CA2782972C - Thermoelectric generator on an aircraft bleed system - Google Patents

Thermoelectric generator on an aircraft bleed system Download PDF

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Publication number
CA2782972C
CA2782972C CA2782972A CA2782972A CA2782972C CA 2782972 C CA2782972 C CA 2782972C CA 2782972 A CA2782972 A CA 2782972A CA 2782972 A CA2782972 A CA 2782972A CA 2782972 C CA2782972 C CA 2782972C
Authority
CA
Canada
Prior art keywords
air
bleed
bleed air
ram
thermoelectric
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
CA2782972A
Other languages
English (en)
French (fr)
Other versions
CA2782972A1 (en
Inventor
Lijun Gao
Liu Shengyi
Chin-Hsi Chien
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.)
Boeing Co
Original Assignee
Boeing Co
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 Boeing Co filed Critical Boeing Co
Publication of CA2782972A1 publication Critical patent/CA2782972A1/en
Application granted granted Critical
Publication of CA2782972C publication Critical patent/CA2782972C/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

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
    • 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)
CA2782972A 2009-12-07 2010-10-21 Thermoelectric generator on an aircraft bleed system Active CA2782972C (en)

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 (2)

Publication Number Publication Date
CA2782972A1 CA2782972A1 (en) 2011-06-16
CA2782972C true CA2782972C (en) 2017-11-21

Family

ID=44063309

Family Applications (1)

Application Number Title Priority Date Filing Date
CA2782972A Active CA2782972C (en) 2009-12-07 2010-10-21 Thermoelectric generator on an aircraft bleed system

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)

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US9470153B2 (en) * 2011-10-05 2016-10-18 United Technologies Corporation Combined pump system for engine TMS AOC reduction and ECS loss elimination
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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

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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
JP2013512821A (ja) 2013-04-18
US8484983B2 (en) 2013-07-16
JP5965320B2 (ja) 2016-08-03
EP2509869A2 (en) 2012-10-17
CN102648127B (zh) 2015-09-30

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Effective date: 20150722