JP2015048848A5 - - Google Patents

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Publication number
JP2015048848A5
JP2015048848A5 JP2014173389A JP2014173389A JP2015048848A5 JP 2015048848 A5 JP2015048848 A5 JP 2015048848A5 JP 2014173389 A JP2014173389 A JP 2014173389A JP 2014173389 A JP2014173389 A JP 2014173389A JP 2015048848 A5 JP2015048848 A5 JP 2015048848A5
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JP
Japan
Prior art keywords
forming
delivery
fluid communication
channels
fluid
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
JP2014173389A
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English (en)
Japanese (ja)
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JP2015048848A (ja
JP7051273B2 (ja
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Publication date
Priority claimed from US14/016,769 external-priority patent/US9416662B2/en
Application filed filed Critical
Publication of JP2015048848A publication Critical patent/JP2015048848A/ja
Publication of JP2015048848A5 publication Critical patent/JP2015048848A5/ja
Application granted granted Critical
Publication of JP7051273B2 publication Critical patent/JP7051273B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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JP2014173389A 2013-09-03 2014-08-28 タービン部品を冷却するための方法およびシステム Active JP7051273B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US14/016,769 US9416662B2 (en) 2013-09-03 2013-09-03 Method and system for providing cooling for turbine components
US14/016,769 2013-09-03

Publications (3)

Publication Number Publication Date
JP2015048848A JP2015048848A (ja) 2015-03-16
JP2015048848A5 true JP2015048848A5 (enExample) 2017-09-28
JP7051273B2 JP7051273B2 (ja) 2022-04-11

Family

ID=52470582

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2014173389A Active JP7051273B2 (ja) 2013-09-03 2014-08-28 タービン部品を冷却するための方法およびシステム

Country Status (4)

Country Link
US (1) US9416662B2 (enExample)
JP (1) JP7051273B2 (enExample)
CH (1) CH708574A2 (enExample)
DE (1) DE102014111844B4 (enExample)

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* Cited by examiner, † Cited by third party
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US9857002B2 (en) * 2014-05-09 2018-01-02 United Technologies Corporation Fluid couplings and methods for additive manufacturing thereof
US10378444B2 (en) 2015-08-19 2019-08-13 General Electric Company Engine component for a gas turbine engine
US9995172B2 (en) * 2015-10-12 2018-06-12 General Electric Company Turbine nozzle with cooling channel coolant discharge plenum
US10533749B2 (en) * 2015-10-27 2020-01-14 Pratt & Whitney Cananda Corp. Effusion cooling holes
US10871075B2 (en) 2015-10-27 2020-12-22 Pratt & Whitney Canada Corp. Cooling passages in a turbine component
US10520193B2 (en) 2015-10-28 2019-12-31 General Electric Company Cooling patch for hot gas path components
DE102016107315A1 (de) * 2016-04-20 2017-10-26 Rolls-Royce Deutschland Ltd & Co Kg Rotor mit Überhang an Laufschaufeln für ein Sicherungselement
US20170306775A1 (en) * 2016-04-21 2017-10-26 General Electric Company Article, component, and method of making a component
US9995175B2 (en) * 2016-06-29 2018-06-12 General Electric Company System and method for gas bearing support of turbine
DE102016217320A1 (de) * 2016-09-12 2018-03-15 Siemens Aktiengesellschaft Gasturbine mit getrennter Kühlung für Turbine und Abgasgehäuse
US10233761B2 (en) 2016-10-26 2019-03-19 General Electric Company Turbine airfoil trailing edge coolant passage created by cover
US10933481B2 (en) 2018-01-05 2021-03-02 General Electric Company Method of forming cooling passage for turbine component with cap element
US10612391B2 (en) 2018-01-05 2020-04-07 General Electric Company Two portion cooling passage for airfoil
JP6636668B1 (ja) 2019-03-29 2020-01-29 三菱重工業株式会社 高温部品、高温部品の製造方法及び流量調節方法
JP7234006B2 (ja) 2019-03-29 2023-03-07 三菱重工業株式会社 高温部品及び高温部品の製造方法
JP6666500B1 (ja) 2019-03-29 2020-03-13 三菱重工業株式会社 高温部品及び高温部品の製造方法
US11460191B2 (en) 2020-08-31 2022-10-04 General Electric Company Cooling insert for a turbomachine
US11371702B2 (en) 2020-08-31 2022-06-28 General Electric Company Impingement panel for a turbomachine
US11994292B2 (en) 2020-08-31 2024-05-28 General Electric Company Impingement cooling apparatus for turbomachine
US11614233B2 (en) 2020-08-31 2023-03-28 General Electric Company Impingement panel support structure and method of manufacture
US11994293B2 (en) 2020-08-31 2024-05-28 General Electric Company Impingement cooling apparatus support structure and method of manufacture
US11255545B1 (en) 2020-10-26 2022-02-22 General Electric Company Integrated combustion nozzle having a unified head end
US11814965B2 (en) 2021-11-10 2023-11-14 General Electric Company Turbomachine blade trailing edge cooling circuit with turn passage having set of obstructions
US11767766B1 (en) 2022-07-29 2023-09-26 General Electric Company Turbomachine airfoil having impingement cooling passages
US11572803B1 (en) 2022-08-01 2023-02-07 General Electric Company Turbine airfoil with leading edge cooling passage(s) coupled via plenum to film cooling holes, and related method

