JP5965320B2 - 航空機ブリードシステムの熱電発電機 - Google Patents
航空機ブリードシステムの熱電発電機 Download PDFInfo
- Publication number
- JP5965320B2 JP5965320B2 JP2012542013A JP2012542013A JP5965320B2 JP 5965320 B2 JP5965320 B2 JP 5965320B2 JP 2012542013 A JP2012542013 A JP 2012542013A JP 2012542013 A JP2012542013 A JP 2012542013A JP 5965320 B2 JP5965320 B2 JP 5965320B2
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- Prior art keywords
- air
- bleed
- thermoelectric generator
- bleed air
- ram
- 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.)
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D37/00—Arrangements in connection with fuel supply for power plant
- B64D37/32—Safety measures not otherwise provided for, e.g. preventing explosive conditions
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS 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; ARRANGEMENTS 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
- B64D2013/0618—Environmental Control Systems with arrangements for reducing or managing bleed air, using another air source, e.g. ram air
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS 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
- B64D2013/0685—Environmental Control Systems with ozone control
-
- 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
- Y02T50/40—Weight reduction
-
- 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
Description
また、本発明は以下に記載する態様を含む。
(態様1)
発電装置であって、ブリード空気システム(100)と、前記ブリード空気システム(100)に連結され、ラム空気とブリード空気との間の温度差を利用して前記発電する熱電発電機(106)を備える発電装置。
(態様2)
前記ブリード空気システム(100)は、前記ブリード空気内のオゾンレベルを低減するオゾンコンバータ(212)と、前記オゾンコンバータ(212)から前記ラム空気と前記ブリード空気を受け入れる空気間熱交換器(200)を備える、態様1に記載の装置。
(態様3)
前記熱電発電機(106)が空気間熱交換器(200)に連結されている、態様1又は2に記載の装置。
(態様4)
前記ブリード空気システム(100)が、前記ラム空気と前記ブリード空気を監視し管理するシステム制御を含む、態様1乃至3のいずれか1項に記載の装置。
(態様5)
空気間熱交換器(200)が、前記ラム空気を使用して前記ブリード空気を冷却する、態様1乃至4のいずれか1項に記載の装置。
(態様6)
前記熱電発電機(106)に連結された窒素発生システム(120)をさらに備える、態様1乃至5のいずれか1項に記載の装置。
(態様7)
航空機ブリードシステム上で発電する方法であって、ラム空気を受入れ、ブリード空気を受け入れ、前記ラム空気及び前記ブリード空気を前記航空機ブリードシステムに連結された熱電発電機(106)に通して発電するステップを含む方法。
(態様8)
前記熱電発電機(106)によって前記ブリード空気を冷却して、前記航空機ブリードシステムによって使用されるラム空気の量を減らすステップをさらに含む、態様7に記載の方法。
(態様9)
前記熱電発電機(106)によって前記ブリード空気を冷却して、前記航空機ブリードシステムによって使用されるラム空気の量を減らすステップをさらに含む、態様7又は8に記載の方法。
Claims (7)
- ラム空気を使用してブリード空気を冷却するブリード空気システムと、
前記ブリード空気システムに連結され、ラム空気とブリード空気との間の温度差を利用して発電する熱電発電機と、を備えるシステム。 - 前記熱電発電機がラム空気とブリード空気を受け入れる空気間熱交換器に連結されている、請求項1に記載のシステム。
- 前記空気間熱交換器が、前記ラム空気を使用して前記ブリード空気を冷却する、請求項2に記載のシステム。
- 前記ブリード空気システムは、前記ブリード空気内のオゾンレベルを低減するオゾンコンバータを備え、前記空気間熱交換器は前記オゾンコンバータから前記ブリード空気を受け入れる、請求項2または3に記載のシステム。
- 前記ブリード空気システムが、前記ラム空気と前記ブリード空気を監視し管理するシステム制御を含む、請求項1乃至4のいずれか1項に記載のシステム。
- 前記熱電発電機に連結された窒素発生システムをさらに備える、請求項1乃至5のいずれか1項に記載のシステム。
- ブリード空気を冷却する方法であって、
ラム空気を受入れるステップと、
ブリード空気を受け入れるステップと、
航空機ブリードシステムにおいて、ラム空気を使用してブリード空気を冷却するステップと、
前記ラム空気及び前記ブリード空気を前記航空機ブリードシステムに連結された熱電発電機に通してラム空気とブリード空気との間の温度差を利用して発電するステップと、を含む方法。
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US12/632,250 US8484983B2 (en) | 2009-12-07 | 2009-12-07 | Thermoelectric generator on an aircraft bleed system |
US12/632,250 | 2009-12-07 | ||
PCT/US2010/053622 WO2011071602A2 (en) | 2009-12-07 | 2010-10-21 | Thermoelectric generator on an aircraft bleed system |
Publications (3)
Publication Number | Publication Date |
---|---|
JP2013512821A JP2013512821A (ja) | 2013-04-18 |
JP2013512821A5 JP2013512821A5 (ja) | 2013-11-07 |
JP5965320B2 true JP5965320B2 (ja) | 2016-08-03 |
Family
ID=44063309
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2012542013A Active JP5965320B2 (ja) | 2009-12-07 | 2010-10-21 | 航空機ブリードシステムの熱電発電機 |
Country Status (6)
Country | Link |
---|---|
US (1) | US8484983B2 (ja) |
EP (1) | EP2509869B1 (ja) |
JP (1) | JP5965320B2 (ja) |
CN (1) | CN102648127B (ja) |
CA (1) | CA2782972C (ja) |
WO (1) | WO2011071602A2 (ja) |
