GB2471185B - Prechorded turbine nozzle - Google Patents
Prechorded turbine nozzleInfo
- Publication number
- GB2471185B GB2471185B GB1009834.1A GB201009834A GB2471185B GB 2471185 B GB2471185 B GB 2471185B GB 201009834 A GB201009834 A GB 201009834A GB 2471185 B GB2471185 B GB 2471185B
- Authority
- GB
- United Kingdom
- Prior art keywords
- prechorded
- turbine nozzle
- turbine
- nozzle
- prechorded turbine
- 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
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 (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US12/486,126 US8328511B2 (en) | 2009-06-17 | 2009-06-17 | Prechorded turbine nozzle |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| GB201009834D0 GB201009834D0 (en) | 2010-07-21 |
| GB2471185A GB2471185A (en) | 2010-12-22 |
| GB2471185B true GB2471185B (en) | 2016-02-03 |
Family
ID=42471536
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB1009834.1A Expired - Fee Related GB2471185B (en) | 2009-06-17 | 2010-06-14 | Prechorded turbine nozzle |
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 |
Citations (10)
| 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 |
| US4759687A (en) * | 1986-04-24 | 1988-07-26 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." | Turbine ring incorporating elements of a ceramic composition divided into sectors |
| 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 |
| EP0907053A2 (en) * | 1997-10-02 | 1999-04-07 | General Electric Company | Apparatus for flanging a separating crown between concentric rings of burners in a multiple combustor |
| US6361273B1 (en) * | 1999-04-01 | 2002-03-26 | Alstom (Switzerland) Ltd | Heat shield for a gas turbine |
| EP1455053A2 (en) * | 2003-03-03 | 2004-09-08 | General Electric Company | Airfoil shape for a turbine nozzle |
| US20060251519A1 (en) * | 2004-10-26 | 2006-11-09 | Bruno Benedetti | Guide vane ring of a turbomachine and associated modification method |
| US20070031245A1 (en) * | 2005-08-06 | 2007-02-08 | General Electric Company | Thermally compliant C-clip |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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 |
| US6183192B1 (en) | 1999-03-22 | 2001-02-06 | General Electric Company | Durable turbine nozzle |
| 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 |
-
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
Patent Citations (10)
| 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 |
| US4759687A (en) * | 1986-04-24 | 1988-07-26 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." | Turbine ring incorporating elements of a ceramic composition divided into sectors |
| 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 |
| EP0907053A2 (en) * | 1997-10-02 | 1999-04-07 | General Electric Company | Apparatus for flanging a separating crown between concentric rings of burners in a multiple combustor |
| US6361273B1 (en) * | 1999-04-01 | 2002-03-26 | Alstom (Switzerland) Ltd | Heat shield for a gas turbine |
| EP1455053A2 (en) * | 2003-03-03 | 2004-09-08 | General Electric Company | Airfoil shape for a turbine nozzle |
| US20060251519A1 (en) * | 2004-10-26 | 2006-11-09 | Bruno Benedetti | Guide vane ring of a turbomachine and associated modification method |
| US20070031245A1 (en) * | 2005-08-06 | 2007-02-08 | General Electric Company | Thermally compliant C-clip |
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 |
| JP5507351B2 (ja) | 2014-05-28 |
| CA2705980A1 (en) | 2010-12-17 |
| JP2011001951A (ja) | 2011-01-06 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 20180614 |