JP5269780B2 - 燃料電池を使用した航空機用発電システム - Google Patents
燃料電池を使用した航空機用発電システム Download PDFInfo
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- JP5269780B2 JP5269780B2 JP2009517349A JP2009517349A JP5269780B2 JP 5269780 B2 JP5269780 B2 JP 5269780B2 JP 2009517349 A JP2009517349 A JP 2009517349A JP 2009517349 A JP2009517349 A JP 2009517349A JP 5269780 B2 JP5269780 B2 JP 5269780B2
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- Prior art keywords
- compressor
- turbine
- shaft
- electric machine
- fuel cell
- Prior art date
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- 239000000446 fuel Substances 0.000 title claims description 26
- 238000010248 power generation Methods 0.000 title claims description 10
- 239000007789 gas Substances 0.000 description 15
- MWUXSHHQAYIFBG-UHFFFAOYSA-N nitrogen oxide Inorganic materials O=[N] MWUXSHHQAYIFBG-UHFFFAOYSA-N 0.000 description 5
- 239000000567 combustion gas Substances 0.000 description 3
- 229930195733 hydrocarbon Natural products 0.000 description 3
- 150000002430 hydrocarbons Chemical class 0.000 description 3
- 230000001360 synchronised effect Effects 0.000 description 3
- 239000004215 Carbon black (E152) Substances 0.000 description 2
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 description 2
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- 239000007858 starting material Substances 0.000 description 2
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 229910002092 carbon dioxide Inorganic materials 0.000 description 1
- 239000001569 carbon dioxide Substances 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 239000003350 kerosene Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 230000009466 transformation Effects 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Chemical compound O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Images
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
-
- 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
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/14—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant
-
- 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
-
- 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, or structural parts of the aircraft
- B64D13/06—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being conditioned
- B64D2013/0603—Environmental Control Systems
- B64D2013/0611—Environmental Control Systems combined with auxiliary power units (APU's)
-
- 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, or structural parts of the aircraft
- B64D13/06—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being conditioned
- B64D2013/0603—Environmental Control Systems
- B64D2013/0644—Environmental Control Systems including electric motors or generators
-
- 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
- B64D2041/002—Mounting arrangements for auxiliary power units (APU's)
-
- 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
- B64D2041/005—Fuel cells
-
- 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
- Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02T90/40—Application of hydrogen technology to transportation, e.g. using fuel cells
