029B1 FR 1659512 A FR1659512 A FR 1659512A FR 1659512 A FR1659512 A FR 1659512A FR 3057029 B1 FR3057029 B1 FR 3057029B1
Authority
FR
France
Prior art keywords
turbopropeller
electricity generator
integrated electricity
turboprop
housed
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
FR1659512A
Other languages
English (en)
Other versions
FR3057029A1 (fr
Inventor
Thomas Klonowski
David Cazaux
Olivier Lafargue
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 Helicopter Engines SAS
Original Assignee
Safran Helicopter Engines 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 Safran Helicopter Engines SAS filed Critical Safran Helicopter Engines SAS
Priority to FR1659512A priority Critical patent/FR3057029B1/fr
Publication of FR3057029A1 publication Critical patent/FR3057029A1/fr
Application granted granted Critical
Publication of FR3057029B1 publication Critical patent/FR3057029B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • F02C7/32—Arrangement, mounting, or driving, of auxiliaries
    • 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
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/20—Adaptations of gas-turbine plants for driving vehicles
    • F02C6/206—Adaptations of gas-turbine plants for driving vehicles the vehicles being airscrew driven
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/10—Aircraft characterised by the type or position of power plants of gas-turbine type 
    • 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
    • F05D2220/70—Application in combination with
    • F05D2220/76—Application in combination with an electrical generator

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)

Abstract

Une génératrice électrique (9) est logée dans une cavité (14) annulaire entre le carter (15) et l'arbre porte-hélice (3) d'un turbopropulseur, en imposant peu ou pas d'encombrement supplémentaire et avec des équipements annexes (16) et (25), légers.
FR1659512A 2016-10-03 2016-10-03 Turbopropulseur comprenant une generatrice d'electricite integree Active FR3057029B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1659512A FR3057029B1 (fr) 2016-10-03 2016-10-03 Turbopropulseur comprenant une generatrice d'electricite integree

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1659512 2016-10-03
FR1659512A FR3057029B1 (fr) 2016-10-03 2016-10-03 Turbopropulseur comprenant une generatrice d'electricite integree

Publications (2)

Publication Number Publication Date
FR3057029A1 FR3057029A1 (fr) 2018-04-06
FR3057029B1 true FR3057029B1 (fr) 2020-06-19

Family

ID=57750161

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1659512A Active FR3057029B1 (fr) 2016-10-03 2016-10-03 Turbopropulseur comprenant une generatrice d'electricite integree

Country Status (1)

Country Link
FR (1) FR3057029B1 (fr)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2019166703A1 (fr) * 2018-02-28 2019-09-06 Safran Helicopter Engines Turbopropulseur comprenant une generatrice d'electricite integree
FR3091060B1 (fr) 2018-12-20 2020-12-04 Safran Helicopter Engines Machine électrique avec dispositif de démagnétisation forcée des aimants permanents
FR3116303B1 (fr) 2020-11-16 2022-10-14 Safran Helicopter Engines Turbomachine à propulsion hybride et aéronef comportant une telle turbomachine
FR3126016A1 (fr) 2021-08-04 2023-02-10 Safran Helicopter Engines Turbopropulseur apte à fournir une fonction d’éolienne de secours et aéronef comportant un tel turbopropulseur
FR3136908A1 (fr) 2022-06-18 2023-12-22 Safran Helicopter Engines Machine électrique pour aéronef comprenant au moins un organe de protection de court-circuit entre deux phases du stator et procédé de protection

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB584563A (en) * 1945-01-01 1947-01-17 British Thomson Houston Co Ltd Improvements relating to the prevention of ice formation on the rotating parts of aircraft
US2488392A (en) * 1945-08-21 1949-11-15 Fairey Aviat Co Ltd Electrical equipment on aircraft
US6769874B2 (en) * 2002-03-15 2004-08-03 Hamilton Sundstrand Permanent magnet alternator for a gas turbine engine
US8757972B2 (en) * 2011-08-12 2014-06-24 Hamilton Sundstrand Corporation De-icing system for modular counter rotating propeller
US9973058B2 (en) * 2014-07-23 2018-05-15 Hamilton Sundstrand Corporation Propeller in-hub power generation and control

Also Published As

Publication number Publication date
FR3057029A1 (fr) 2018-04-06

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