Families Citing this family (36)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2500269A1 (en) * | 2011-03-18 | 2012-09-19 | AGUSTAWESTLAND S.p.A. | Aircraft capable of hovering |
US9470153B2 (en) * | 2011-10-05 | 2016-10-18 | United Technologies Corporation | Combined pump system for engine TMS AOC reduction and ECS loss elimination |
GB2496839A (en) * | 2011-10-24 | 2013-05-29 | Ge Aviat Systems Ltd | Thermal electrical power generation for aircraft |
US9388740B2 (en) * | 2012-02-15 | 2016-07-12 | The Boeing Company | Thermoelectric generator in turbine engine nozzles |
US8944367B2 (en) * | 2012-03-05 | 2015-02-03 | Sikorsky Aircraft Corporation | Rotary wing aircraft propulsion system |
US9163562B2 (en) * | 2012-03-14 | 2015-10-20 | United Technologies Corporation | Constant speed pump system for engine ECS loss elimination |
US9394803B2 (en) * | 2012-03-14 | 2016-07-19 | United Technologies Corporation | Bypass air-pump system within the core engine to provide air for an environmental control system in a gas turbine engine |
US9151224B2 (en) * | 2012-03-14 | 2015-10-06 | United Technologies Corporation | Constant-speed pump system for engine thermal management system AOC reduction and environmental control system loss elimination |
US9360240B2 (en) | 2012-11-09 | 2016-06-07 | Laird Technologies, Inc. | Thermoelectric assembly |
WO2014105334A1 (en) * | 2012-12-28 | 2014-07-03 | General Electric Company | System and method for aviation electric power production |
GB2513132B (en) * | 2013-04-16 | 2015-05-27 | Ge Aviat Systems Ltd | Method for predicting a bleed air system fault |
US20140352324A1 (en) * | 2013-05-29 | 2014-12-04 | Hamilton Sunstrand Corporation | Dual pressure regulator shut off valve apparatus |
EP2829706B1 (en) * | 2013-07-25 | 2016-09-14 | The Boeing Company | Bleed air systems for use with aircrafts and related methods |
US9666781B2 (en) * | 2013-08-19 | 2017-05-30 | The Boeing Company | Methods for recovering waste energy from bleed air ducts |
JP6612272B2 (ja) | 2014-07-03 | 2019-11-27 | ゼネラル・エレクトリック・カンパニイ | ジェットエンジン冷気冷却システム |
GB201415078D0 (en) | 2014-08-26 | 2014-10-08 | Rolls Royce Plc | Gas turbine engine anti-icing system |
EP2995553B1 (en) * | 2014-09-09 | 2017-02-01 | Airbus Defence and Space GmbH | Air generation unit for an aircraft and method for its operation |
US9901874B2 (en) | 2015-01-20 | 2018-02-27 | Hamilton Sundstrand Corporation | High temperature air separation system architecture |
EP3069997B1 (en) * | 2015-03-16 | 2020-04-29 | Airbus Operations S.L. | Aircraft comprising a heat exchanger |
US10144521B2 (en) | 2015-08-04 | 2018-12-04 | Hamilton Sundstrand Corporation | Electric compressor for use with a wing anti-ice system |
US10082059B2 (en) * | 2015-09-17 | 2018-09-25 | Borla Performance Industries, Inc. | Recovery of electrical energy and water from exhaust gas |
US20170159563A1 (en) * | 2015-12-07 | 2017-06-08 | General Electric Company | Method and system for pre-cooler exhaust energy recovery |
US10801408B2 (en) * | 2016-02-03 | 2020-10-13 | Rolls-Royce North American Technologies Inc. | Gas turbine engine with thermoelectric system |
US11473497B2 (en) | 2016-03-15 | 2022-10-18 | Hamilton Sundstrand Corporation | Engine bleed system with motorized compressor |
US10794295B2 (en) * | 2016-03-15 | 2020-10-06 | Hamilton Sunstrand Corporation | Engine bleed system with multi-tap bleed array |
US20170268430A1 (en) * | 2016-03-15 | 2017-09-21 | Hamilton Sundstrand Corporation | Engine bleed system with turbo-compressor |
CN106089438A (zh) * | 2016-06-16 | 2016-11-09 | 电子科技大学 | 一种微型温差发电装置及其在小型发动机能量回收上的应用方法 |
EP3478581B1 (en) * | 2016-06-30 | 2021-04-28 | Bombardier Inc. | Assembly and method for conditioning engine-heated air onboard an aircraft |
