GB230419A - Improvements in high pressure steam turbines - Google Patents

Improvements in high pressure steam turbines

Info

Publication number
GB230419A
GB230419A GB965/25A GB96525A GB230419A GB 230419 A GB230419 A GB 230419A GB 965/25 A GB965/25 A GB 965/25A GB 96525 A GB96525 A GB 96525A GB 230419 A GB230419 A GB 230419A
Authority
GB
United Kingdom
Prior art keywords
passages
high pressure
rotor blade
pressure steam
guide
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
Application number
GB965/25A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Erste Bruenner Maschinen Fabriks Gesellschaft
Original Assignee
Erste Bruenner Maschinen Fabriks Gesellschaft
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 by Erste Bruenner Maschinen Fabriks Gesellschaft filed Critical Erste Bruenner Maschinen Fabriks Gesellschaft
Publication of GB230419A publication Critical patent/GB230419A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/141Shape, i.e. outer, aerodynamic form
    • F01D5/142Shape, i.e. outer, aerodynamic form of the blades of successive rotor or stator blade-rows

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

230,419. Erste Br³nner Maschinen- Fabriks-Ges. March 7, 1924, [Convention date]. Void [Published under Sect. 91 of the Act]. Drawings to Specification. Axial-flow type. - In turbines using steam at high pressures, above 30 atmospheres, the crosssectional areas of the guide and rotor blade passages are so dimensioned that the steam velocity in the guide passages and the relative steam velocity in the rotor blade passages vary in such a manner that, with increasing pressure, the compression shocks in the passages tend to vanish.
GB965/25A 1924-03-07 1925-01-12 Improvements in high pressure steam turbines Expired GB230419A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
AT230419X 1924-03-07

Publications (1)

Publication Number Publication Date
GB230419A true GB230419A (en) 1925-12-17

Family

ID=3669932

Family Applications (1)

Application Number Title Priority Date Filing Date
GB965/25A Expired GB230419A (en) 1924-03-07 1925-01-12 Improvements in high pressure steam turbines

Country Status (1)

Country Link
GB (1) GB230419A (en)

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