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
- Authority
- JP
- Japan
- 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.)
- Active
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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; 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
-
- 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
- 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; 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
- 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; 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
- B64D2013/0685—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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Health & Medical Sciences (AREA)
- General Health & Medical Sciences (AREA)
- Pulmonology (AREA)
- Separation By Low-Temperature Treatments (AREA)
- Motor Or Generator Cooling System (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
- Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
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 (enExample) | 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 (enExample) |
| EP (1) | EP2509869B1 (enExample) |
| JP (1) | JP5965320B2 (enExample) |
| CN (1) | CN102648127B (enExample) |
| CA (1) | CA2782972C (enExample) |
| WO (1) | WO2011071602A2 (enExample) |
Families Citing this family (42)
| 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 |
| CN104870312B (zh) * | 2012-12-28 | 2019-06-18 | 通用电气公司 | 用于航空电功率产生的系统和方法 |
| 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 |
| US10247100B2 (en) * | 2014-07-03 | 2019-04-02 | General Electric Company | Jet engine cold air cooling system |
| 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 |
| 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 |
| US11473497B2 (en) | 2016-03-15 | 2022-10-18 | Hamilton Sundstrand Corporation | Engine bleed system with motorized 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 |
| CA3028989A1 (en) * | 2016-06-30 | 2018-01-04 | 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 |
| CN114435597B (zh) * | 2022-01-25 | 2024-04-26 | 山东大学 | 用于机翼防除冰组件的温差发电装置、防除冰组件及方法 |
| EP4276017A1 (en) * | 2022-05-10 | 2023-11-15 | Airbus SAS | Fluid transport device and method for manufacturing a fluid transport device |
| CN115473261A (zh) * | 2022-08-12 | 2022-12-13 | 江苏航空职业技术学院 | 一种基于追踪控制器的航空网温差发电系统及追踪控制方法 |
| GB202214249D0 (en) | 2022-09-29 | 2022-11-16 | Rolls Royce Plc | A gas turbine engine |
| US12473093B2 (en) | 2023-06-30 | 2025-11-18 | Hamilton Sundstrand Corporation | Outflow energy recovery system |
| 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 |
| US12428988B1 (en) * | 2024-08-16 | 2025-09-30 | General Electric Company | High temperature anti-ice systems for aircraft engines |
| US12435668B1 (en) | 2024-11-01 | 2025-10-07 | General Electric Company | Methods and apparatus for anti-ice heat supply from waste heat recovery systems |
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 |
| ES2358484T3 (es) | 2006-09-08 | 2011-05-11 | PARKER FILTRATION & SEPARATION B.V. | Utilización de un medio de conversión de ozono para la inertización de un depósito de combustible de aeronave. |
| 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 CA CA2782972A patent/CA2782972C/en active Active
- 2010-10-21 EP EP10771858.7A patent/EP2509869B1/en active Active
- 2010-10-21 JP JP2012542013A patent/JP5965320B2/ja active Active
- 2010-10-21 CN CN201080055524.0A patent/CN102648127B/zh active Active
- 2010-10-21 WO PCT/US2010/053622 patent/WO2011071602A2/en not_active Ceased
Also Published As
| Publication number | Publication date |
|---|---|
| US20110131999A1 (en) | 2011-06-09 |
| WO2011071602A3 (en) | 2011-08-18 |
| CA2782972A1 (en) | 2011-06-16 |
| WO2011071602A2 (en) | 2011-06-16 |
| CN102648127A (zh) | 2012-08-22 |
| EP2509869B1 (en) | 2016-08-24 |
| CA2782972C (en) | 2017-11-21 |
| JP2013512821A (ja) | 2013-04-18 |
| US8484983B2 (en) | 2013-07-16 |
| EP2509869A2 (en) | 2012-10-17 |
| CN102648127B (zh) | 2015-09-30 |
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