FR2995635B1 - Dispositif et procede de fourniture de puissance non propulsive pour un aeronef - Google Patents

Dispositif et procede de fourniture de puissance non propulsive pour un aeronef Download PDF

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Publication number
FR2995635B1
FR2995635B1 FR1258682A FR1258682A FR2995635B1 FR 2995635 B1 FR2995635 B1 FR 2995635B1 FR 1258682 A FR1258682 A FR 1258682A FR 1258682 A FR1258682 A FR 1258682A FR 2995635 B1 FR2995635 B1 FR 2995635B1
Authority
FR
France
Prior art keywords
power
turbine
aircraft
compressor
control system
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
FR1258682A
Other languages
English (en)
Other versions
FR2995635A1 (fr
Inventor
Fabien Silet
Jean-Francois Rideau
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 Power Units SAS
Original Assignee
Safran Power Units 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
Priority to FR1258682A priority Critical patent/FR2995635B1/fr
Application filed by Safran Power Units SAS filed Critical Safran Power Units SAS
Priority to JP2015531622A priority patent/JP2015531721A/ja
Priority to EP13767043.6A priority patent/EP2895719A1/fr
Priority to US14/427,625 priority patent/US20150246733A1/en
Priority to BR112015005648A priority patent/BR112015005648A2/pt
Priority to PCT/FR2013/052072 priority patent/WO2014041291A1/fr
Priority to CA2884409A priority patent/CA2884409A1/fr
Priority to RU2015111682A priority patent/RU2659860C2/ru
Priority to CN201380050484.4A priority patent/CN104781522A/zh
Publication of FR2995635A1 publication Critical patent/FR2995635A1/fr
Application granted granted Critical
Publication of FR2995635B1 publication Critical patent/FR2995635B1/fr
Active legal-status Critical Current
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Classifications

    • 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
    • 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
    • B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space
    • B64D13/06—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space the air being conditioned
    • 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
    • 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
    • B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space
    • B64D13/06—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space the air being conditioned
    • B64D2013/0603—Environmental Control Systems
    • B64D2013/0611—Environmental Control Systems combined with auxiliary power units (APU's)
    • 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
    • Y02T50/50—On board measures aiming to increase energy efficiency
    • 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)
  • Combustion & Propulsion (AREA)
  • Chemical & Material Sciences (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Pulmonology (AREA)
  • General Health & Medical Sciences (AREA)
  • Health & Medical Sciences (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
  • Control Of Eletrric Generators (AREA)
  • Direct Current Feeding And Distribution (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)

Abstract

Un dispositif de fourniture de puissance non propulsive pour un aéronef, le dispositif comportant : - un système de contrôle de l'environnement (1) qui comprend une turbine (12) de distribution d'air régulé (A ) destiné à une cabine d'aéronef (2) et un compresseur de charge (11) relié à la turbine de distribution (12) par un arbre de liaison (13) ; - un groupe de puissance auxiliaire (4) comportant un compresseur de puissance (41), une chambre de combustion (44) et une turbine de puissance (42) reliée au dit compresseur de puissance (41) par un arbre de puissance (43) ; - le système de contrôle de l'environnement (1) comportant une turbine libre d'entraînement (5) solidaire de l'arbre de liaison (13), le système de contrôle de l'environnement (1) et le groupe de puissance auxiliaire (4) étant configurés de manière à ce que la turbine de puissance (42) fournisse un flux d'air (A ) à la turbine libre d'entraînement (5) de manière à entraîner le compresseur de charge (11) solidaire de l'arbre de liaison (13).
FR1258682A 2012-09-17 2012-09-17 Dispositif et procede de fourniture de puissance non propulsive pour un aeronef Active FR2995635B1 (fr)

Priority Applications (9)

Application Number Priority Date Filing Date Title
FR1258682A FR2995635B1 (fr) 2012-09-17 2012-09-17 Dispositif et procede de fourniture de puissance non propulsive pour un aeronef
EP13767043.6A EP2895719A1 (fr) 2012-09-17 2013-09-10 Dispositif et procede de fourniture de puissance non propulsive pour un aeronef
US14/427,625 US20150246733A1 (en) 2012-09-17 2013-09-10 Device and method for supplying non-propulsive power for an aircraft
BR112015005648A BR112015005648A2 (pt) 2012-09-17 2013-09-10 dispositivo e processo de fornecimento de potência não propulsora para uma aeronave
JP2015531622A JP2015531721A (ja) 2012-09-17 2013-09-10 非推進動力を航空機に供給する装置及び方法
PCT/FR2013/052072 WO2014041291A1 (fr) 2012-09-17 2013-09-10 Dispositif et procede de fourniture de puissance non propulsive pour un aeronef
CA2884409A CA2884409A1 (fr) 2012-09-17 2013-09-10 Dispositif et procede de fourniture de puissance non propulsive pour un aeronef
RU2015111682A RU2659860C2 (ru) 2012-09-17 2013-09-10 Устройство и способ обеспечения нетяговой мощностью летательного аппарата
CN201380050484.4A CN104781522A (zh) 2012-09-17 2013-09-10 用于为飞行器提供非推进功率的设备和方法

