JP2012026439A5 - - Google Patents
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- Publication number
- JP2012026439A5 JP2012026439A5 JP2011153391A JP2011153391A JP2012026439A5 JP 2012026439 A5 JP2012026439 A5 JP 2012026439A5 JP 2011153391 A JP2011153391 A JP 2011153391A JP 2011153391 A JP2011153391 A JP 2011153391A JP 2012026439 A5 JP2012026439 A5 JP 2012026439A5
- Authority
- JP
- Japan
- Prior art keywords
- edge
- leading edge
- turbine
- stationary nozzle
- trailing edge
- 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
- 239000012530 fluid Substances 0.000 claims 2
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US12/841,365 | 2010-07-22 | ||
| US12/841,365 US8602727B2 (en) | 2010-07-22 | 2010-07-22 | Turbine nozzle segment having arcuate concave leading edge |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JP2012026439A JP2012026439A (ja) | 2012-02-09 |
| JP2012026439A5 true JP2012026439A5 (enExample) | 2014-08-21 |
Family
ID=45443675
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2011153391A Pending JP2012026439A (ja) | 2010-07-22 | 2011-07-12 | 弓形凹状の前縁を有するタービンノズルセグメント |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US8602727B2 (enExample) |
| JP (1) | JP2012026439A (enExample) |
| DE (1) | DE102011052077A1 (enExample) |
| FR (1) | FR2963056B1 (enExample) |
| RU (1) | RU2011130225A (enExample) |
Families Citing this family (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP2476862B1 (en) * | 2011-01-13 | 2013-11-20 | Alstom Technology Ltd | Vane for an axial flow turbomachine and corresponding turbomachine |
| KR101473117B1 (ko) * | 2013-12-31 | 2014-12-15 | 이도훈 | 역결제 방식의 모바일 pos 시스템 및 그 방법 |
| GB2544526B (en) * | 2015-11-20 | 2019-09-18 | Rolls Royce Plc | Gas turbine engine |
| EP3358134B1 (en) * | 2017-02-02 | 2021-07-14 | General Electric Company | Steam turbine with rotor blade |
| US10808535B2 (en) * | 2018-09-27 | 2020-10-20 | General Electric Company | Blade structure for turbomachine |
| US11220910B2 (en) * | 2019-07-26 | 2022-01-11 | Pratt & Whitney Canada Corp. | Compressor stator |
| US11286779B2 (en) * | 2020-06-03 | 2022-03-29 | Honeywell International Inc. | Characteristic distribution for rotor blade of booster rotor |
Family Cites Families (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP3631271B2 (ja) * | 1993-11-19 | 2005-03-23 | ユナイテッド テクノロジーズ コーポレイション | インナーシュラウド一体型ステータベーン構造 |
| JPH10103002A (ja) * | 1996-09-30 | 1998-04-21 | Toshiba Corp | 軸流流体機械用翼 |
| JP4315597B2 (ja) * | 1998-06-12 | 2009-08-19 | 株式会社荏原製作所 | タービンノズル翼 |
| US6398489B1 (en) | 2001-02-08 | 2002-06-04 | General Electric Company | Airfoil shape for a turbine nozzle |
| US6508630B2 (en) * | 2001-03-30 | 2003-01-21 | General Electric Company | Twisted stator vane |
| US7086829B2 (en) * | 2004-02-03 | 2006-08-08 | General Electric Company | Film cooling for the trailing edge of a steam cooled nozzle |
| US7758306B2 (en) * | 2006-12-22 | 2010-07-20 | General Electric Company | Turbine assembly for a gas turbine engine and method of manufacturing the same |
-
2010
- 2010-07-22 US US12/841,365 patent/US8602727B2/en not_active Expired - Fee Related
-
2011
- 2011-07-12 JP JP2011153391A patent/JP2012026439A/ja active Pending
- 2011-07-19 FR FR1156547A patent/FR2963056B1/fr not_active Expired - Fee Related
- 2011-07-21 RU RU2011130225/06A patent/RU2011130225A/ru not_active Application Discontinuation
- 2011-07-22 DE DE102011052077A patent/DE102011052077A1/de not_active Withdrawn
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