CS183840B2 - High peripheral velocity running blade arch for thermal turbine machines with axial flow - Google Patents
High peripheral velocity running blade arch for thermal turbine machines with axial flowInfo
- Publication number
- CS183840B2 CS183840B2 CS7600003486A CS348676A CS183840B2 CS 183840 B2 CS183840 B2 CS 183840B2 CS 7600003486 A CS7600003486 A CS 7600003486A CS 348676 A CS348676 A CS 348676A CS 183840 B2 CS183840 B2 CS 183840B2
- Authority
- CS
- Czechoslovakia
- Prior art keywords
- axial flow
- thermal turbine
- peripheral velocity
- high peripheral
- turbine machines
- Prior art date
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
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19752524250 DE2524250A1 (de) | 1975-05-31 | 1975-05-31 | Laufschaufelkranz grosser umfangsgeschwindigkeit fuer thermische, axial durchstroemte turbomaschinen |
Publications (1)
Publication Number | Publication Date |
---|---|
CS183840B2 true CS183840B2 (en) | 1978-07-31 |
Family
ID=5947952
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CS7600003486A CS183840B2 (en) | 1975-05-31 | 1976-05-25 | High peripheral velocity running blade arch for thermal turbine machines with axial flow |
Country Status (7)
Country | Link |
---|---|
US (1) | US4080102A (cs) |
JP (1) | JPS51145008A (cs) |
CH (1) | CH596435A5 (cs) |
CS (1) | CS183840B2 (cs) |
DD (1) | DD125284A1 (cs) |
DE (1) | DE2524250A1 (cs) |
GB (1) | GB1500858A (cs) |
Families Citing this family (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS55123301A (en) * | 1979-03-16 | 1980-09-22 | Hitachi Ltd | Turbine blade |
US4968216A (en) * | 1984-10-12 | 1990-11-06 | The Boeing Company | Two-stage fluid driven turbine |
US4900230A (en) * | 1989-04-27 | 1990-02-13 | Westinghouse Electric Corp. | Low pressure end blade for a low pressure steam turbine |
US5088894A (en) * | 1990-05-02 | 1992-02-18 | Westinghouse Electric Corp. | Turbomachine blade fastening |
US5192193A (en) * | 1991-06-21 | 1993-03-09 | Ingersoll-Dresser Pump Company | Impeller for centrifugal pumps |
US5197854A (en) * | 1991-09-05 | 1993-03-30 | Industrial Design Laboratories, Inc. | Axial flow fan |
JP2710729B2 (ja) * | 1992-06-16 | 1998-02-10 | 株式会社日立製作所 | 軸流タービンの動翼 |
US5292230A (en) * | 1992-12-16 | 1994-03-08 | Westinghouse Electric Corp. | Curvature steam turbine vane airfoil |
DE10054244C2 (de) * | 2000-11-02 | 2002-10-10 | Honda Motor Co Ltd | Turbinenblattanordnung und Turbinenblatt für eine Axialturbine |
US6682301B2 (en) | 2001-10-05 | 2004-01-27 | General Electric Company | Reduced shock transonic airfoil |
JP3836050B2 (ja) * | 2002-06-07 | 2006-10-18 | 三菱重工業株式会社 | タービン動翼 |
US7685713B2 (en) * | 2005-08-09 | 2010-03-30 | Honeywell International Inc. | Process to minimize turbine airfoil downstream shock induced flowfield disturbance |
US8998582B2 (en) | 2010-11-15 | 2015-04-07 | Sundyne, Llc | Flow vector control for high speed centrifugal pumps |
JP6030853B2 (ja) * | 2011-06-29 | 2016-11-24 | 三菱日立パワーシステムズ株式会社 | タービン動翼及び軸流タービン |
US8998577B2 (en) * | 2011-11-03 | 2015-04-07 | General Electric Company | Turbine last stage flow path |
JP5999348B2 (ja) * | 2012-10-31 | 2016-09-28 | 株式会社Ihi | タービン翼 |
US10018075B2 (en) * | 2015-04-22 | 2018-07-10 | General Electric Company | Methods for positioning neighboring nozzles of a gas turbine engine |
JP6684593B2 (ja) * | 2016-01-07 | 2020-04-22 | 三菱重工業株式会社 | 軸流タービン |
US10443607B2 (en) * | 2016-04-11 | 2019-10-15 | Rolls-Royce Plc | Blade for an axial flow machine |
US10935041B2 (en) * | 2016-06-29 | 2021-03-02 | Rolls-Royce Corporation | Pressure recovery axial-compressor blading |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US874993A (en) * | 1906-07-09 | 1907-12-31 | Gen Electric | Bucket for turbines. |
CH85284A (de) * | 1917-12-03 | 1920-06-16 | Ver Dampfturbinen Ges Mit Besc | Leitapparat für Gas oder Dampf. |
US1504710A (en) * | 1922-04-01 | 1924-08-12 | Allis Chalmers Mfg Co | Rotor |
US1553627A (en) * | 1922-06-07 | 1925-09-15 | Allis Chalmers Mfg Co | Rotor |
US2918254A (en) * | 1954-05-10 | 1959-12-22 | Hausammann Werner | Turborunner |
DE1053713B (de) * | 1956-09-29 | 1959-03-26 | Messerschmitt Boelkow Blohm | Verdichter mit relativer UEberschallgeschwindigkeit des Stroemungsmediums im Laufrad |
US3565548A (en) * | 1969-01-24 | 1971-02-23 | Gen Electric | Transonic buckets for axial flow turbines |
US3820918A (en) * | 1972-01-21 | 1974-06-28 | N A S A | Supersonic fan blading |
-
1975
- 1975-05-31 DE DE19752524250 patent/DE2524250A1/de active Pending
-
1976
- 1976-05-17 CH CH611376A patent/CH596435A5/xx not_active IP Right Cessation
- 1976-05-25 DD DD193002A patent/DD125284A1/xx unknown
- 1976-05-25 CS CS7600003486A patent/CS183840B2/cs unknown
- 1976-05-28 GB GB22274/76A patent/GB1500858A/en not_active Expired
- 1976-05-28 JP JP51062168A patent/JPS51145008A/ja active Granted
- 1976-06-01 US US05/691,291 patent/US4080102A/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
JPS561443B2 (cs) | 1981-01-13 |
JPS51145008A (en) | 1976-12-13 |
US4080102A (en) | 1978-03-21 |
DE2524250A1 (de) | 1976-12-02 |
GB1500858A (en) | 1978-02-15 |
DD125284A1 (cs) | 1977-04-13 |
CH596435A5 (cs) | 1978-03-15 |
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