JP2019173595A5 - - Google Patents

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Publication number
JP2019173595A5
JP2019173595A5 JP2018060015A JP2018060015A JP2019173595A5 JP 2019173595 A5 JP2019173595 A5 JP 2019173595A5 JP 2018060015 A JP2018060015 A JP 2018060015A JP 2018060015 A JP2018060015 A JP 2018060015A JP 2019173595 A5 JP2019173595 A5 JP 2019173595A5
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JP
Japan
Prior art keywords
cooling
ventral
wall
dorsal
side opening
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JP2018060015A
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English (en)
Japanese (ja)
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JP7093658B2 (ja
JP2019173595A (ja
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Priority claimed from JP2018060015A external-priority patent/JP7093658B2/ja
Priority to JP2018060015A priority Critical patent/JP7093658B2/ja
Priority to KR1020207026110A priority patent/KR102526809B1/ko
Priority to CN201980019689.3A priority patent/CN111936724B/zh
Priority to US16/981,387 priority patent/US11346231B2/en
Priority to DE112019000921.4T priority patent/DE112019000921B4/de
Priority to PCT/JP2019/011455 priority patent/WO2019188588A1/ja
Publication of JP2019173595A publication Critical patent/JP2019173595A/ja
Publication of JP2019173595A5 publication Critical patent/JP2019173595A5/ja
Publication of JP7093658B2 publication Critical patent/JP7093658B2/ja
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JP2018060015A 2018-03-27 2018-03-27 タービン動翼及びガスタービン Active JP7093658B2 (ja)

Priority Applications (6)

Application Number Priority Date Filing Date Title
JP2018060015A JP7093658B2 (ja) 2018-03-27 2018-03-27 タービン動翼及びガスタービン
DE112019000921.4T DE112019000921B4 (de) 2018-03-27 2019-03-19 Turbinenrotorschaufel und gasturbine
CN201980019689.3A CN111936724B (zh) 2018-03-27 2019-03-19 涡轮动叶以及燃气轮机
US16/981,387 US11346231B2 (en) 2018-03-27 2019-03-19 Turbine rotor blade and gas turbine
KR1020207026110A KR102526809B1 (ko) 2018-03-27 2019-03-19 터빈 동익 및 가스 터빈
PCT/JP2019/011455 WO2019188588A1 (ja) 2018-03-27 2019-03-19 タービン動翼及びガスタービン

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2018060015A JP7093658B2 (ja) 2018-03-27 2018-03-27 タービン動翼及びガスタービン

Publications (3)

Publication Number Publication Date
JP2019173595A JP2019173595A (ja) 2019-10-10
JP2019173595A5 true JP2019173595A5 (https=) 2021-04-15
JP7093658B2 JP7093658B2 (ja) 2022-06-30

Family

ID=68061619

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2018060015A Active JP7093658B2 (ja) 2018-03-27 2018-03-27 タービン動翼及びガスタービン

Country Status (6)

Country Link
US (1) US11346231B2 (https=)
JP (1) JP7093658B2 (https=)
KR (1) KR102526809B1 (https=)
CN (1) CN111936724B (https=)
DE (1) DE112019000921B4 (https=)
WO (1) WO2019188588A1 (https=)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SG11201607376VA (en) 2014-05-05 2016-12-29 Sulzer Management Ag Seal arrangement for a high-pressure pump and high-pressure pump having such a one
EP3974618B1 (en) * 2020-09-24 2023-04-19 Doosan Enerbility Co., Ltd. A technique for cooling squealer tip of a gas turbine blade
KR102466386B1 (ko) * 2020-09-25 2022-11-10 두산에너빌리티 주식회사 터빈 블레이드 및 이를 포함하는 터빈
US20250188843A1 (en) * 2022-08-24 2025-06-12 General Electric Company Turbine engine airfoil

Family Cites Families (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS62228603A (ja) * 1986-03-31 1987-10-07 Toshiba Corp ガスタ−ビンの翼
JPS6466401A (en) * 1987-09-07 1989-03-13 Toshiba Corp Turbine cooling blade
US5326224A (en) * 1991-03-01 1994-07-05 General Electric Company Cooling hole arrangements in jet engine components exposed to hot gas flow
JP3137527B2 (ja) * 1994-04-21 2001-02-26 三菱重工業株式会社 ガスタービン動翼チップ冷却装置
JPH1054203A (ja) * 1996-05-28 1998-02-24 Toshiba Corp 構造要素
US6092982A (en) * 1996-05-28 2000-07-25 Kabushiki Kaisha Toshiba Cooling system for a main body used in a gas stream
JPH10231703A (ja) 1997-02-17 1998-09-02 Toshiba Corp ガスタービンの翼
JPH11200805A (ja) * 1998-01-14 1999-07-27 Toshiba Corp 構造要素の冷却方法、冷却用流路付構造要素および冷却用流路付ガスタービン翼
US6491496B2 (en) * 2001-02-23 2002-12-10 General Electric Company Turbine airfoil with metering plates for refresher holes
US6494678B1 (en) * 2001-05-31 2002-12-17 General Electric Company Film cooled blade tip
JP4137508B2 (ja) 2002-05-02 2008-08-20 ゼネラル・エレクトリック・カンパニイ リフレッシュ用孔のメータリング板を備えるタービン翼形部
FR2885645A1 (fr) * 2005-05-13 2006-11-17 Snecma Moteurs Sa Aube creuse de rotor pour la turbine d'un moteur a turbine a gaz, equipee d'une baignoire
US7249934B2 (en) 2005-08-31 2007-07-31 General Electric Company Pattern cooled turbine airfoil
US7645122B1 (en) * 2006-12-01 2010-01-12 Florida Turbine Technologies, Inc. Turbine rotor blade with a nested parallel serpentine flow cooling circuit
US20100239409A1 (en) * 2009-03-18 2010-09-23 General Electric Company Method of Using and Reconstructing a Film-Cooling Augmentation Device for a Turbine Airfoil
US8684691B2 (en) * 2011-05-03 2014-04-01 Siemens Energy, Inc. Turbine blade with chamfered squealer tip and convective cooling holes
US8920124B2 (en) * 2013-02-14 2014-12-30 Siemens Energy, Inc. Turbine blade with contoured chamfered squealer tip
WO2014137686A1 (en) * 2013-03-04 2014-09-12 United Technologies Corporation Gas turbine engine high lift airfoil cooling in stagnation zone
JP6565105B2 (ja) 2015-09-29 2019-08-28 三菱日立パワーシステムズ株式会社 動翼及びこれを備えるガスタービン
US10605170B2 (en) * 2015-11-24 2020-03-31 General Electric Company Engine component with film cooling
US10227876B2 (en) 2015-12-07 2019-03-12 General Electric Company Fillet optimization for turbine airfoil
KR20190096569A (ko) * 2018-02-09 2019-08-20 두산중공업 주식회사 가스 터빈

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