US10919637B2 (en) | 2016-07-12 | 2021-02-16 | Hamilton Sunstrand Corporation | Temperature control system for fuel tank inerting system |
US10267334B2 (en) * | 2016-08-01 | 2019-04-23 | United Technologies Corporation | Annular heatshield |
US10931170B2 (en) | 2017-05-10 | 2021-02-23 | Hamilton Sundstrand Corporation | Motor cooling utilizing cabin air |
US10711693B2 (en) | 2017-07-12 | 2020-07-14 | General Electric Company | Gas turbine engine with an engine rotor element turning device |
CN108045587B (zh) * | 2017-12-26 | 2023-07-11 | 南京航空航天大学 | 基于温差发电技术的耗氧型惰化燃油箱废热回收系统 |
CN108843460A (zh) * | 2018-06-28 | 2018-11-20 | 厦门大学 | 涡轮冲压组合发动机预冷热电转换及增推方法 |
EP4276017A1 (en) * | 2022-05-10 | 2023-11-15 | Airbus SAS | Fluid transport device and method for manufacturing a fluid transport device |
CN117360779B (zh) * | 2023-12-08 | 2024-02-23 | 中国航空工业集团公司金城南京机电液压工程研究中心 | 一种燃油作为动力源和热沉的电热互补系统 |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4819425A (en) * | 1982-03-18 | 1989-04-11 | The Boeing Company | Primary-secondary ventilated flow mixer nozzle for high bypass turbo fan jet propulsion system |
US6100463A (en) * | 1997-11-18 | 2000-08-08 | The Boeing Company | Method for making advanced thermoelectric devices |
JP2001071999A (ja) * | 1999-09-06 | 2001-03-21 | Shimadzu Corp | 航空機用空気調和装置 |
JP2002130860A (ja) * | 2000-10-18 | 2002-05-09 | Shimadzu Corp | 空気調和装置 |
US6782701B2 (en) | 2003-01-22 | 2004-08-31 | Honeywell International Inc. | Master-slave engine bleed flow sharing control method and system |
US20050022855A1 (en) | 2003-07-30 | 2005-02-03 | Raver Bernard J. | Thermoelectric power generator for a gas turbine engine |
US7152635B2 (en) * | 2004-02-10 | 2006-12-26 | The Boeing Company | Commercial aircraft on-board inerting system |
US7013636B2 (en) * | 2004-04-22 | 2006-03-21 | The Boeing Company | System and method for controlling the temperature and infrared signature of an engine |
DE102004038860A1 (de) * | 2004-08-10 | 2006-02-23 | Airbus Deutschland Gmbh | System zur Erzeugung von Prozessluft |
WO2007098847A1 (de) * | 2006-02-28 | 2007-09-07 | Bayerische Motoren Werke Aktiengesellschaft | Kraftfahrzeug mit einem mit tiefkalt gespeichertem kraftstoff betriebenen aggregat |
ATE492331T1 (de) | 2006-09-08 | 2011-01-15 | Parker Filtration & Separation B V | Verwendung eines ozonumwandlungsmittels zur inertisierung von flugzeugkraftstoffbehälter |
DE102007019820B4 (de) * | 2007-04-26 | 2012-03-08 | Airbus Operations Gmbh | Kühlsystem durch Grenzschichtabsaugung |
US8127555B2 (en) | 2007-12-13 | 2012-03-06 | Pratt & Whitney Rocketdyne, Inc. | Flowpath heat exchanger for thermal management and power generation within a hypersonic vehicle |
US9018512B2 (en) | 2007-12-21 | 2015-04-28 | The Boeing Company | Thermoelectric generation system |
US20100011781A1 (en) | 2008-07-21 | 2010-01-21 | Lents Charles E | Heat exchanger assembly for an aircraft control |
-
2009
- 2009-12-07 US US12/632,250 patent/US8484983B2/en active Active
-
2010
- 2010-10-21 JP JP2012542013A patent/JP5965320B2/ja active Active
- 2010-10-21 EP EP10771858.7A patent/EP2509869B1/en active Active
- 2010-10-21 WO PCT/US2010/053622 patent/WO2011071602A2/en active Application Filing
- 2010-10-21 CN CN201080055524.0A patent/CN102648127B/zh active Active
- 2010-10-21 CA CA2782972A patent/CA2782972C/en active Active
Also Published As
Publication number | Publication date |
---|---|
CN102648127A (zh) | 2012-08-22 |
CA2782972A1 (en) | 2011-06-16 |
WO2011071602A3 (en) | 2011-08-18 |
JP2013512821A (ja) | 2013-04-18 |
US8484983B2 (en) | 2013-07-16 |
EP2509869B1 (en) | 2016-08-24 |
US20110131999A1 (en) | 2011-06-09 |
EP2509869A2 (en) | 2012-10-17 |
CA2782972C (en) | 2017-11-21 |
WO2011071602A2 (en) | 2011-06-16 |
CN102648127B (zh) | 2015-09-30 |
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