JP2010038161A5 - - Google Patents
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- Publication number
- JP2010038161A5 JP2010038161A5 JP2009175957A JP2009175957A JP2010038161A5 JP 2010038161 A5 JP2010038161 A5 JP 2010038161A5 JP 2009175957 A JP2009175957 A JP 2009175957A JP 2009175957 A JP2009175957 A JP 2009175957A JP 2010038161 A5 JP2010038161 A5 JP 2010038161A5
- Authority
- JP
- Japan
- Prior art keywords
- band
- doublet vane
- doublet
- seal
- airfoil
- 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
Links
- 239000012720 thermal barrier coating Substances 0.000 claims 3
- 239000002184 metal Substances 0.000 claims 2
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US12/222,091 US8157515B2 (en) | 2008-08-01 | 2008-08-01 | Split doublet power nozzle and related method |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JP2010038161A JP2010038161A (ja) | 2010-02-18 |
| JP2010038161A5 true JP2010038161A5 (enExample) | 2012-08-23 |
Family
ID=41528291
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2009175957A Pending JP2010038161A (ja) | 2008-08-01 | 2009-07-29 | 二分割パワーノズル及び関連方法 |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US8157515B2 (enExample) |
| JP (1) | JP2010038161A (enExample) |
| CN (1) | CN101638996A (enExample) |
| DE (1) | DE102009026301A1 (enExample) |
Families Citing this family (28)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20110012240A1 (en) * | 2009-07-15 | 2011-01-20 | Chenglin Liu | Multi-Connect Lead |
| US20110182726A1 (en) * | 2010-01-25 | 2011-07-28 | United Technologies Corporation | As-cast shroud slots with pre-swirled leakage |
| US8449249B2 (en) * | 2010-04-09 | 2013-05-28 | Williams International Co., L.L.C. | Turbine nozzle apparatus and associated method of manufacture |
| US20130011265A1 (en) * | 2011-07-05 | 2013-01-10 | Alstom Technology Ltd. | Chevron platform turbine vane |
| DE102011084125A1 (de) * | 2011-10-07 | 2013-04-11 | Mtu Aero Engines Gmbh | Schaufelsegment und Strömungsmaschine |
| US8967973B2 (en) * | 2011-10-26 | 2015-03-03 | General Electric Company | Turbine bucket platform shaping for gas temperature control and related method |
| US20130142640A1 (en) * | 2011-12-02 | 2013-06-06 | David P. Houston | Alternate shroud width to provide mistuning on compressor stator clusters |
| US9169782B2 (en) * | 2012-01-04 | 2015-10-27 | General Electric Company | Turbine to operate at part-load |
| US9039370B2 (en) * | 2012-03-29 | 2015-05-26 | Solar Turbines Incorporated | Turbine nozzle |
| US20140023517A1 (en) * | 2012-07-23 | 2014-01-23 | General Electric Company | Nozzle for turbine system |
| EP2716787A1 (en) * | 2012-10-05 | 2014-04-09 | Siemens Aktiengesellschaft | Method for manufacturing a turbine assembly |
| US9506362B2 (en) * | 2013-11-20 | 2016-11-29 | General Electric Company | Steam turbine nozzle segment having transitional interface, and nozzle assembly and steam turbine including such nozzle segment |
| GB201408258D0 (en) * | 2014-05-09 | 2014-06-25 | British Sky Broadcasting Ltd | Television display and remote control |
| JP5717904B1 (ja) * | 2014-08-04 | 2015-05-13 | 三菱日立パワーシステムズ株式会社 | 静翼、ガスタービン、分割環、静翼の改造方法、および、分割環の改造方法 |
| US20170051619A1 (en) * | 2015-08-18 | 2017-02-23 | General Electric Company | Cmc nozzles with split endwalls for gas turbine engines |
| US10047613B2 (en) * | 2015-08-31 | 2018-08-14 | General Electric Company | Gas turbine components having non-uniformly applied coating and methods of assembling the same |
| US10599324B2 (en) * | 2015-12-31 | 2020-03-24 | Microsoft Technology Licensing, Llc | Hand gesture API using finite state machine and gesture language discrete values |
