FR2981637B1 - THERMAL PRODUCTION SYSTEM OF ELECTRICITY FOR AIRCRAFT - Google Patents

THERMAL PRODUCTION SYSTEM OF ELECTRICITY FOR AIRCRAFT

Info

Publication number
FR2981637B1
FR2981637B1 FR1259978A FR1259978A FR2981637B1 FR 2981637 B1 FR2981637 B1 FR 2981637B1 FR 1259978 A FR1259978 A FR 1259978A FR 1259978 A FR1259978 A FR 1259978A FR 2981637 B1 FR2981637 B1 FR 2981637B1
Authority
FR
France
Prior art keywords
aircraft
electricity
production system
thermal production
thermal
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
FR1259978A
Other languages
French (fr)
Other versions
FR2981637A1 (en
Inventor
Adrian Shipley
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.)
GE Aviation Systems Ltd
Original Assignee
GE Aviation Systems Ltd
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 GE Aviation Systems Ltd filed Critical GE Aviation Systems Ltd
Publication of FR2981637A1 publication Critical patent/FR2981637A1/en
Application granted granted Critical
Publication of FR2981637B1 publication Critical patent/FR2981637B1/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
    • 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
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/18—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use using the waste heat of gas-turbine plants outside the plants themselves, e.g. gas-turbine power heat plants
    • H—ELECTRICITY
    • H10—SEMICONDUCTOR DEVICES; ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
    • H10N—ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
    • H10N10/00—Thermoelectric devices comprising a junction of dissimilar materials, i.e. devices exhibiting Seebeck or Peltier effects
    • H10N10/10—Thermoelectric devices comprising a junction of dissimilar materials, i.e. devices exhibiting Seebeck or Peltier effects operating with only the Peltier or Seebeck effects
    • H—ELECTRICITY
    • H10—SEMICONDUCTOR DEVICES; ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
    • H10N—ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
    • H10N10/00—Thermoelectric devices comprising a junction of dissimilar materials, i.e. devices exhibiting Seebeck or Peltier effects
    • H10N10/10—Thermoelectric devices comprising a junction of dissimilar materials, i.e. devices exhibiting Seebeck or Peltier effects operating with only the Peltier or Seebeck effects
    • H10N10/17—Thermoelectric devices comprising a junction of dissimilar materials, i.e. devices exhibiting Seebeck or Peltier effects operating with only the Peltier or Seebeck effects characterised by the structure or configuration of the cell or thermocouple forming the device
    • 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
    • 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)
  • Engine Equipment That Uses Special Cycles (AREA)
  • Hybrid Cells (AREA)
FR1259978A 2011-10-24 2012-10-19 THERMAL PRODUCTION SYSTEM OF ELECTRICITY FOR AIRCRAFT Active FR2981637B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1118313.4A GB2496839A (en) 2011-10-24 2011-10-24 Thermal electrical power generation for aircraft

Publications (2)

Publication Number Publication Date
FR2981637A1 FR2981637A1 (en) 2013-04-26
FR2981637B1 true FR2981637B1 (en) 2016-12-09

Family

ID=45373306

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1259978A Active FR2981637B1 (en) 2011-10-24 2012-10-19 THERMAL PRODUCTION SYSTEM OF ELECTRICITY FOR AIRCRAFT

Country Status (7)

