JP2014156851A5 - - Google Patents

Download PDF

Info

Publication number
JP2014156851A5
JP2014156851A5 JP2013029430A JP2013029430A JP2014156851A5 JP 2014156851 A5 JP2014156851 A5 JP 2014156851A5 JP 2013029430 A JP2013029430 A JP 2013029430A JP 2013029430 A JP2013029430 A JP 2013029430A JP 2014156851 A5 JP2014156851 A5 JP 2014156851A5
Authority
JP
Japan
Prior art keywords
ring
turbine nozzle
manufacturing
wing
inner ring
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
JP2013029430A
Other languages
English (en)
Japanese (ja)
Other versions
JP2014156851A (ja
JP6045389B2 (ja
Filing date
Publication date
Application filed filed Critical
Priority claimed from JP2013029430A external-priority patent/JP6045389B2/ja
Priority to JP2013029430A priority Critical patent/JP6045389B2/ja
Priority to US14/760,517 priority patent/US20150354593A1/en
Priority to RU2015128612A priority patent/RU2015128612A/ru
Priority to CN201480005178.3A priority patent/CN104937220B/zh
Priority to EP14751725.4A priority patent/EP2933440A4/en
Priority to PCT/JP2014/053603 priority patent/WO2014126234A1/ja
Publication of JP2014156851A publication Critical patent/JP2014156851A/ja
Publication of JP2014156851A5 publication Critical patent/JP2014156851A5/ja
Publication of JP6045389B2 publication Critical patent/JP6045389B2/ja
Application granted granted Critical
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

JP2013029430A 2013-02-18 2013-02-18 タービンノズル及びその製造方法 Expired - Fee Related JP6045389B2 (ja)

Priority Applications (6)

Application Number Priority Date Filing Date Title
JP2013029430A JP6045389B2 (ja) 2013-02-18 2013-02-18 タービンノズル及びその製造方法
EP14751725.4A EP2933440A4 (en) 2013-02-18 2014-02-17 TURBINE NOZZLE AND METHOD FOR THE MANUFACTURE THEREOF
RU2015128612A RU2015128612A (ru) 2013-02-18 2014-02-17 Сопло турбины и способ его изготовления
CN201480005178.3A CN104937220B (zh) 2013-02-18 2014-02-17 涡轮机喷嘴及其制造方法
US14/760,517 US20150354593A1 (en) 2013-02-18 2014-02-17 Turbine nozzle and manufacturing method thereof
PCT/JP2014/053603 WO2014126234A1 (ja) 2013-02-18 2014-02-17 タービンノズル及びその製造方法

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2013029430A JP6045389B2 (ja) 2013-02-18 2013-02-18 タービンノズル及びその製造方法

Publications (3)

Publication Number Publication Date
JP2014156851A JP2014156851A (ja) 2014-08-28
JP2014156851A5 true JP2014156851A5 (cg-RX-API-DMAC7.html) 2015-12-17
JP6045389B2 JP6045389B2 (ja) 2016-12-14

Family

ID=51354232

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2013029430A Expired - Fee Related JP6045389B2 (ja) 2013-02-18 2013-02-18 タービンノズル及びその製造方法

Country Status (6)

Country Link
US (1) US20150354593A1 (cg-RX-API-DMAC7.html)
EP (1) EP2933440A4 (cg-RX-API-DMAC7.html)
JP (1) JP6045389B2 (cg-RX-API-DMAC7.html)
CN (1) CN104937220B (cg-RX-API-DMAC7.html)
RU (1) RU2015128612A (cg-RX-API-DMAC7.html)
WO (1) WO2014126234A1 (cg-RX-API-DMAC7.html)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3760869B1 (en) 2018-02-27 2023-08-23 Ihi Corporation Rocket-engine turbo pump
CN115523029B (zh) * 2022-10-24 2024-12-10 德阳钰鑫机械制造有限公司 一种整流器的制造工艺及整流器
CN119589139B (zh) * 2024-11-05 2025-12-12 中国航发南方工业有限公司 一种悬臂结构静子组件真空钎焊的尺寸控制方法

