JP5507351B2 - プリコーディングされたタービンノズル - Google Patents
プリコーディングされたタービンノズル Download PDFInfo
- Publication number
- JP5507351B2 JP5507351B2 JP2010135647A JP2010135647A JP5507351B2 JP 5507351 B2 JP5507351 B2 JP 5507351B2 JP 2010135647 A JP2010135647 A JP 2010135647A JP 2010135647 A JP2010135647 A JP 2010135647A JP 5507351 B2 JP5507351 B2 JP 5507351B2
- Authority
- JP
- Japan
- Prior art keywords
- rail
- circumferential
- nozzle
- circumferentially
- groove
- 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.)
- Expired - Fee Related
Links
- 239000000567 combustion gas Substances 0.000 description 11
- 239000007789 gas Substances 0.000 description 9
- 238000001816 cooling Methods 0.000 description 7
- 230000004048 modification Effects 0.000 description 4
- 238000012986 modification Methods 0.000 description 4
- 230000008859 change Effects 0.000 description 3
- 230000035882 stress Effects 0.000 description 3
- 230000007423 decrease Effects 0.000 description 2
- 238000013461 design Methods 0.000 description 2
- 239000000446 fuel Substances 0.000 description 2
- 230000007246 mechanism Effects 0.000 description 2
- 238000007789 sealing Methods 0.000 description 2
- 210000002105 tongue Anatomy 0.000 description 2
- 230000002411 adverse Effects 0.000 description 1
- 238000004458 analytical method Methods 0.000 description 1
- 238000004873 anchoring Methods 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 239000000284 extract Substances 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
- 230000008646 thermal stress Effects 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
- F01D25/246—Fastening of diaphragms or stator-rings
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
- F01D9/041—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using blades
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
- F01D9/047—Nozzle boxes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2230/00—Manufacture
- F05D2230/60—Assembly methods
- F05D2230/64—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins
- F05D2230/642—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins using maintaining alignment while permitting differential dilatation
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2250/00—Geometry
- F05D2250/70—Shape
- F05D2250/71—Shape curved
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2250/00—Geometry
- F05D2250/70—Shape
- F05D2250/71—Shape curved
- F05D2250/711—Shape curved convex
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2250/00—Geometry
- F05D2250/70—Shape
- F05D2250/71—Shape curved
- F05D2250/712—Shape curved concave
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
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 JP2011001951A5 (enExample) | 2013-08-01 |
| JP5507351B2 true 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
Also Published As
| Publication number | Publication date |
|---|---|
| US8328511B2 (en) | 2012-12-11 |
| DE102010017314A1 (de) | 2010-12-23 |
| GB2471185A (en) | 2010-12-22 |
| GB201009834D0 (en) | 2010-07-21 |
| US20100319352A1 (en) | 2010-12-23 |
| CA2705980A1 (en) | 2010-12-17 |
| GB2471185B (en) | 2016-02-03 |
| JP2011001951A (ja) | 2011-01-06 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| A521 | Written amendment |
Free format text: JAPANESE INTERMEDIATE CODE: A523 Effective date: 20130614 |
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| A01 | Written decision to grant a patent or to grant a registration (utility model) |
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| A61 | First payment of annual fees (during grant procedure) |
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| R150 | Certificate of patent or registration of utility model |
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| LAPS | Cancellation because of no payment of annual fees |