DD125284A1 - - Google Patents

Info

Publication number
DD125284A1
DD125284A1 DD193002A DD19300276A DD125284A1 DD 125284 A1 DD125284 A1 DD 125284A1 DD 193002 A DD193002 A DD 193002A DD 19300276 A DD19300276 A DD 19300276A DD 125284 A1 DD125284 A1 DD 125284A1
Authority
DD
German Democratic Republic
Application number
DD193002A
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed filed Critical
Publication of DD125284A1 publication Critical patent/DD125284A1/xx

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)
DD193002A 1975-05-31 1976-05-25 DD125284A1 (xx)

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
DD125284A1 true DD125284A1 (xx) 1977-04-13

Family

ID=5947952

Family Applications (1)

Application Number Title Priority Date Filing Date
DD193002A DD125284A1 (xx) 1975-05-31 1976-05-25

Country Status (7)

Country Link
US (1) US4080102A (xx)
JP (1) JPS51145008A (xx)
CH (1) CH596435A5 (xx)
CS (1) CS183840B2 (xx)
DD (1) DD125284A1 (xx)
DE (1) DE2524250A1 (xx)
GB (1) GB1500858A (xx)

Families Citing this family (20)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

Also Published As

Publication number Publication date
JPS561443B2 (xx) 1981-01-13
JPS51145008A (en) 1976-12-13
CS183840B2 (en) 1978-07-31
US4080102A (en) 1978-03-21
DE2524250A1 (de) 1976-12-02
GB1500858A (en) 1978-02-15
CH596435A5 (xx) 1978-03-15

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