FR3011589B1 - Machine thermique aeronautique comprenant une reserve de fluide sous pression pour demarrer un moteur a cycle ferme - Google Patents

Machine thermique aeronautique comprenant une reserve de fluide sous pression pour demarrer un moteur a cycle ferme Download PDF

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Publication number
FR3011589B1
FR3011589B1 FR1359645A FR1359645A FR3011589B1 FR 3011589 B1 FR3011589 B1 FR 3011589B1 FR 1359645 A FR1359645 A FR 1359645A FR 1359645 A FR1359645 A FR 1359645A FR 3011589 B1 FR3011589 B1 FR 3011589B1
Authority
FR
France
Prior art keywords
aeronautical
starting
pressurized fluid
cycle engine
closed cycle
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
FR1359645A
Other languages
English (en)
Other versions
FR3011589A1 (fr
Inventor
Denis Joubert Hugues
Philippe Devieilletoile
Guillaume Labedan
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.)
Societe Motorisations Aeronautiques SA
Original Assignee
Societe Motorisations Aeronautiques SA
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 Societe Motorisations Aeronautiques SA filed Critical Societe Motorisations Aeronautiques SA
Priority to FR1359645A priority Critical patent/FR3011589B1/fr
Priority to PCT/FR2014/052502 priority patent/WO2015049469A1/fr
Publication of FR3011589A1 publication Critical patent/FR3011589A1/fr
Application granted granted Critical
Publication of FR3011589B1 publication Critical patent/FR3011589B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02N—STARTING OF COMBUSTION ENGINES; STARTING AIDS FOR SUCH ENGINES, NOT OTHERWISE PROVIDED FOR
    • F02N9/00—Starting of engines by supplying auxiliary pressure fluid to their working chambers
    • F02N9/04—Starting of engines by supplying auxiliary pressure fluid to their working chambers the pressure fluid being generated otherwise, e.g. by compressing air
    • 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
    • B64D41/00—Power installations for auxiliary purposes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B33/00—Engines characterised by provision of pumps for charging or scavenging
    • F02B33/44—Passages conducting the charge from the pump to the engine inlet, e.g. reservoirs
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B37/00—Engines characterised by provision of pumps driven at least for part of the time by exhaust
    • F02B37/04—Engines with exhaust drive and other drive of pumps, e.g. with exhaust-driven pump and mechanically-driven second pump
    • F02B37/10—Engines with exhaust drive and other drive of pumps, e.g. with exhaust-driven pump and mechanically-driven second pump at least one pump being alternatively or simultaneously driven by exhaust and other drive, e.g. by pressurised fluid from a reservoir or an engine-driven pump
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B37/00—Engines characterised by provision of pumps driven at least for part of the time by exhaust
    • F02B37/12—Control of the pumps
    • F02B37/20—Control of the pumps by increasing exhaust energy, e.g. using combustion chamber by after-burning
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02D—CONTROLLING COMBUSTION ENGINES
    • F02D41/00—Electrical control of supply of combustible mixture or its constituents
    • F02D41/0002—Controlling intake air
    • F02D41/0007—Controlling intake air for control of turbo-charged or super-charged engines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02N—STARTING OF COMBUSTION ENGINES; STARTING AIDS FOR SUCH ENGINES, NOT OTHERWISE PROVIDED FOR
    • F02N13/00—Starting of engines, or driving of starting apparatus by use of explosives, e.g. stored in cartridges
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02N—STARTING OF COMBUSTION ENGINES; STARTING AIDS FOR SUCH ENGINES, NOT OTHERWISE PROVIDED FOR
    • F02N99/00—Subject matter not provided for in other groups of this subclass
    • F02N99/002—Starting combustion engines by ignition means
    • F02N99/006—Providing a combustible mixture inside the cylinder
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B33/00—Engines characterised by provision of pumps for charging or scavenging
    • F02B33/44—Passages conducting the charge from the pump to the engine inlet, e.g. reservoirs
    • F02B33/443—Heating of charging air, e.g. for facilitating the starting
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02D—CONTROLLING COMBUSTION ENGINES
    • F02D41/00—Electrical control of supply of combustible mixture or its constituents
    • F02D41/0025—Controlling engines characterised by use of non-liquid fuels, pluralities of fuels, or non-fuel substances added to the combustible mixtures
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02D—CONTROLLING COMBUSTION ENGINES
    • F02D41/00—Electrical control of supply of combustible mixture or its constituents
    • F02D41/02—Circuit arrangements for generating control signals
    • F02D41/04—Introducing corrections for particular operating conditions
    • F02D41/06—Introducing corrections for particular operating conditions for engine starting or warming up
    • F02D41/062—Introducing corrections for particular operating conditions for engine starting or warming up for starting
    • F02D41/064—Introducing corrections for particular operating conditions for engine starting or warming up for starting at cold start
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02N—STARTING OF COMBUSTION ENGINES; STARTING AIDS FOR SUCH ENGINES, NOT OTHERWISE PROVIDED FOR
    • F02N11/00—Starting of engines by means of electric motors
    • F02N11/04—Starting of engines by means of electric motors the motors being associated with current generators
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02N—STARTING OF COMBUSTION ENGINES; STARTING AIDS FOR SUCH ENGINES, NOT OTHERWISE PROVIDED FOR
    • F02N19/00—Starting aids for combustion engines, not otherwise provided for
    • F02N19/02—Aiding engine start by thermal means, e.g. using lighted wicks
    • F02N19/04—Aiding engine start by thermal means, e.g. using lighted wicks by heating of fluids used in engines
    • 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
    • Y02T10/00—Road transport of goods or passengers
    • Y02T10/10—Internal combustion engine [ICE] based vehicles
    • Y02T10/12—Improving ICE efficiencies

