JP2018150829A5 - - Google Patents

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Publication number
JP2018150829A5
JP2018150829A5 JP2017045927A JP2017045927A JP2018150829A5 JP 2018150829 A5 JP2018150829 A5 JP 2018150829A5 JP 2017045927 A JP2017045927 A JP 2017045927A JP 2017045927 A JP2017045927 A JP 2017045927A JP 2018150829 A5 JP2018150829 A5 JP 2018150829A5
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JP
Japan
Prior art keywords
cooling
adjacent
rib
wall
lattice
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Application number
JP2017045927A
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English (en)
Japanese (ja)
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JP6860383B2 (ja
JP2018150829A (ja
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Publication date
Application filed filed Critical
Priority claimed from JP2017045927A external-priority patent/JP6860383B2/ja
Priority to JP2017045927A priority Critical patent/JP6860383B2/ja
Priority to DE112018001266.2T priority patent/DE112018001266B4/de
Priority to CN201880014034.2A priority patent/CN110337530B/zh
Priority to GB1912924.6A priority patent/GB2574951B/en
Priority to PCT/JP2018/008645 priority patent/WO2018164150A1/ja
Publication of JP2018150829A publication Critical patent/JP2018150829A/ja
Priority to US16/558,706 priority patent/US11384644B2/en
Publication of JP2018150829A5 publication Critical patent/JP2018150829A5/ja
Publication of JP6860383B2 publication Critical patent/JP6860383B2/ja
Application granted granted Critical
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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JP2017045927A 2017-03-10 2017-03-10 タービン翼の冷却構造 Active JP6860383B2 (ja)

Priority Applications (6)

Application Number Priority Date Filing Date Title
JP2017045927A JP6860383B2 (ja) 2017-03-10 2017-03-10 タービン翼の冷却構造
PCT/JP2018/008645 WO2018164150A1 (ja) 2017-03-10 2018-03-06 タービン翼の冷却構造
CN201880014034.2A CN110337530B (zh) 2017-03-10 2018-03-06 涡轮叶片的冷却结构
GB1912924.6A GB2574951B (en) 2017-03-10 2018-03-06 Cooling structure for turbine airfoil
DE112018001266.2T DE112018001266B4 (de) 2017-03-10 2018-03-06 Kühlstruktur für turbinenschaufel
US16/558,706 US11384644B2 (en) 2017-03-10 2019-09-03 Cooling structure for turbine airfoil

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2017045927A JP6860383B2 (ja) 2017-03-10 2017-03-10 タービン翼の冷却構造

Publications (3)

Publication Number Publication Date
JP2018150829A JP2018150829A (ja) 2018-09-27
JP2018150829A5 true JP2018150829A5 (enExample) 2020-03-19
JP6860383B2 JP6860383B2 (ja) 2021-04-14

Family

ID=63447846

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2017045927A Active JP6860383B2 (ja) 2017-03-10 2017-03-10 タービン翼の冷却構造

Country Status (6)

Country Link
US (1) US11384644B2 (enExample)
JP (1) JP6860383B2 (enExample)
CN (1) CN110337530B (enExample)
DE (1) DE112018001266B4 (enExample)
GB (1) GB2574951B (enExample)
WO (1) WO2018164150A1 (enExample)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11248471B2 (en) * 2020-01-22 2022-02-15 General Electric Company Turbine rotor blade with angel wing with coolant transfer passage between adjacent wheel space portions by additive manufacture
CN113623011B (zh) * 2021-07-13 2022-11-29 哈尔滨工业大学 涡轮叶片
CN113623010B (zh) * 2021-07-13 2022-11-29 哈尔滨工业大学 涡轮叶片
US11674446B2 (en) * 2021-08-30 2023-06-13 Collins Engine Nozzles, Inc. Cooling for surface ignitors in torch ignition devices
US11674445B2 (en) * 2021-08-30 2023-06-13 Collins Engine Nozzles, Inc. Cooling for continuous ignition devices
CN114872909B (zh) * 2022-05-06 2023-03-24 中国航发四川燃气涡轮研究院 飞机型涡轮叶片冷却通道换热结构

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4407632A (en) * 1981-06-26 1983-10-04 United Technologies Corporation Airfoil pedestaled trailing edge region cooling configuration
US5603606A (en) 1994-11-14 1997-02-18 Solar Turbines Incorporated Turbine cooling system
JP4957131B2 (ja) * 2006-09-06 2012-06-20 株式会社Ｉｈｉ 冷却構造
CN100557199C (zh) * 2007-07-13 2009-11-04 北京航空航天大学 一种适用于涡轮叶片等内冷部件中的渐宽型开槽交错肋通道
JP2011085084A (ja) * 2009-10-16 2011-04-28 Ihi Corp タービン翼
EP2418357A1 (en) * 2010-08-05 2012-02-15 Siemens Aktiengesellschaft Turbine airfoil and method for thermal barrier coating
CN102116178A (zh) * 2011-01-18 2011-07-06 中国科学院工程热物理研究所 一种气冷涡轮的双射流孔冷却结构
CN102102543B (zh) * 2011-03-11 2013-05-15 北京华清燃气轮机与煤气化联合循环工程技术有限公司 燃气轮机的涡轮转子叶片
RU2014125561A (ru) * 2011-11-25 2015-12-27 Сименс Акциенгезелльшафт Аэродинамический профиль с охлаждающими каналами
JP6036424B2 (ja) * 2013-03-14 2016-11-30 株式会社Ihi 冷却促進構造
US9464528B2 (en) 2013-06-14 2016-10-11 Solar Turbines Incorporated Cooled turbine blade with double compound angled holes and slots
WO2015147672A1 (en) * 2014-03-27 2015-10-01 Siemens Aktiengesellschaft Blade for a gas turbine and method of cooling the blade
GB2533315B (en) * 2014-12-16 2017-04-12 Rolls Royce Plc Cooling of engine components
JP2016125380A (ja) * 2014-12-26 2016-07-11 川崎重工業株式会社 タービン翼の冷却構造

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