GB323941A - Improvements in the rotor and guide blades for steam and gas turbines - Google Patents

Improvements in the rotor and guide blades for steam and gas turbines

Info

Publication number
GB323941A
GB323941A GB288829A GB288829A GB323941A GB 323941 A GB323941 A GB 323941A GB 288829 A GB288829 A GB 288829A GB 288829 A GB288829 A GB 288829A GB 323941 A GB323941 A GB 323941A
Authority
GB
United Kingdom
Prior art keywords
rotor
steam
gas turbines
guide blades
radial
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
GB288829A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to GB288829A priority Critical patent/GB323941A/en
Publication of GB323941A publication Critical patent/GB323941A/en
Expired legal-status Critical Current

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)

Abstract

323,941. Leistritz, P., and Burghauser, F. Jan. 28, 1929. Drawings to Specification. Blades.-A turbine blade surface is generated by a straight line which is moved along terminal guide curves and keeps parallel with a plane normal to the rotor axis. A blade surface may be formed of two or more sections generated by different straight lines. The outlet edge may be radial or the generating line may be radial at an intermediate position.
GB288829A 1929-01-28 1929-01-28 Improvements in the rotor and guide blades for steam and gas turbines Expired GB323941A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB288829A GB323941A (en) 1929-01-28 1929-01-28 Improvements in the rotor and guide blades for steam and gas turbines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB288829A GB323941A (en) 1929-01-28 1929-01-28 Improvements in the rotor and guide blades for steam and gas turbines

Publications (1)

Publication Number Publication Date
GB323941A true GB323941A (en) 1930-01-16

Family

ID=9747889

Family Applications (1)

Application Number Title Priority Date Filing Date
GB288829A Expired GB323941A (en) 1929-01-28 1929-01-28 Improvements in the rotor and guide blades for steam and gas turbines

Country Status (1)

Country Link
GB (1) GB323941A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2001061152A1 (en) * 2000-02-17 2001-08-23 Alstom Power N.V. Aerofoil for an axial flow turbomachine

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2001061152A1 (en) * 2000-02-17 2001-08-23 Alstom Power N.V. Aerofoil for an axial flow turbomachine
US6709233B2 (en) 2000-02-17 2004-03-23 Alstom Power N.V. Aerofoil for an axial flow turbomachine

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