JP2015040566A5 - - Google Patents

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Publication number
JP2015040566A5
JP2015040566A5 JP2014164625A JP2014164625A JP2015040566A5 JP 2015040566 A5 JP2015040566 A5 JP 2015040566A5 JP 2014164625 A JP2014164625 A JP 2014164625A JP 2014164625 A JP2014164625 A JP 2014164625A JP 2015040566 A5 JP2015040566 A5 JP 2015040566A5
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JP
Japan
Prior art keywords
outlet opening
angel wing
shank
cooling
cooling passage
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
JP2014164625A
Other languages
English (en)
Japanese (ja)
Other versions
JP2015040566A (ja
JP6506514B2 (ja
Filing date
Publication date
Priority claimed from US13/972,667 external-priority patent/US9528377B2/en
Application filed filed Critical
Publication of JP2015040566A publication Critical patent/JP2015040566A/ja
Publication of JP2015040566A5 publication Critical patent/JP2015040566A5/ja
Application granted granted Critical
Publication of JP6506514B2 publication Critical patent/JP6506514B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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JP2014164625A 2013-08-21 2014-08-13 動翼エンジェルウイングを冷却する方法およびシステム Active JP6506514B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/972,667 US9528377B2 (en) 2013-08-21 2013-08-21 Method and system for cooling rotor blade angelwings
US13/972,667 2013-08-21

Publications (3)

Publication Number Publication Date
JP2015040566A JP2015040566A (ja) 2015-03-02
JP2015040566A5 true JP2015040566A5 (enExample) 2017-09-14
JP6506514B2 JP6506514B2 (ja) 2019-04-24

Family

ID=52446906

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2014164625A Active JP6506514B2 (ja) 2013-08-21 2014-08-13 動翼エンジェルウイングを冷却する方法およびシステム

Country Status (5)

Country Link
US (1) US9528377B2 (enExample)
JP (1) JP6506514B2 (enExample)
CN (1) CN104420892B (enExample)
CH (1) CH708487A2 (enExample)
DE (1) DE102014111510A1 (enExample)

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB201016423D0 (en) * 2010-09-30 2010-11-17 Rolls Royce Plc Cooled rotor blade
US20160146016A1 (en) * 2014-11-24 2016-05-26 General Electric Company Rotor rim impingement cooling
EP3043024A1 (en) * 2015-01-09 2016-07-13 Siemens Aktiengesellschaft Blade platform cooling and corresponding gas turbine
US10066488B2 (en) * 2015-12-01 2018-09-04 General Electric Company Turbomachine blade with generally radial cooling conduit to wheel space
CN105626157B (zh) * 2016-03-02 2017-03-01 哈尔滨工程大学 一种包括自适应喷气孔的多重轮缘密封结构的涡轮
EP3232000A1 (de) * 2016-04-15 2017-10-18 Siemens Aktiengesellschaft Plattform einer laufschaufel mit filmkühlungsöffnungen an der plattform und zugehörige strömugsmaschine
JP7019331B2 (ja) * 2016-07-22 2022-02-15 ゼネラル・エレクトリック・カンパニイ タービンバケット冷却
US10247015B2 (en) * 2017-01-13 2019-04-02 Rolls-Royce Corporation Cooled blisk with dual wall blades for gas turbine engine
US10934865B2 (en) * 2017-01-13 2021-03-02 Rolls-Royce Corporation Cooled single walled blisk for gas turbine engine
US20180216467A1 (en) * 2017-02-02 2018-08-02 General Electric Company Turbine engine with an extension into a buffer cavity
US10683765B2 (en) * 2017-02-14 2020-06-16 General Electric Company Turbine blades having shank features and methods of fabricating the same
KR101958109B1 (ko) * 2017-09-15 2019-03-13 두산중공업 주식회사 가스 터빈
US10968750B2 (en) 2018-09-04 2021-04-06 General Electric Company Component for a turbine engine with a hollow pin
FR3099786B1 (fr) * 2019-08-07 2021-07-30 Safran Helicopter Engines Aube mobile pour une roue d’une turbomachine
US11492908B2 (en) 2020-01-22 2022-11-08 General Electric Company Turbine rotor blade root with hollow mount with lattice support structure by additive manufacture
US11220916B2 (en) 2020-01-22 2022-01-11 General Electric Company Turbine rotor blade with platform with non-linear cooling passages by additive manufacture
US11242760B2 (en) 2020-01-22 2022-02-08 General Electric Company Turbine rotor blade with integral impingement sleeve by additive manufacture
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
CN114109517A (zh) * 2021-11-19 2022-03-01 华能国际电力股份有限公司 一种透平叶片伸出翼冷却和密封结构
CN114229015B (zh) * 2021-12-14 2025-05-13 杭州牧星科技有限公司 一种进气道

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6331097B1 (en) * 1999-09-30 2001-12-18 General Electric Company Method and apparatus for purging turbine wheel cavities
US6402471B1 (en) * 2000-11-03 2002-06-11 General Electric Company Turbine blade for gas turbine engine and method of cooling same
EP1306521A1 (de) * 2001-10-24 2003-05-02 Siemens Aktiengesellschaft Laufschaufel für eine Gasturbine und Gasturbine mit einer Anzahl von Laufschaufeln
US7549835B2 (en) 2006-07-07 2009-06-23 Siemens Energy, Inc. Leakage flow control and seal wear minimization system for a turbine engine
US8057157B2 (en) 2007-10-22 2011-11-15 General Electric Company System for delivering air from a multi-stage compressor to a turbine portion of a gas turbine engine
US8016297B2 (en) 2008-03-27 2011-09-13 United Technologies Corporation Gas turbine engine seals and engines incorporating such seals
US8057178B2 (en) * 2008-09-04 2011-11-15 General Electric Company Turbine bucket for a turbomachine and method of reducing bow wave effects at a turbine bucket
US8038399B1 (en) 2008-11-22 2011-10-18 Florida Turbine Technologies, Inc. Turbine rim cavity sealing
US7993102B2 (en) 2009-01-09 2011-08-09 General Electric Company Rotor cooling circuit
US8277177B2 (en) 2009-01-19 2012-10-02 Siemens Energy, Inc. Fluidic rim seal system for turbine engines
US8186933B2 (en) 2009-03-24 2012-05-29 General Electric Company Systems, methods, and apparatus for passive purge flow control in a turbine
US8529194B2 (en) * 2010-05-19 2013-09-10 General Electric Company Shank cavity and cooling hole
GB201016423D0 (en) * 2010-09-30 2010-11-17 Rolls Royce Plc Cooled rotor blade
US8979481B2 (en) * 2011-10-26 2015-03-17 General Electric Company Turbine bucket angel wing features for forward cavity flow control and related method
US20130170983A1 (en) * 2012-01-04 2013-07-04 General Electric Company Turbine assembly and method for reducing fluid flow between turbine components

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