GB535601A - Improvements in and relating to the manufacture of nozzle rings for exhaust gas turbines - Google Patents

Improvements in and relating to the manufacture of nozzle rings for exhaust gas turbines

Info

Publication number
GB535601A
GB535601A GB8541/40A GB854140A GB535601A GB 535601 A GB535601 A GB 535601A GB 8541/40 A GB8541/40 A GB 8541/40A GB 854140 A GB854140 A GB 854140A GB 535601 A GB535601 A GB 535601A
Authority
GB
United Kingdom
Prior art keywords
exhaust gas
gas turbines
relating
manufacture
nozzle
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
GB8541/40A
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.)
BBC Brown Boveri AG Germany
BBC Brown Boveri France SA
Original Assignee
Brown Boveri und Cie AG Germany
BBC Brown Boveri France SA
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 Brown Boveri und Cie AG Germany, BBC Brown Boveri France SA filed Critical Brown Boveri und Cie AG Germany
Publication of GB535601A publication Critical patent/GB535601A/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

535,601. Exhaust gas turbines. AKT.-GES. BROWN, BOVERI & CIE. May 11, 1940, No. 8541. Convention date, May 11, 1939. Drawings to Specification. [Class 110 (iii)] The nozzle hinges of exhaust gas turbines have convergent nozzle passages such that by turning- off the outlet face of a ring the outlet width of the nozzle passage is increased.
GB8541/40A 1939-05-11 1940-05-11 Improvements in and relating to the manufacture of nozzle rings for exhaust gas turbines Expired GB535601A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH535601X 1939-05-11

Publications (1)

Publication Number Publication Date
GB535601A true GB535601A (en) 1941-04-15

Family

ID=4518746

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8541/40A Expired GB535601A (en) 1939-05-11 1940-05-11 Improvements in and relating to the manufacture of nozzle rings for exhaust gas turbines

Country Status (1)

Country Link
GB (1) GB535601A (en)

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