JP2010509532A5 - - Google Patents

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Publication number
JP2010509532A5
JP2010509532A5 JP2009535648A JP2009535648A JP2010509532A5 JP 2010509532 A5 JP2010509532 A5 JP 2010509532A5 JP 2009535648 A JP2009535648 A JP 2009535648A JP 2009535648 A JP2009535648 A JP 2009535648A JP 2010509532 A5 JP2010509532 A5 JP 2010509532A5
Authority
JP
Japan
Prior art keywords
cooling
turbine blade
wall
wall portion
elements
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.)
Pending
Application number
JP2009535648A
Other languages
English (en)
Japanese (ja)
Other versions
JP2010509532A (ja
Filing date
Publication date
Priority claimed from EP06023274A external-priority patent/EP1921268A1/de
Application filed filed Critical
Publication of JP2010509532A publication Critical patent/JP2010509532A/ja
Publication of JP2010509532A5 publication Critical patent/JP2010509532A5/ja
Pending legal-status Critical Current

Links

JP2009535648A 2006-11-08 2007-09-20 タービン翼 Pending JP2010509532A (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
EP06023274A EP1921268A1 (de) 2006-11-08 2006-11-08 Turbinenschaufel
PCT/EP2007/059935 WO2008055737A1 (de) 2006-11-08 2007-09-20 Turbinenschaufel

Related Child Applications (1)

Application Number Title Priority Date Filing Date
JP2012046594A Division JP5269223B2 (ja) 2006-11-08 2012-03-02 タービン翼

Publications (2)

Publication Number Publication Date
JP2010509532A JP2010509532A (ja) 2010-03-25
JP2010509532A5 true JP2010509532A5 (enExample) 2010-07-22

Family

ID=37951488

Family Applications (2)

Application Number Title Priority Date Filing Date
JP2009535648A Pending JP2010509532A (ja) 2006-11-08 2007-09-20 タービン翼
JP2012046594A Expired - Fee Related JP5269223B2 (ja) 2006-11-08 2012-03-02 タービン翼

Family Applications After (1)

Application Number Title Priority Date Filing Date
JP2012046594A Expired - Fee Related JP5269223B2 (ja) 2006-11-08 2012-03-02 タービン翼

Country Status (7)

Country Link
US (1) US8297926B2 (enExample)
EP (2) EP1921268A1 (enExample)
JP (2) JP2010509532A (enExample)
CN (1) CN101535602B (enExample)
AT (1) ATE459785T1 (enExample)
DE (1) DE502007003044D1 (enExample)
WO (1) WO2008055737A1 (enExample)

