SE8001888L - TURBINE - Google Patents

TURBINE

Info

Publication number
SE8001888L
SE8001888L SE8001888A SE8001888A SE8001888L SE 8001888 L SE8001888 L SE 8001888L SE 8001888 A SE8001888 A SE 8001888A SE 8001888 A SE8001888 A SE 8001888A SE 8001888 L SE8001888 L SE 8001888L
Authority
SE
Sweden
Prior art keywords
guide blade
blade ring
turbine
guide
united
Prior art date
Application number
SE8001888A
Other languages
Swedish (sv)
Other versions
SE420632B (en
Inventor
M Mansson
Original Assignee
Stal Laval Turbin Ab
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 Stal Laval Turbin Ab filed Critical Stal Laval Turbin Ab
Priority to SE8001888A priority Critical patent/SE420632B/en
Publication of SE8001888L publication Critical patent/SE8001888L/en
Publication of SE420632B publication Critical patent/SE420632B/en

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
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/02—Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

Turbine with one or more guide blade rings 3 which are constructed from a number of radially oriented guide blades 1, 2 which at their outer ends are inserted in an outer guide blade ring 4 and which at their inner ends are united with an inner guide blade ring 6. The inner guide blade ring consists of an outer first portion 6a and an inner second portion 6b and also a third zigzag formed portion 6c, 6d, 6e, 6f, 6g containing one or more annular parts 6c, 6d, with a generally axial orientation. <IMAGE>
SE8001888A 1980-03-11 1980-03-11 Turbine with one or more guide blade rings SE420632B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SE8001888A SE420632B (en) 1980-03-11 1980-03-11 Turbine with one or more guide blade rings

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE8001888A SE420632B (en) 1980-03-11 1980-03-11 Turbine with one or more guide blade rings

Publications (2)

Publication Number Publication Date
SE8001888L true SE8001888L (en) 1981-09-12
SE420632B SE420632B (en) 1981-10-19

Family

ID=20340475

Family Applications (1)

Application Number Title Priority Date Filing Date
SE8001888A SE420632B (en) 1980-03-11 1980-03-11 Turbine with one or more guide blade rings

Country Status (1)

Country Link
SE (1) SE420632B (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE459683B (en) * 1987-11-19 1989-07-24 Abb Stal Ab GAS TURBIN WITH LINKING INSTALLATION OF A SEALING RING IN A LED ROVER WIRE
FR3115819B1 (en) * 2020-11-02 2023-04-14 Safran Aircraft Engines Aircraft turbomachine stator assembly, comprising an external structure formed of two annular sections surrounding a bladed stator crown

Also Published As

Publication number Publication date
SE420632B (en) 1981-10-19

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