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US5820337A (en) 1995-01-03 1998-10-13 General Electric Company Double wall turbine parts
US5626462A (en) 1995-01-03 1997-05-06 General Electric Company Double-wall airfoil
US5957657A (en) 1996-02-26 1999-09-28 Mitisubishi Heavy Industries, Ltd. Method of forming a cooling air passage in a gas turbine stationary blade shroud
US6329015B1 (en) 2000-05-23 2001-12-11 General Electric Company Method for forming shaped holes
US20040086635A1 (en) 2002-10-30 2004-05-06 Grossklaus Warren Davis Method of repairing a stationary shroud of a gas turbine engine using laser cladding
US6905302B2 (en) * 2003-09-17 2005-06-14 General Electric Company Network cooled coated wall
US7363707B2 (en) 2004-06-14 2008-04-29 General Electric Company Braze repair of shroud block seal teeth in a gas turbine engine
ATE513980T1 (de) 2004-12-24 2011-07-15 Alstom Technology Ltd Verfahren zur herstellung eines bauteils mit eingebettetem kanal sowie bauteil
US7653994B2 (en) 2006-03-22 2010-02-02 General Electric Company Repair of HPT shrouds with sintered preforms
US7712316B2 (en) * 2007-01-09 2010-05-11 United Technologies Corporation Turbine blade with reverse cooling air film hole direction
US7900458B2 (en) 2007-05-29 2011-03-08 Siemens Energy, Inc. Turbine airfoils with near surface cooling passages and method of making same
EP2108477B1 (en) 2008-04-09 2011-03-23 Alstom Technology Ltd Gas turbine hot gas component repair method
US8449254B2 (en) * 2010-03-29 2013-05-28 United Technologies Corporation Branched airfoil core cooling arrangement
US8651805B2 (en) 2010-04-22 2014-02-18 General Electric Company Hot gas path component cooling system
US8608443B2 (en) * 2010-06-11 2013-12-17 Siemens Energy, Inc. Film cooled component wall in a turbine engine
US9181819B2 (en) 2010-06-11 2015-11-10 Siemens Energy, Inc. Component wall having diffusion sections for cooling in a turbine engine
US8727727B2 (en) * 2010-12-10 2014-05-20 General Electric Company Components with cooling channels and methods of manufacture
US8753071B2 (en) 2010-12-22 2014-06-17 General Electric Company Cooling channel systems for high-temperature components covered by coatings, and related processes
US8533949B2 (en) 2011-02-14 2013-09-17 General Electric Company Methods of manufacture for components with cooling channels
US8870536B2 (en) * 2012-01-13 2014-10-28 General Electric Company Airfoil

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