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Supercharger (AREA)
FR1359645A 2013-10-04 2013-10-04 Machine thermique aeronautique comprenant une reserve de fluide sous pression pour demarrer un moteur a cycle ferme Active FR3011589B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR1359645A FR3011589B1 (fr) 2013-10-04 2013-10-04 Machine thermique aeronautique comprenant une reserve de fluide sous pression pour demarrer un moteur a cycle ferme
PCT/FR2014/052502 WO2015049469A1 (fr) 2013-10-04 2014-10-02 Machine thermique aeronautique comprenant une reserve de fluide sous pression pour demarrer un moteur a cycle ferme

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1359645 2013-10-04
FR1359645A FR3011589B1 (fr) 2013-10-04 2013-10-04 Machine thermique aeronautique comprenant une reserve de fluide sous pression pour demarrer un moteur a cycle ferme

Publications (2)

Publication Number Publication Date
FR3011589A1 FR3011589A1 (fr) 2015-04-10
FR3011589B1 true FR3011589B1 (fr) 2018-02-23

Family

ID=49753400

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1359645A Active FR3011589B1 (fr) 2013-10-04 2013-10-04 Machine thermique aeronautique comprenant une reserve de fluide sous pression pour demarrer un moteur a cycle ferme

Country Status (2)

Country Link
FR (1) FR3011589B1 (fr)
WO (1) WO2015049469A1 (fr)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104832346B (zh) * 2015-05-12 2016-11-23 广西玉柴机器股份有限公司 一种电控发动机的高原冷启动的辅助装置
US10968825B2 (en) * 2018-04-19 2021-04-06 The Boeing Company Flow multiplier systems for aircraft
CN108730094B (zh) * 2018-06-28 2024-07-19 潍柴动力股份有限公司 一种在高原低温环境下的辅助起动控制系统及方法
RU194761U1 (ru) * 2019-09-02 2019-12-23 ФЕДЕРАЛЬНОЕ ГОСУДАРСТВЕННОЕ КАЗЕННОЕ ВОЕННОЕ ОБРАЗОВАТЕЛЬНОЕ УЧРЕЖДЕНИЕ ВЫСШЕГО ОБРАЗОВАНИЯ Военная академия Ракетных войск стратегического назначения имени Петра Великого МИНИСТЕРСТВА ОБОРОНЫ РОССИЙСКОЙ ФЕДЕРАЦИИ Система экстренного пуска дизельного двигателя транспортного средства
CN115421543B (zh) * 2022-11-02 2023-05-16 北京宇航系统工程研究所 一种低温贮箱压力控制方法及系统

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2842937A (en) * 1955-09-01 1958-07-15 Gen Electric Aircraft engine cartridge starter control system
US2921431A (en) * 1955-11-01 1960-01-19 Thompson Prod Inc Engine turbosupercharger system
DE2735545C3 (de) * 1977-08-06 1981-07-30 Mtu Motoren- Und Turbinen-Union Friedrichshafen Gmbh, 7990 Friedrichshafen Vorrichtung zum Fördern von Hilfsluft für den Startvorgang eines aufgeladenen Dieselmotors
JPS58146036U (ja) * 1982-03-26 1983-10-01 株式会社小松製作所 エンジンの２段過給装置
GB9417338D0 (en) * 1994-08-25 1994-10-19 Randle James N Internal combustion engine
DE10005490A1 (de) * 2000-02-08 2001-08-16 Bosch Gmbh Robert Heizanlage
DE10139526A1 (de) * 2001-08-10 2003-02-20 Daimler Chrysler Ag Kraftfahrzeug
FR2854652B1 (fr) * 2003-05-09 2007-03-23 Renault Sa Moteur a combustion interne comportant des moyens pour ameliorer le rendement d'un turbocompresseur
FR2901846A1 (fr) * 2006-06-01 2007-12-07 Peugeot Citroen Automobiles Sa Moteur a combustion interne equipe de moyens d'alimentation en air d'appoint et procede d'actionnement du moteur
JP5530117B2 (ja) * 2009-03-31 2014-06-25 川崎重工業株式会社 過給機付内燃機関の排気再循環システム
US8434305B2 (en) * 2010-05-06 2013-05-07 Honeywell International Inc. Compressed-air-assisted turbocharger system for internal combustion engine
JP5994232B2 (ja) * 2011-11-07 2016-09-21 いすゞ自動車株式会社 発進加速補助装置

Also Published As

Publication number Publication date
FR3011589A1 (fr) 2015-04-10
WO2015049469A1 (fr) 2015-04-09

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