JP2011001951A5 - - Google Patents
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- Publication number
- JP2011001951A5 JP2011001951A5 JP2010135647A JP2010135647A JP2011001951A5 JP 2011001951 A5 JP2011001951 A5 JP 2011001951A5 JP 2010135647 A JP2010135647 A JP 2010135647A JP 2010135647 A JP2010135647 A JP 2010135647A JP 2011001951 A5 JP2011001951 A5 JP 2011001951A5
- Authority
- JP
- Japan
- Prior art keywords
- rail
- circumferential
- circumferentially
- nozzle according
- central portion
- 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
Links
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US12/486,126 US8328511B2 (en) | 2009-06-17 | 2009-06-17 | Prechorded turbine nozzle |
| US12/486,126 | 2009-06-17 |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2011001951A JP2011001951A (ja) | 2011-01-06 |
| JP2011001951A5 true JP2011001951A5 (enExample) | 2013-08-01 |
| JP5507351B2 JP5507351B2 (ja) | 2014-05-28 |
Family
ID=42471536
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2010135647A Expired - Fee Related JP5507351B2 (ja) | 2009-06-17 | 2010-06-15 | プリコーディングされたタービンノズル |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US8328511B2 (enExample) |
| JP (1) | JP5507351B2 (enExample) |
| CA (1) | CA2705980A1 (enExample) |
| DE (1) | DE102010017314A1 (enExample) |
| GB (1) | GB2471185B (enExample) |
Families Citing this family (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104471197B (zh) * | 2012-04-27 | 2016-05-11 | 通用电气公司 | 限制涡轮机组件内的吊架与整流罩组件间轴向移动的系统和方法 |
| WO2015105654A1 (en) | 2014-01-08 | 2015-07-16 | United Technologies Corporation | Clamping seal for jet engine mid-turbine frame |
| EP3023597B1 (en) * | 2014-10-30 | 2019-11-27 | United Technologies Corporation | Sealing systems |
| US9863260B2 (en) * | 2015-03-30 | 2018-01-09 | General Electric Company | Hybrid nozzle segment assemblies for a gas turbine engine |
| US10392950B2 (en) | 2015-05-07 | 2019-08-27 | General Electric Company | Turbine band anti-chording flanges |
| JP6614407B2 (ja) * | 2015-06-10 | 2019-12-04 | 株式会社Ｉｈｉ | タービン |
| EP3118419A1 (en) * | 2015-07-15 | 2017-01-18 | Siemens Aktiengesellschaft | Non-concentrically shaped ring segment |
| EP3438416B1 (de) | 2017-08-04 | 2021-03-17 | MTU Aero Engines GmbH | Leitschaufelsegment für eine turbomaschine |
| US11674400B2 (en) * | 2021-03-12 | 2023-06-13 | Ge Avio S.R.L. | Gas turbine engine nozzles |
| US12442304B1 (en) | 2025-03-12 | 2025-10-14 | General Electric Company | Gas turbine engine with bow wave mitigation |
Family Cites Families (16)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3860358A (en) * | 1974-04-18 | 1975-01-14 | United Aircraft Corp | Turbine blade tip seal |
| JPS6030431A (ja) | 1983-07-29 | 1985-02-16 | Hitachi Ltd | ガスタ−ビン燃焼器用シ−ル |
| FR2597921A1 (fr) * | 1986-04-24 | 1987-10-30 | Snecma | Anneau de turbine sectorise |
| US5205708A (en) * | 1992-02-07 | 1993-04-27 | General Electric Company | High pressure turbine component interference fit up |
| US5641267A (en) * | 1995-06-06 | 1997-06-24 | General Electric Company | Controlled leakage shroud panel |
| US5669757A (en) * | 1995-11-30 | 1997-09-23 | General Electric Company | Turbine nozzle retainer assembly |
| US5655876A (en) * | 1996-01-02 | 1997-08-12 | General Electric Company | Low leakage turbine nozzle |
| US5797723A (en) * | 1996-11-13 | 1998-08-25 | General Electric Company | Turbine flowpath seal |
| US5970716A (en) | 1997-10-02 | 1999-10-26 | General Electric Company | Apparatus for retaining centerbody between adjacent domes of multiple annular combustor employing interference and clamping fits |
| US6183192B1 (en) * | 1999-03-22 | 2001-02-06 | General Electric Company | Durable turbine nozzle |
| DE19915049A1 (de) * | 1999-04-01 | 2000-10-05 | Abb Alstom Power Ch Ag | Hitzeschild für eine Gasturbine |
| JP4011296B2 (ja) * | 2001-02-14 | 2007-11-21 | 株式会社日立製作所 | ガスタービン |
| US6702550B2 (en) * | 2002-01-16 | 2004-03-09 | General Electric Company | Turbine shroud segment and shroud assembly |
| US6887041B2 (en) | 2003-03-03 | 2005-05-03 | General Electric Company | Airfoil shape for a turbine nozzle |
| US7458772B2 (en) * | 2004-10-26 | 2008-12-02 | Alstom Technology Ltd. | Guide vane ring of a turbomachine and associated modification method |
| US7442004B2 (en) * | 2005-08-06 | 2008-10-28 | General Electric Company | Thermally compliant C-clip |
-
2009
- 2009-06-17 US US12/486,126 patent/US8328511B2/en active Active
-
2010
- 2010-06-03 CA CA2705980A patent/CA2705980A1/en not_active Abandoned
- 2010-06-09 DE DE102010017314A patent/DE102010017314A1/de not_active Withdrawn
- 2010-06-14 GB GB1009834.1A patent/GB2471185B/en not_active Expired - Fee Related
- 2010-06-15 JP JP2010135647A patent/JP5507351B2/ja not_active Expired - Fee Related