Country Link
JP (1) JP2013091487A (en)
CN (1) CN103061856A (en)
BR (1) BR102012025929A2 (en)
CA (1) CA2792589A1 (en)
DE (1) DE102012109992A1 (en)
FR (1) FR2981637B1 (en)
GB (1) GB2496839A (en)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2014135171A1 (en) * 2013-03-07 2014-09-12 Atta Moustafa Mahmoud Abd El-Daym New source of electric power for aircraft
JP5832697B2 (en) * 2013-03-27 2015-12-16 Ｊｆｅスチール株式会社 Thermoelectric power generation apparatus and thermoelectric power generation method using the same
US20140360547A1 (en) * 2013-06-06 2014-12-11 Hamilton Sundstrand Corporation Energy recovery and regeneration system
US9666781B2 (en) * 2013-08-19 2017-05-30 The Boeing Company Methods for recovering waste energy from bleed air ducts
CN104092409A (en) * 2014-07-17 2014-10-08 北京航空航天大学 Combined thermoelectric conversion device
US10291156B2 (en) 2015-10-30 2019-05-14 Ge Aviation Systems Llc Combined hybrid thermionic and thermoelectric generator
CN105281607A (en) * 2015-11-16 2016-01-27 滨州学院 Hot waste water generator
CN105515448A (en) * 2016-01-19 2016-04-20 哈尔滨工业大学 Hypersonic speed aircraft skin cooling and semiconductor thermoelectric power generation integrated system
DE102016107303A1 (en) * 2016-04-20 2017-10-26 Rolls-Royce Deutschland Ltd & Co Kg Energy conversion system of a turbomachine, transmission or bearing housing of a turbomachine and turbomachinery
CN108768212B (en) * 2018-06-12 2020-03-17 西安交通大学 Energy recovery device of underwater vehicle
DE102018116155A1 (en) * 2018-07-04 2020-01-09 Dr. Ing. H.C. F. Porsche Aktiengesellschaft aircraft
CN113014144B (en) * 2021-04-12 2023-03-21 西北工业大学 Forced cooling thermoelectric power generation system of miniature turbojet engine

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2001023666A (en) * 1999-07-08 2001-01-26 Toyota Motor Corp Waste heat recovering device and its control method
JP2001082166A (en) * 1999-09-13 2001-03-27 Toyota Motor Corp Electric power generating device
JP2001082167A (en) * 1999-09-13 2001-03-27 Toyota Motor Corp Power generating device
JP2002257313A (en) * 2001-02-27 2002-09-11 Tokyo Gas Co Ltd Combustible gas treatment system
US20050022855A1 (en) * 2003-07-30 2005-02-03 Raver Bernard J. Thermoelectric power generator for a gas turbine engine
US8481843B2 (en) * 2003-09-12 2013-07-09 Board Of Trustees Operating Michigan State University Silver-containing p-type semiconductor
CN100452466C (en) * 2003-09-12 2009-01-14 密歇根州州立大学托管委员会 Silver-containing p-type semiconductor
US8313056B2 (en) * 2005-07-19 2012-11-20 United Technologies Corporation Engine heat exchanger with thermoelectric generation
US20070277866A1 (en) * 2006-05-31 2007-12-06 General Electric Company Thermoelectric nanotube arrays
US7488888B2 (en) * 2006-09-15 2009-02-10 The Boeing Company Energy harvesting devices
GB2447333B (en) * 2007-03-09 2009-02-18 Boeing Co Energy harvesting devices
DE102007036930A1 (en) * 2007-08-04 2009-04-09 Mtu Aero Engines Gmbh Gas-turbine engine e.g. civilian aircraft engine or military aircraft engine, has thermoelectric generator generating electrical energy from temperature difference between hot current via core engine and cold current via bypass channel
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
US8453456B2 (en) * 2009-03-25 2013-06-04 United Technologies Corporation Fuel-cooled flexible heat exchanger with thermoelectric device compression
JP4878382B2 (en) * 2009-05-14 2012-02-15 独立行政法人 宇宙航空研究開発機構 Solar thermal collector in solar combined power generation system and solar thermal power generation module using the solar thermal collector
US8568938B2 (en) * 2009-08-28 2013-10-29 The Boeing Company Thermoelectric generator and fuel cell for electric power co-generation
US8484983B2 (en) * 2009-12-07 2013-07-16 The Boeing Company Thermoelectric generator on an aircraft bleed system
DE102009058156B4 (en) * 2009-12-15 2014-11-13 Mann + Hummel Gmbh Cooling device in a vehicle

Also Published As

Publication number Publication date
BR102012025929A2 (en) 2014-03-18
JP2013091487A (en) 2013-05-16
DE102012109992A1 (en) 2013-04-25
CA2792589A1 (en) 2013-04-24
GB2496839A (en) 2013-05-29
CN103061856A (en) 2013-04-24
FR2981637A1 (en) 2013-04-26
GB201118313D0 (en) 2011-12-07

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