Family Cites Families (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2143466A (en) * 1937-12-31 1939-01-10 Westinghouse Electric & Mfg Co Turbine apparatus
US2611161A (en) * 1949-03-17 1952-09-23 Caterpillar Tractor Co Pattern fixture for making molds for turbines
JPS5812441B2 (ja) * 1979-04-17 1983-03-08 三井造船株式会社 タ−ビンノズル製作方法
US4464094A (en) * 1979-05-04 1984-08-07 Trw Inc. Turbine engine component and method of making the same
JPS5741405A (en) * 1980-08-22 1982-03-08 Hitachi Ltd Manufacturing method of turbine stator
JPH05202701A (ja) * 1992-01-28 1993-08-10 Mitsubishi Heavy Ind Ltd 接合方法
US5332360A (en) * 1993-09-08 1994-07-26 General Electric Company Stator vane having reinforced braze joint
EP1294528A4 (en) * 2000-04-28 2007-08-01 Elliott Turbo METHOD OF SOLDERING AND MANUFACTURING WORKPIECE THEREOF
SE523075C2 (sv) * 2001-11-22 2004-03-23 Volvo Aero Corp Förfarande för framställning av en stator- eller rotorkomponent
US6969240B2 (en) * 2003-08-01 2005-11-29 Honeywell International Inc. Integral turbine composed of a cast single crystal blade ring diffusion bonded to a high strength disk
JP2005098133A (ja) * 2003-09-22 2005-04-14 Toshiba Corp ガスタービン翼の拡散ろう付補修方法および補修用治具
US20050067061A1 (en) * 2003-09-26 2005-03-31 General Electric Company Nickel-based braze alloy compositions and related processes and articles
US7341427B2 (en) * 2005-12-20 2008-03-11 General Electric Company Gas turbine nozzle segment and process therefor
US7628586B2 (en) * 2005-12-28 2009-12-08 Elliott Company Impeller
CN101215977A (zh) * 2007-12-29 2008-07-09 东方电气集团东方汽轮机有限公司 汽轮机喷嘴组及其加工工艺
JP4672747B2 (ja) 2008-03-18 2011-04-20 三菱重工業株式会社 ロケットノズル及びロケットエンジン燃焼ガス流れの制御方法
CA2685995A1 (en) * 2008-11-25 2010-05-25 General Electric Company Vane with reduced stress
JP4699531B2 (ja) * 2009-01-27 2011-06-15 三菱重工業株式会社 インペラの製造方法およびインペラ
CN201574784U (zh) * 2009-12-31 2010-09-08 山东齐鲁电机制造有限公司 整体铣制汽轮机高压进汽喷嘴组
US8650754B2 (en) * 2010-11-11 2014-02-18 Mitsubishi Heavy Industries, Ltd. Method for manufacturing impeller
US9447689B2 (en) * 2011-06-17 2016-09-20 General Electric Company Method of repairing a turbine nozzle segment in a turbine engine
JP2013029430A (ja) 2011-07-28 2013-02-07 Mitsubishi Electric Corp 2チャネル追尾装置、および追尾方法

Similar Documents

Publication Publication Date Title
USD743321S1 (en) Aircraft cabin
JP2015226935A5 (cg-RX-API-DMAC7.html)
EP3042008A4 (en) Method of fabricating a 3-dimensional structure, mesh formwork element for fabricating a 3-dimensional structure, and method of fabricating the same
JP2012247336A5 (ja) 物理量検出器の製造方法、物理量検出器
JP2019528225A5 (cg-RX-API-DMAC7.html)
RU2015146763A (ru) Способ изготовления асимметричного компонента с применением аддитивного производства
WO2014143364A3 (en) Co-formed element with low conductivity layer
WO2015057310A3 (en) Platform cooling core for a gas turbine engine rotor blade
WO2014197119A3 (en) Rotors with modulus mistuned airfoils
JP2015110246A5 (cg-RX-API-DMAC7.html)
EP2497596A3 (en) Method of fabricating a component and a component
WO2014099067A3 (en) Aluminum brazing of hollow titanium fan blades
FR2990642B1 (fr) Procede de collage de pieces intermediaires de fabrication dites pif sur une aube en materiau composite de turbomachine
WO2014163703A3 (en) Method for making gas turbine engine composite structure
WO2015017478A3 (en) SYNTHESIS OF CdSe/ZnS CORE/SHELL SEMICONDUCTOR NANOWIRES
EP3351728A4 (en) ROTOR BUCKET, GAS TURBINE AND ROTOR SHAFT MANUFACTURING EQUIPMENT THUS EQUIPPED
FR3004197B1 (fr) Toles minces en alliage d'aluminium-cuivre-lithium pour la fabrication de fuselages d'avion.
WO2014175940A3 (en) Gas turbine engine component manufacturing method and core for making same
WO2015191330A8 (en) Turbine blisk and method of manufacturing thereof
JP2014156851A5 (cg-RX-API-DMAC7.html)
JP2016521913A5 (cg-RX-API-DMAC7.html)
FR3002877B1 (fr) Procede de fabrication d'un materiau composite multicouche, materiau composite multicouche obtenu par le procede et pieces ou structures mecaniques realisees avec ledit materiau.
WO2013092920A3 (fr) Procede de realisation d'un resonateur
JP2016112787A5 (ja) 複合構造体の成形方法
EP3520915A4 (en) METHOD FOR MANUFACTURING NI HEAT-RESISTANT ALLOY EXTRUDED MATERIAL, AND NI HEAT-RESISTANT ALLOY EXTRUDED MATERIAL