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Fuel Cell (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
Description
第1のコンプレッサと、
第1のコンプレッサに接続される圧縮空気の入口と、燃料入口とを有し、直流電力を生み出す燃料電池と、
加圧下で燃料電池からガス流を受け入れて、第1のコンプレッサに機械的に結合されて第1のコンプレッサを駆動するためのタービンと、
航空機客室に加圧空気を供給するために飛行中に使用される回路の第2のコンプレッサであって、タービンの軸に機械的に結合されている客室への供給用の第2のコンプレッサと、
を備える。
Claims (8)
- 第1のコンプレッサ(20)と、
第1のコンプレッサに接続された圧縮空気入口と、燃料入口とを有し、直流電力を生み出す燃料電池(10)と、
加圧下で燃料電池からガス流を受け入れて、第1のコンプレッサを駆動するために第1のコンプレッサに機械的に結合されたタービン(30)と、
航空機客室に加圧空気を供給するために飛行中に使用される回路の第2のコンプレッサ(46)と、
を備える航空機用の発電システムであって、
客室に供給する第2のコンプレッサ(46)がタービン(30)の軸に機械的に結合されることを特徴とする、システム。 - 第1のコンプレッサ(20)と第2のコンプレッサ(46)とが共通のタービン軸(34)に取り付けられることを特徴とする、請求項1に記載のシステム。
- タービン(30)が、加圧下で、燃料電池(10)からガス流を受け入れて第1のタービン軸(34)を駆動する第1のタービン段と、第1のタービン段からガス流を受け入れて第2のタービン軸(35)を駆動する第2のタービン段とを備え、第1のコンプレッサ(20)が第1のタービン軸(34)によって駆動され、第2のコンプレッサ(46)が第2の軸(35)によって駆動されることを特徴とする、請求項1に記載のシステム。
- タービン(30)の軸に機械的に結合された電気機械(50)をさらに備えることを特徴とする、請求項1に記載のシステム。
- 電気機械(50)および第2のコンプレッサ(46)が同じタービン軸に共通に取り付けられることを特徴とする、請求項4に記載のシステム。
- 電気機械(50)が発電機としての第1の動作モードと電動機としての第2の動作モードを有し、電気機械が取り付けられるタービン軸で得られる機械トルクを少なくとも所定の最小値の値に維持するために、電気機械の第1の動作モードと第2の動作モードとを切り替える調整回路(52)が設けられることを特徴とする、請求項4および5のいずれか一項に記載のシステム。
- 電気機械の回転速度を所定の設定点値にサーボ制御する調整システムが設けられることを特徴とする、請求項4から6のいずれか一項に記載のシステム。
- コンプレッサ(20)から供給される圧縮空気を燃料電池に入れる前に加熱するために、燃料電池(10)に供給する圧縮空気とタービン(30)から出るガス流とを独立に通す熱交換器(38)を含むことを特徴とする、請求項1から7のいずれか一項に記載のシステム。
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0652660A FR2902759B1 (fr) | 2006-06-27 | 2006-06-27 | Systeme de generation de puissance pour aeronef utilisant une pile a combustible |
FR0652660 | 2006-06-27 | ||
PCT/FR2007/051528 WO2008001006A1 (fr) | 2006-06-27 | 2007-06-26 | Systeme de generation de puissance pour aeronef utilisant une pile a combustible |
Publications (2)
Publication Number | Publication Date |
---|---|
JP2009541141A JP2009541141A (ja) | 2009-11-26 |
JP5269780B2 true JP5269780B2 (ja) | 2013-08-21 |
Family
ID=37775529
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2009517349A Active JP5269780B2 (ja) | 2006-06-27 | 2007-06-26 | 燃料電池を使用した航空機用発電システム |
Country Status (9)
Country | Link |
---|---|
US (1) | US7986052B2 (ja) |
JP (1) | JP5269780B2 (ja) |
CN (1) | CN101479153B (ja) |
CA (1) | CA2656435C (ja) |
DE (1) | DE112007001611B4 (ja) |
FR (1) | FR2902759B1 (ja) |
GB (1) | GB2452217B (ja) |
RU (1) | RU2431585C2 (ja) |
WO (1) | WO2008001006A1 (ja) |
Families Citing this family (31)
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FR2902759B1 (fr) * | 2006-06-27 | 2008-10-24 | Turbomeca | Systeme de generation de puissance pour aeronef utilisant une pile a combustible |
DE102007001912A1 (de) * | 2007-01-12 | 2008-07-17 | Airbus Deutschland Gmbh | Brennstoffversorgungsanlage für ein Brennstoffzellensystem |
US8097968B2 (en) * | 2007-12-21 | 2012-01-17 | Honeywell International, Inc. | Position-controlled start from the AC line using a synchronous machine |
DE102008006742A1 (de) | 2008-01-30 | 2009-08-06 | Airbus Deutschland Gmbh | Luftfahrzeug-Brennstoffzellensystem |
JP5442206B2 (ja) * | 2008-02-05 | 2014-03-12 | 新明和工業株式会社 | 電力システム |
US8727270B2 (en) * | 2010-11-16 | 2014-05-20 | Rolls-Royce Corporation | Aircraft, propulsion system, and system for taxiing an aircraft |
