JP2021050688A5 - - Google Patents

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Publication number
JP2021050688A5
JP2021050688A5 JP2019175092A JP2019175092A JP2021050688A5 JP 2021050688 A5 JP2021050688 A5 JP 2021050688A5 JP 2019175092 A JP2019175092 A JP 2019175092A JP 2019175092 A JP2019175092 A JP 2019175092A JP 2021050688 A5 JP2021050688 A5 JP 2021050688A5
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JP
Japan
Prior art keywords
edge portion
side edge
turbine blade
wall surface
lattice
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
JP2019175092A
Other languages
English (en)
Japanese (ja)
Other versions
JP7681382B2 (ja
JP2021050688A (ja
Filing date
Publication date
Application filed filed Critical
Priority claimed from JP2019175092A external-priority patent/JP7681382B2/ja
Priority to JP2019175092A priority Critical patent/JP7681382B2/ja
Priority to DE112020004602.8T priority patent/DE112020004602B4/de
Priority to CN202080067343.3A priority patent/CN114450466B/zh
Priority to PCT/JP2020/034988 priority patent/WO2021060093A1/ja
Priority to GB2203943.2A priority patent/GB2603338B/en
Publication of JP2021050688A publication Critical patent/JP2021050688A/ja
Priority to US17/702,914 priority patent/US11708763B2/en
Publication of JP2021050688A5 publication Critical patent/JP2021050688A5/ja
Publication of JP7681382B2 publication Critical patent/JP7681382B2/ja
Application granted granted Critical
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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JP2019175092A 2019-09-26 2019-09-26 タービン翼 Active JP7681382B2 (ja)

Priority Applications (6)

Application Number Priority Date Filing Date Title
JP2019175092A JP7681382B2 (ja) 2019-09-26 2019-09-26 タービン翼
GB2203943.2A GB2603338B (en) 2019-09-26 2020-09-15 Turbine Airfoil
CN202080067343.3A CN114450466B (zh) 2019-09-26 2020-09-15 涡轮叶片
PCT/JP2020/034988 WO2021060093A1 (ja) 2019-09-26 2020-09-15 タービン翼
DE112020004602.8T DE112020004602B4 (de) 2019-09-26 2020-09-15 Turbinenflügel
US17/702,914 US11708763B2 (en) 2019-09-26 2022-03-24 Turbine airfoil

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2019175092A JP7681382B2 (ja) 2019-09-26 2019-09-26 タービン翼

Publications (3)

Publication Number Publication Date
JP2021050688A JP2021050688A (ja) 2021-04-01
JP2021050688A5 true JP2021050688A5 (enExample) 2022-06-24
JP7681382B2 JP7681382B2 (ja) 2025-05-22

Family

ID=75157408

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2019175092A Active JP7681382B2 (ja) 2019-09-26 2019-09-26 タービン翼

Country Status (6)

Country Link
US (1) US11708763B2 (enExample)
JP (1) JP7681382B2 (enExample)
CN (1) CN114450466B (enExample)
DE (1) DE112020004602B4 (enExample)
GB (1) GB2603338B (enExample)
WO (1) WO2021060093A1 (enExample)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113623010B (zh) * 2021-07-13 2022-11-29 哈尔滨工业大学 涡轮叶片
WO2023286206A1 (ja) * 2021-07-14 2023-01-19 ヤマハ発動機株式会社 筐体
WO2023286624A1 (ja) * 2021-07-14 2023-01-19 ヤマハ発動機株式会社 筐体具備装置
WO2023286205A1 (ja) * 2021-07-14 2023-01-19 ヤマハ発動機株式会社 筐体

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1404757A (en) * 1971-08-25 1975-09-03 Rolls Royce Gas turbine engine blades
US5603606A (en) 1994-11-14 1997-02-18 Solar Turbines Incorporated Turbine cooling system
SE512384C2 (sv) * 1998-05-25 2000-03-06 Abb Ab Komponent för en gasturbin
SE526847C2 (sv) * 2004-02-27 2005-11-08 Demag Delaval Ind Turbomachine En komponent som innefattar en ledskena eller ett rotorblad för en gasturbin
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
JP2009221995A (ja) * 2008-03-18 2009-10-01 Ihi Corp 高温部品の内面冷却構造
EP2378073A1 (en) 2010-04-14 2011-10-19 Siemens Aktiengesellschaft Blade or vane for a turbomachine
US20130230379A1 (en) 2012-03-01 2013-09-05 General Electric Company Rotating turbomachine component having a tip leakage flow guide
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
US10247015B2 (en) * 2017-01-13 2019-04-02 Rolls-Royce Corporation Cooled blisk with dual wall blades for gas turbine engine
JP6898104B2 (ja) * 2017-01-18 2021-07-07 川崎重工業株式会社 タービン翼の冷却構造
JP6906332B2 (ja) 2017-03-10 2021-07-21 川崎重工業株式会社 タービン翼の冷却構造
JP2018150828A (ja) 2017-03-10 2018-09-27 川崎重工業株式会社 タービン翼の冷却構造
US10895157B2 (en) * 2017-04-24 2021-01-19 Honeywell International Inc. Gas turbine engine components with air-cooling features, and related methods of manufacturing the same
JP2019175092A (ja) 2018-03-28 2019-10-10 三菱プレシジョン株式会社 Icカードリーダシステム

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