IE54653B1 - Rotor blade for the first stage of a combustion turbine - Google Patents
Rotor blade for the first stage of a combustion turbineInfo
- Publication number
- IE54653B1 IE54653B1 IE2335/83A IE233583A IE54653B1 IE 54653 B1 IE54653 B1 IE 54653B1 IE 2335/83 A IE2335/83 A IE 2335/83A IE 233583 A IE233583 A IE 233583A IE 54653 B1 IE54653 B1 IE 54653B1
- Authority
- IE
- Ireland
- Prior art keywords
- airfoil
- blade
- decreases
- inch
- radius
- Prior art date
Links
- 238000002485 combustion reaction Methods 0.000 title claims abstract description 8
- 238000001816 cooling Methods 0.000 claims description 25
- 230000007423 decrease Effects 0.000 claims description 22
- 239000002826 coolant Substances 0.000 claims description 6
- 230000003247 decreasing effect Effects 0.000 claims description 4
- 239000007789 gas Substances 0.000 description 14
- 238000011161 development Methods 0.000 description 13
- 238000000034 method Methods 0.000 description 13
- 238000009826 distribution Methods 0.000 description 11
- 230000008569 process Effects 0.000 description 10
- 238000012546 transfer Methods 0.000 description 7
- 238000004458 analytical method Methods 0.000 description 5
- 238000004364 calculation method Methods 0.000 description 5
- 238000013461 design Methods 0.000 description 4
- 230000006872 improvement Effects 0.000 description 4
- 239000013598 vector Substances 0.000 description 4
- 230000008859 change Effects 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 238000012938 design process Methods 0.000 description 2
- 238000010248 power generation Methods 0.000 description 2
- 238000012360 testing method Methods 0.000 description 2
- 101100432968 Mus musculus Yrdc gene Proteins 0.000 description 1
- 229910000086 alane Inorganic materials 0.000 description 1
- 230000004075 alteration Effects 0.000 description 1
- 238000007630 basic procedure Methods 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 238000004590 computer program Methods 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 230000002452 interceptive effect Effects 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
- 238000011144 upstream manufacturing Methods 0.000 description 1
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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/141—Shape, i.e. outer, aerodynamic form
-
- 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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
-
- 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
- F05D2240/00—Components
- F05D2240/20—Rotors
- F05D2240/30—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
- F05D2240/301—Cross-sectional characteristics
-
- 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)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US43610282A | 1982-10-22 | 1982-10-22 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| IE832335L IE832335L (en) | 1984-04-22 |
| IE54653B1 true IE54653B1 (en) | 1989-12-20 |
Family
ID=23731117
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| IE2335/83A IE54653B1 (en) | 1982-10-22 | 1983-10-04 | Rotor blade for the first stage of a combustion turbine |
Country Status (12)
| Country | Link |
|---|---|
| EP (1) | EP0112003B1 (enExample) |
| JP (1) | JPS59131704A (enExample) |
| KR (1) | KR910010034B1 (enExample) |
| AU (1) | AU568313B2 (enExample) |
| BR (1) | BR8305902A (enExample) |
| CA (1) | CA1210334A (enExample) |
| DE (1) | DE3377925D1 (enExample) |
| ES (1) | ES8504330A1 (enExample) |
| IE (1) | IE54653B1 (enExample) |
| IL (1) | IL69920A (enExample) |
| IN (1) | IN158893B (enExample) |
| MX (1) | MX157076A (enExample) |
Families Citing this family (19)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5088894A (en) * | 1990-05-02 | 1992-02-18 | Westinghouse Electric Corp. | Turbomachine blade fastening |
| US5286169A (en) * | 1992-12-15 | 1994-02-15 | General Electric Company | Bucket for the next-to-last stage of a steam turbine |
