JP2002138802A5 - - Google Patents

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Publication number
JP2002138802A5
JP2002138802A5 JP2001225349A JP2001225349A JP2002138802A5 JP 2002138802 A5 JP2002138802 A5 JP 2002138802A5 JP 2001225349 A JP2001225349 A JP 2001225349A JP 2001225349 A JP2001225349 A JP 2001225349A JP 2002138802 A5 JP2002138802 A5 JP 2002138802A5
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JP
Japan
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.)
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Application number
JP2001225349A
Other versions
JP2002138802A (ja
JP4733306B2 (ja
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Publication date
Priority claimed from US09/626,980 external-priority patent/US6354797B1/en
Application filed filed Critical
Publication of JP2002138802A publication Critical patent/JP2002138802A/ja
Publication of JP2002138802A5 publication Critical patent/JP2002138802A5/ja
Application granted granted Critical
Publication of JP4733306B2 publication Critical patent/JP4733306B2/ja
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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JP2001225349A 2000-07-27 2001-07-26 ろう付け無し隅肉を用いるタービンノズル Expired - Fee Related JP4733306B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US09/626980 2000-07-27
US09/626,980 US6354797B1 (en) 2000-07-27 2000-07-27 Brazeless fillet turbine nozzle

Publications (3)

Publication Number Publication Date
JP2002138802A JP2002138802A (ja) 2002-05-17
JP2002138802A5 true JP2002138802A5 (ja) 2008-09-11
JP4733306B2 JP4733306B2 (ja) 2011-07-27

Family

ID=24512663

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2001225349A Expired - Fee Related JP4733306B2 (ja) 2000-07-27 2001-07-26 ろう付け無し隅肉を用いるタービンノズル

Country Status (4)

Country Link
US (1) US6354797B1 (ja)
EP (1) EP1176284B1 (ja)
JP (1) JP4733306B2 (ja)
DE (1) DE60132521T2 (ja)

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US9447689B2 (en) 2011-06-17 2016-09-20 General Electric Company Method of repairing a turbine nozzle segment in a turbine engine
US8944750B2 (en) 2011-12-22 2015-02-03 Pratt & Whitney Canada Corp. High pressure turbine vane cooling hole distribution
US9097124B2 (en) 2012-01-24 2015-08-04 United Technologies Corporation Gas turbine engine stator vane assembly with inner shroud
US9322279B2 (en) * 2012-07-02 2016-04-26 United Technologies Corporation Airfoil cooling arrangement
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US9988932B2 (en) 2013-12-06 2018-06-05 Honeywell International Inc. Bi-cast turbine nozzles and methods for cooling slip joints therein
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US9581029B2 (en) 2014-09-24 2017-02-28 Pratt & Whitney Canada Corp. High pressure turbine blade cooling hole distribution
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EP3075960B1 (en) 2015-03-31 2017-12-27 Ansaldo Energia IP UK Limited Multi-airfoil guide vane unit
US10018075B2 (en) * 2015-04-22 2018-07-10 General Electric Company Methods for positioning neighboring nozzles of a gas turbine engine
EP3103580B1 (en) * 2015-06-12 2021-01-20 Ansaldo Energia IP UK Limited Method for manufacturing a blading member assembly
EP3147454B1 (en) 2015-09-22 2020-11-04 Ansaldo Energia IP UK Limited Turboengine component and method for assembling and reconditioning a turboengine component
US20170198602A1 (en) * 2016-01-11 2017-07-13 General Electric Company Gas turbine engine with a cooled nozzle segment
EP3293354B1 (en) * 2016-09-07 2021-04-14 Ansaldo Energia IP UK Limited Turboengine blading member and a method for assembling such a member
US10648363B2 (en) * 2017-12-28 2020-05-12 United Technologies Corporation Turbine vane cooling arrangement
US10830074B2 (en) * 2018-07-03 2020-11-10 Raytheon Technologies Corporation Potted stator vane with metal fillet
CN109047512B (zh) * 2018-10-12 2023-05-23 福建兵工装备有限公司 固体发动机喷管毛坯组件及其生产方法和使用的模具
RU192446U1 (ru) * 2019-03-13 2019-09-17 Федеральное государственное бюджетное образовательное учреждение высшего образования "Рыбинский государственный авиационный технический университет имени П.А. Соловьева" Блок сопловых турбинных лопаток с охлаждаемой несимметричной торцевой полкой
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CN113927116B (zh) * 2021-11-10 2023-03-28 中国航发南方工业有限公司 航空发动机扩压器组件真空钎焊方法和扩压器组件
CN114278388A (zh) * 2021-12-24 2022-04-05 上海电气燃气轮机有限公司 一种透平叶片的气膜冷却结构
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CN118371824B (zh) * 2024-05-27 2024-09-27 威海克莱特菲尔风机股份有限公司 一种空心叶片的焊接方法及离心叶轮

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