JP2013512821A5 - - Google Patents

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Publication number
JP2013512821A5
JP2013512821A5 JP2012542013A JP2012542013A JP2013512821A5 JP 2013512821 A5 JP2013512821 A5 JP 2013512821A5 JP 2012542013 A JP2012542013 A JP 2012542013A JP 2012542013 A JP2012542013 A JP 2012542013A JP 2013512821 A5 JP2013512821 A5 JP 2013512821A5
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JP
Japan
Prior art keywords
air
bleed
ram
bleed air
thermoelectric generator
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.)
Granted
Application number
JP2012542013A
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English (en)
Japanese (ja)
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JP2013512821A (ja
JP5965320B2 (ja
Filing date
Publication date
Priority claimed from US12/632,250 external-priority patent/US8484983B2/en
Application filed filed Critical
Publication of JP2013512821A publication Critical patent/JP2013512821A/ja
Publication of JP2013512821A5 publication Critical patent/JP2013512821A5/ja
Application granted granted Critical
Publication of JP5965320B2 publication Critical patent/JP5965320B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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JP2012542013A 2009-12-07 2010-10-21 航空機ブリードシステムの熱電発電機 Active JP5965320B2 (ja)

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 true JP2013512821A5 (enExample) 2013-11-07
JP5965320B2 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)

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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
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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
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