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 |
|---|---|---|---|---|
| JP5997835B2 (ja) * | 2012-04-27 | 2016-09-28 | ゼネラル・エレクトリック・カンパニイ | タービン組立体の中でハンガーとフェアリング組立体との間の軸方向の移動を制限するシステムおよび方法 |
| EP3092372B1 (en) | 2014-01-08 | 2019-06-19 | United Technologies Corporation | Clamping seal for jet engine mid-turbine frame |
| EP3628822B1 (en) * | 2014-10-30 | 2022-05-04 | Raytheon 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 |
| ES2865387T3 (es) | 2017-08-04 | 2021-10-15 | MTU Aero Engines AG | Segmento de paletas guía para una turbina |
| 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
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