Families Citing this family (29)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8348613B2 (en) 2009-03-30 2013-01-08 United Technologies Corporation Airflow influencing airfoil feature array
US8523524B2 (en) * 2010-03-25 2013-09-03 General Electric Company Airfoil cooling hole flag region
EP2584145A1 (en) * 2011-10-20 2013-04-24 Siemens Aktiengesellschaft A cooled turbine guide vane or blade for a turbomachine
JP2013100765A (ja) * 2011-11-08 2013-05-23 Ihi Corp インピンジ冷却機構、タービン翼及び燃焼器
JP5834876B2 (ja) 2011-12-15 2015-12-24 株式会社Ihi インピンジ冷却機構、タービン翼及び燃焼器
EP2703601B8 (en) * 2012-08-30 2016-09-14 General Electric Technology GmbH Modular Blade or Vane for a Gas Turbine and Gas Turbine with Such a Blade or Vane
US9995148B2 (en) 2012-10-04 2018-06-12 General Electric Company Method and apparatus for cooling gas turbine and rotor blades
KR101513474B1 (ko) * 2013-02-27 2015-04-23 두산중공업 주식회사 터빈 블레이드
US9850762B2 (en) 2013-03-13 2017-12-26 General Electric Company Dust mitigation for turbine blade tip turns
US20150204197A1 (en) * 2014-01-23 2015-07-23 Siemens Aktiengesellschaft Airfoil leading edge chamber cooling with angled impingement
US10001013B2 (en) * 2014-03-06 2018-06-19 General Electric Company Turbine rotor blades with platform cooling arrangements
US10422235B2 (en) 2014-05-29 2019-09-24 General Electric Company Angled impingement inserts with cooling features
US10563514B2 (en) 2014-05-29 2020-02-18 General Electric Company Fastback turbulator
US10364684B2 (en) 2014-05-29 2019-07-30 General Electric Company Fastback vorticor pin
CA2949539A1 (en) * 2014-05-29 2016-02-18 General Electric Company Engine components with impingement cooling features
US9957816B2 (en) 2014-05-29 2018-05-01 General Electric Company Angled impingement insert
CN106471213B (zh) 2014-07-09 2018-06-26 西门子公司 内部冷却系统内的冲击射流撞击通道系统
US10233775B2 (en) 2014-10-31 2019-03-19 General Electric Company Engine component for a gas turbine engine
US10280785B2 (en) 2014-10-31 2019-05-07 General Electric Company Shroud assembly for a turbine engine
US20160201476A1 (en) * 2014-10-31 2016-07-14 General Electric Company Airfoil for a turbine engine
US20160333701A1 (en) * 2015-05-12 2016-11-17 United Technologies Corporation Airfoil impingement cavity
US20170107827A1 (en) * 2015-10-15 2017-04-20 General Electric Company Turbine blade
US10352177B2 (en) 2016-02-16 2019-07-16 General Electric Company Airfoil having impingement openings
KR101906701B1 (ko) * 2017-01-03 2018-10-10 두산중공업 주식회사 가스터빈 블레이드
EP3396297A1 (de) * 2017-04-28 2018-10-31 Siemens Aktiengesellschaft Kühlvorrichtung
US10830049B2 (en) * 2017-05-02 2020-11-10 Raytheon Technologies Corporation Leading edge hybrid cavities and cores for airfoils of gas turbine engine
JP7096695B2 (ja) * 2018-04-17 2022-07-06 三菱重工業株式会社 タービン翼及びガスタービン
US10907480B2 (en) * 2018-09-28 2021-02-02 Raytheon Technologies Corporation Ribbed pin fins
CN113374535A (zh) * 2021-06-28 2021-09-10 常州大学 一种格子阵列式双层冷却燃气涡轮叶片

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1350424A (en) * 1971-07-02 1974-04-18 Rolls Royce Cooled blade for a gas turbine engine
JPS6163401U (enExample) * 1984-06-20 1986-04-30
JPS61187501A (ja) * 1985-02-15 1986-08-21 Hitachi Ltd 流体冷却構造
JPH0663442B2 (ja) * 1989-09-04 1994-08-22 株式会社日立製作所 タービン翼
FR2678318B1 (fr) * 1991-06-25 1993-09-10 Snecma Aube refroidie de distributeur de turbine.
US5468125A (en) * 1994-12-20 1995-11-21 Alliedsignal Inc. Turbine blade with improved heat transfer surface
JPH08296403A (ja) * 1995-04-25 1996-11-12 Toshiba Corp ガスタービン空冷翼
DE69718673T2 (de) * 1996-06-28 2003-05-22 United Technologies Corp., Hartford Kühlbare schaufelstruktur für eine gasturbine
US5738493A (en) * 1997-01-03 1998-04-14 General Electric Company Turbulator configuration for cooling passages of an airfoil in a gas turbine engine
EP0945595A3 (en) * 1998-03-26 2001-10-10 Mitsubishi Heavy Industries, Ltd. Gas turbine cooled blade
US6142734A (en) 1999-04-06 2000-11-07 General Electric Company Internally grooved turbine wall
EP1077311A1 (de) * 1999-08-17 2001-02-21 Siemens Aktiengesellschaft Gekühlte Gasturbinenschaufel
DE10248548A1 (de) * 2002-10-18 2004-04-29 Alstom (Switzerland) Ltd. Kühlbares Bauteil
US6890153B2 (en) * 2003-04-29 2005-05-10 General Electric Company Castellated turbine airfoil
EP1510653B1 (de) * 2003-07-29 2008-05-28 Siemens Aktiengesellschaft Gekühlte Turbinenschaufel
US7104757B2 (en) * 2003-07-29 2006-09-12 Siemens Aktiengesellschaft Cooled turbine blade
CA2476803C (en) * 2003-08-14 2010-10-26 Mitsubishi Heavy Industries, Ltd. Heat exchanging wall, gas turbine using the same, and flying body with gas turbine engine

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