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1258682A FR2995635B1 (fr) 2012-09-17 2012-09-17 Dispositif et procede de fourniture de puissance non propulsive pour un aeronef

Publications (2)

Publication Number Publication Date
FR2995635A1 FR2995635A1 (fr) 2014-03-21
FR2995635B1 true FR2995635B1 (fr) 2025-02-14

Family

ID=47754609

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1258682A Active FR2995635B1 (fr) 2012-09-17 2012-09-17 Dispositif et procede de fourniture de puissance non propulsive pour un aeronef

Country Status (9)

Country Link
US (1) US20150246733A1 (fr)
EP (1) EP2895719A1 (fr)
JP (1) JP2015531721A (fr)
CN (1) CN104781522A (fr)
BR (1) BR112015005648A2 (fr)
CA (1) CA2884409A1 (fr)
FR (1) FR2995635B1 (fr)
RU (1) RU2659860C2 (fr)
WO (1) WO2014041291A1 (fr)

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GB201513952D0 (en) 2015-08-07 2015-09-23 Rolls Royce Plc Aircraft pneumatic system
FR3041607B1 (fr) * 2015-09-24 2018-08-17 Microturbo Unite d'alimentation en air sous pression pour aeronef
US10919638B2 (en) * 2016-05-31 2021-02-16 The Boeing Company Aircraft cabin pressurization energy harvesting
JP6609334B2 (ja) 2018-01-30 2019-11-20 株式会社Ｓｕｂａｒｕ 航空機用レシプロエンジンの高空始動装置
GB201915307D0 (en) * 2019-10-23 2019-12-04 Rolls Royce Plc Aircraft auxiliary power unit
US12275536B2 (en) * 2019-10-24 2025-04-15 Pratt & Whitney Canada Corp. Aircraft power supply arrangements
US11795872B2 (en) 2020-02-14 2023-10-24 Rtx Corporation Engine and secondary power unit integrated operation
CN113323757B (zh) * 2021-06-01 2022-12-20 北京清软创想信息技术有限责任公司 一种分离式气压型辅助动力空气管路系统
US12146443B2 (en) 2023-03-31 2024-11-19 Pratt & Whitney Canada Corp. Boosting gas turbine engine power with fluid motor

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US2777301A (en) * 1952-06-30 1957-01-15 Garrett Corp All-purpose power and air conditioning system
US4684081A (en) * 1986-06-11 1987-08-04 Lockheed Corporation Multifunction power system for an aircraft
US5490645A (en) * 1993-12-09 1996-02-13 Allied-Signal Inc. Fully integrated environmental and secondary power system
US5442905A (en) * 1994-04-08 1995-08-22 Alliedsignal Inc. Integrated power and cooling environmental control system
US5813630A (en) * 1996-09-27 1998-09-29 Mcdonnell Douglas Corporation Multi-mode secondary power unit
EP0975862B1 (fr) * 1997-04-18 2003-01-08 Honeywell International Inc. Systeme integre ameliore servant a l'alimentation secondaire et a la gestion des conditions ambiantes de la cabine
US5899085A (en) * 1997-08-01 1999-05-04 Mcdonnell Douglas Corporation Integrated air conditioning and power unit
JP2000203497A (ja) * 1999-01-12 2000-07-25 Shimadzu Corp 航空機用空気調和装置
US6305156B1 (en) * 1999-09-03 2001-10-23 Alliedsignal Inc. Integrated bleed air and engine starting system
US6283410B1 (en) * 1999-11-04 2001-09-04 Hamilton Sundstrand Corporation Secondary power integrated cabin energy system for a pressurized aircraft
JP4300682B2 (ja) * 2000-05-30 2009-07-22 株式会社島津製作所 走行体
AU2002242188A1 (en) * 2001-02-16 2002-09-04 United Technologies Corporation Improved aircraft architecture with a reduced bleed aircraft secondary power system
US7210653B2 (en) * 2002-10-22 2007-05-01 The Boeing Company Electric-based secondary power system architectures for aircraft
FR2900636B1 (fr) * 2006-05-05 2009-03-06 Hispano Suiza Sa Circuit d'alimentation en energie electrique pour des equipements electriques d'un moteur d'aeronef ou de son environnement
US7624592B2 (en) * 2006-05-17 2009-12-01 Northrop Grumman Corporation Flexible power and thermal architectures using a common machine
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US20100170262A1 (en) * 2009-01-06 2010-07-08 Kaslusky Scott F Aircraft power and thermal management system with electric co-generation
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US20120138737A1 (en) * 2010-12-02 2012-06-07 Bruno Louis J Aircraft power distribution architecture

Also Published As

Publication number Publication date
EP2895719A1 (fr) 2015-07-22
FR2995635A1 (fr) 2014-03-21
CN104781522A (zh) 2015-07-15
BR112015005648A2 (pt) 2017-07-04
JP2015531721A (ja) 2015-11-05
RU2659860C2 (ru) 2018-07-04
RU2015111682A (ru) 2016-11-10
CA2884409A1 (fr) 2014-03-20
WO2014041291A1 (fr) 2014-03-20
US20150246733A1 (en) 2015-09-03

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