FR2968716B1 (fr) * | 2010-12-13 | 2012-12-28 | Turbomeca | Procede de controle de la generation electrique appliquee a une turbine a gaz d'aeronef et turbomoteur mettant en oeuvre un tel procede |
CN102201586B (zh) * | 2011-04-22 | 2013-12-25 | 爱科腾博(大连)科技有限公司 | 燃料电池系统 |
FR2975375B1 (fr) * | 2011-05-18 | 2014-01-10 | Dassault Aviat | Systeme autonome de generation de puissance electrique et de conditionnement pour un aeronef, aeronef et procede associes |
FR2978123B1 (fr) * | 2011-07-18 | 2013-08-23 | Snecma | Systeme de controle et de surveillance d'un aeronef |
GB2494666B (en) | 2011-09-15 | 2014-11-05 | Rolls Royce Fuel Cell Systems Ltd | A solid oxide fuel cell system |
GB2494667A (en) | 2011-09-15 | 2013-03-20 | Rolls Royce Fuel Cell Systems Ltd | A solid oxide fuel cell system |
US20130087632A1 (en) * | 2011-10-11 | 2013-04-11 | Patrick Germain | Gas turbine engine exhaust ejector nozzle with de-swirl cascade |
FR2983248B1 (fr) * | 2011-11-29 | 2015-04-03 | Turbomeca | Turbomachine comportant une pompe d'alimentation en carburant a activation electrique et procede d'alimentation en carburant d'une turbomachine |
DE102013204200A1 (de) * | 2013-03-12 | 2014-09-18 | Robert Bosch Gmbh | Elektrische Maschine in einem Kraftfahrzeug mit Drehzahlsignaleingang |
FR3013683B1 (fr) * | 2013-11-27 | 2017-07-07 | Microturbo | Procede et systeme pour la production optimisee d'energie non propulsive |
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FR3041607B1 (fr) * | 2015-09-24 | 2018-08-17 | Microturbo | Unite d'alimentation en air sous pression pour aeronef |
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FR3068009B1 (fr) * | 2017-06-23 | 2023-09-15 | Zodiac Aerotechnics | Systeme d'inertage d'au moins un volume dans un aeronef via au moins une pile a combustible |
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-
2006
- 2006-06-27 FR FR0652660A patent/FR2902759B1/fr active Active
-
2007
- 2007-06-26 RU RU2009102513/11A patent/RU2431585C2/ru active
- 2007-06-26 JP JP2009517349A patent/JP5269780B2/ja active Active
- 2007-06-26 CA CA2656435A patent/CA2656435C/fr active Active
- 2007-06-26 DE DE112007001611.6T patent/DE112007001611B4/de active Active
- 2007-06-26 CN CN2007800242117A patent/CN101479153B/zh active Active
- 2007-06-26 US US12/306,575 patent/US7986052B2/en active Active
- 2007-06-26 GB GB0823393A patent/GB2452217B/en active Active
- 2007-06-26 WO PCT/FR2007/051528 patent/WO2008001006A1/fr active Application Filing
Also Published As
Publication number | Publication date |
---|---|
GB2452217A (en) | 2009-02-25 |
FR2902759B1 (fr) | 2008-10-24 |
CN101479153A (zh) | 2009-07-08 |
US20090309364A1 (en) | 2009-12-17 |
CA2656435C (fr) | 2013-12-17 |
GB0823393D0 (en) | 2009-01-28 |
WO2008001006A1 (fr) | 2008-01-03 |
JP2009541141A (ja) | 2009-11-26 |
FR2902759A1 (fr) | 2007-12-28 |
RU2431585C2 (ru) | 2011-10-20 |
US7986052B2 (en) | 2011-07-26 |
DE112007001611T5 (de) | 2009-04-30 |
GB2452217B (en) | 2010-12-22 |
RU2009102513A (ru) | 2010-08-10 |
CN101479153B (zh) | 2012-07-25 |
CA2656435A1 (fr) | 2008-01-03 |
DE112007001611B4 (de) | 2020-02-27 |
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