| US5352092A (en) * | 1993-11-24 | 1994-10-04 | Westinghouse Electric Corporation | Light weight steam turbine blade |
| US5980209A (en) * | 1997-06-27 | 1999-11-09 | General Electric Co. | Turbine blade with enhanced cooling and profile optimization |
| US6461110B1 (en) | 2001-07-11 | 2002-10-08 | General Electric Company | First-stage high pressure turbine bucket airfoil |
| US6503054B1 (en) * | 2001-07-13 | 2003-01-07 | General Electric Company | Second-stage turbine nozzle airfoil |
| WO2003006797A1 (en) * | 2001-07-13 | 2003-01-23 | General Electric Company | Second-stage turbine nozzle airfoil |
| US6461109B1 (en) * | 2001-07-13 | 2002-10-08 | General Electric Company | Third-stage turbine nozzle airfoil |
| US7648340B2 (en) | 2005-12-29 | 2010-01-19 | Rolls-Royce Power Engineering Plc | First stage turbine airfoil |
| US7625184B2 (en) | 2005-12-29 | 2009-12-01 | Rolls-Royce Power Engineering Plc | Second stage turbine airfoil |
| CA2633334C (en) | 2005-12-29 | 2014-11-25 | Rolls-Royce Power Engineering Plc | Airfoil for a first stage nozzle guide vane |
| US7632072B2 (en) | 2005-12-29 | 2009-12-15 | Rolls-Royce Power Engineering Plc | Third stage turbine airfoil |
| CA2633337C (en) | 2005-12-29 | 2014-11-18 | Rolls-Royce Power Engineering Plc | Airfoil for a second stage nozzle guide vane |
| US7722329B2 (en) | 2005-12-29 | 2010-05-25 | Rolls-Royce Power Engineering Plc | Airfoil for a third stage nozzle guide vane |
| DE102008031781B4 (de) * | 2008-07-04 | 2020-06-10 | Man Energy Solutions Se | Schaufelgitter für eine Strömungsmaschine und Strömungsmaschine mit einem solchen Schaufelgitter |
| JP5946707B2 (ja) * | 2012-07-06 | 2016-07-06 | 三菱日立パワーシステムズ株式会社 | 軸流タービン動翼 |
| FR3089550B1 (fr) * | 2018-12-11 | 2021-01-22 | Safran Aircraft Engines | Aube de turbomachine a loi d’epaisseur maximale a forte marge au flottement |
| FR3089553B1 (fr) * | 2018-12-11 | 2021-01-22 | Safran Aircraft Engines | Aube de turbomachine a loi de fleche a forte marge au flottement |
| JP2025165430A (ja) * | 2024-04-23 | 2025-11-05 | 三菱重工業株式会社 | 軸流圧縮機、及びその動翼 |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1548613A (en) * | 1924-03-21 | 1925-08-04 | Aeg | Elastic-fluid turbine |
| GB686807A (en) * | 1950-11-14 | 1953-01-28 | British Thomson Houston Co Ltd | Improvements in and relating to blades for compressors and the like |
| US4111604A (en) * | 1976-07-12 | 1978-09-05 | General Electric Company | Bucket tip construction for open circuit liquid cooled turbines |
-
1983
- 1983-10-04 IE IE2335/83A patent/IE54653B1/en not_active IP Right Cessation
- 1983-10-06 IL IL69920A patent/IL69920A/xx not_active IP Right Cessation
- 1983-10-06 IN IN1238/CAL/83A patent/IN158893B/en unknown
- 1983-10-07 AU AU19963/83A patent/AU568313B2/en not_active Ceased
- 1983-10-19 EP EP83306343A patent/EP0112003B1/en not_active Expired
- 1983-10-19 DE DE8383306343T patent/DE3377925D1/de not_active Expired
- 1983-10-20 CA CA000439371A patent/CA1210334A/en not_active Expired
- 1983-10-20 JP JP58196934A patent/JPS59131704A/ja active Granted
- 1983-10-21 ES ES526667A patent/ES8504330A1/es not_active Expired
- 1983-10-21 BR BR8305902A patent/BR8305902A/pt not_active IP Right Cessation
- 1983-10-21 MX MX199169A patent/MX157076A/es unknown
- 1983-10-22 KR KR1019830005009A patent/KR910010034B1/ko not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| EP0112003B1 (en) | 1988-09-07 |
| BR8305902A (pt) | 1984-05-29 |
| JPH0312641B2 (enExample) | 1991-02-20 |
| CA1210334A (en) | 1986-08-26 |
| IN158893B (enExample) | 1987-02-14 |
| IL69920A0 (en) | 1984-01-31 |
| JPS59131704A (ja) | 1984-07-28 |
| MX157076A (es) | 1988-10-26 |
| AU1996383A (en) | 1984-05-03 |
| ES526667A0 (es) | 1985-04-16 |
| EP0112003A1 (en) | 1984-06-27 |
| AU568313B2 (en) | 1987-12-24 |
| ES8504330A1 (es) | 1985-04-16 |
| KR910010034B1 (ko) | 1991-12-10 |
| IL69920A (en) | 1988-10-31 |
| IE832335L (en) | 1984-04-22 |
| DE3377925D1 (en) | 1988-10-13 |
| KR840006397A (ko) | 1984-11-29 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| MM4A | Patent lapsed |