GB555868A - Improvements in or relating to turbine blading, especially for gas turbines - Google Patents

Improvements in or relating to turbine blading, especially for gas turbines

Info

Publication number
GB555868A
GB555868A GB15312/41A GB1531241A GB555868A GB 555868 A GB555868 A GB 555868A GB 15312/41 A GB15312/41 A GB 15312/41A GB 1531241 A GB1531241 A GB 1531241A GB 555868 A GB555868 A GB 555868A
Authority
GB
United Kingdom
Prior art keywords
relating
gas turbines
turbine blading
blading
turbine
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
GB15312/41A
Other languages
English (en)
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.)
Rheinmetall Air Defence AG
Maschinenfabrik Oerlikon AG
Original Assignee
Werkzeugmaschinenfabrik Oerlikon Buhrle AG
Maschinenfabrik Oerlikon AG
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 Werkzeugmaschinenfabrik Oerlikon Buhrle AG, Maschinenfabrik Oerlikon AG filed Critical Werkzeugmaschinenfabrik Oerlikon Buhrle AG
Publication of GB555868A publication Critical patent/GB555868A/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
    • F01D5/143Contour of the outer or inner working fluid flow path wall, i.e. shroud or hub contour

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
GB15312/41A 1940-12-07 1941-11-27 Improvements in or relating to turbine blading, especially for gas turbines Expired GB555868A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH555868X 1940-12-07

Publications (1)

Publication Number Publication Date
GB555868A true GB555868A (en) 1943-09-10

Family

ID=4519989

Family Applications (1)

Application Number Title Priority Date Filing Date
GB15312/41A Expired GB555868A (en) 1940-12-07 1941-11-27 Improvements in or relating to turbine blading, especially for gas turbines

Country Status (3)

Country Link
CH (1) CH218193A (de)
FR (1) FR889601A (de)
GB (1) GB555868A (de)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4741667A (en) * 1986-05-28 1988-05-03 United Technologies Corporation Stator vane

Also Published As

Publication number Publication date
FR889601A (fr) 1944-01-14
CH218193A (de) 1941-11-30

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