| US10633991B2 (en) | 2016-01-15 | 2020-04-28 | DOOSAN Heavy Industries Construction Co., LTD | Nozzle box assembly |
| KR101845695B1 (ko) * | 2016-01-15 | 2018-04-06 | 두산중공업 주식회사 | 노즐 박스 어셈블리 |
| FR3052486B1 (fr) * | 2016-06-09 | 2020-03-13 | Safran Aircraft Engines | Secteur de distributeur pour turbomachine comprenant une plateforme separees en portions circonferentielles |
| FR3070718B1 (fr) * | 2017-09-06 | 2019-08-23 | Safran Aircraft Engines | Ensemble de turbine a secteurs d'anneau |
| KR101937586B1 (ko) * | 2017-09-12 | 2019-01-10 | 두산중공업 주식회사 | 베인 조립체, 터빈 및 이를 포함하는 가스터빈 |
| US11047248B2 (en) * | 2018-06-19 | 2021-06-29 | General Electric Company | Curved seal for adjacent gas turbine components |
| US11156116B2 (en) | 2019-04-08 | 2021-10-26 | Honeywell International Inc. | Turbine nozzle with reduced leakage feather seals |
| US11092022B2 (en) * | 2019-11-04 | 2021-08-17 | Raytheon Technologies Corporation | Vane with chevron face |
| US11492917B2 (en) | 2020-02-18 | 2022-11-08 | General Electric Company | Nozzle with slash face(s) with swept surfaces joining at arc with peak aligned with stiffening member |
| US11359502B2 (en) | 2020-02-18 | 2022-06-14 | General Electric Company | Nozzle with slash face(s) with swept surfaces with joining line aligned with stiffening member |
| US12180859B2 (en) | 2023-02-01 | 2024-12-31 | Ge Infrastructure Technology Llc | Nozzle segment for use with multiple different turbine engines |
Family Cites Families (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR1330656A (fr) * | 1962-08-08 | 1963-06-21 | Bbc Brown Boveri & Cie | Aubage à bande de recouvrement, pour turbines ou compresseurs |
| JPS6026103A (ja) * | 1983-07-20 | 1985-02-09 | Hitachi Ltd | ガスタ−ビン静翼 |
| US5441385A (en) * | 1993-12-13 | 1995-08-15 | Solar Turbines Incorporated | Turbine nozzle/nozzle support structure |
| JPH1181911A (ja) * | 1997-09-12 | 1999-03-26 | Niigata Eng Co Ltd | 軸流式タービンの静翼におけるシール装置 |
| JPH11125102A (ja) * | 1997-10-22 | 1999-05-11 | Mitsubishi Heavy Ind Ltd | ガスタービン静翼 |
| US6099245A (en) * | 1998-10-30 | 2000-08-08 | General Electric Company | Tandem airfoils |
| US6910854B2 (en) * | 2002-10-08 | 2005-06-28 | United Technologies Corporation | Leak resistant vane cluster |
| EP1510654A1 (de) * | 2003-08-25 | 2005-03-02 | Siemens Aktiengesellschaft | Einstückige Turbinenbeschaufelungseinheit und Verfahren zur Herstellung einer einstückigen Turbinenbeschaufelungseinheit |
| US7008178B2 (en) * | 2003-12-17 | 2006-03-07 | General Electric Company | Inboard cooled nozzle doublet |
| US7101150B2 (en) * | 2004-05-11 | 2006-09-05 | Power Systems Mfg, Llc | Fastened vane assembly |
| US7334306B2 (en) * | 2004-06-02 | 2008-02-26 | General Electric Company | Methods and apparatus for fabricating a turbine nozzle assembly |
| US7329096B2 (en) * | 2005-10-18 | 2008-02-12 | General Electric Company | Machine tooled diaphragm partitions and nozzles |
| US7341427B2 (en) * | 2005-12-20 | 2008-03-11 | General Electric Company | Gas turbine nozzle segment and process therefor |
| FR2902843A1 (fr) * | 2006-06-23 | 2007-12-28 | Snecma Sa | Secteur de redresseur de compresseur ou secteur de distributeur de turbomachine |
-
2008
- 2008-08-01 US US12/222,091 patent/US8157515B2/en active Active
-
2009
- 2009-07-29 JP JP2009175957A patent/JP2010038161A/ja active Pending
- 2009-07-31 DE DE102009026301A patent/DE102009026301A1/de not_active Withdrawn
- 2009-07-31 CN CN200910165827A patent/CN101638996A/zh active Pending
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