SE0102967D0 - A connecting device for a turbine - Google Patents

A connecting device for a turbine

Info

Publication number
SE0102967D0
SE0102967D0 SE0102967A SE0102967A SE0102967D0 SE 0102967 D0 SE0102967 D0 SE 0102967D0 SE 0102967 A SE0102967 A SE 0102967A SE 0102967 A SE0102967 A SE 0102967A SE 0102967 D0 SE0102967 D0 SE 0102967D0
Authority
SE
Sweden
Prior art keywords
conduit
stator part
inlet
outlet
turbine
Prior art date
Application number
SE0102967A
Other languages
Swedish (sv)
Other versions
SE520577C2 (en
SE0102967L (en
Original Assignee
Turbec 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 Turbec Ab filed Critical Turbec Ab
Priority to SE0102967A priority Critical patent/SE520577C2/en
Publication of SE0102967D0 publication Critical patent/SE0102967D0/en
Priority to PCT/SE2002/001599 priority patent/WO2003023192A1/en
Publication of SE0102967L publication Critical patent/SE0102967L/en
Publication of SE520577C2 publication Critical patent/SE520577C2/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
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/026—Scrolls for radial machines or engines
    • 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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/243—Flange connections; Bolting arrangements

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Rigid Pipes And Flexible Pipes (AREA)
  • Joints Allowing Movement (AREA)
  • Quick-Acting Or Multi-Walled Pipe Joints (AREA)

Abstract

A gas turbine unit (20) has a conduit (10) comprising two halves, a first half (loa) and a second half (lOb) , assembled together. The conduit has an inlet (10') in the tangential direction and an outlet (10") in the radial direction. An inlet (301) of a stator part (30) is received inside the outlet of the conduit, whereby the conduit is securely connected to the stator part by a pressure exerted in the axial direction of the gas turbine unit against the inlet of the stator part when the conduit and the stator part are assembled together.
SE0102967A 2001-09-07 2001-09-07 Conduction for a gas turbine unit and a method for manufacturing a conduit for a gas turbine unit SE520577C2 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
SE0102967A SE520577C2 (en) 2001-09-07 2001-09-07 Conduction for a gas turbine unit and a method for manufacturing a conduit for a gas turbine unit
PCT/SE2002/001599 WO2003023192A1 (en) 2001-09-07 2002-09-06 A conduit for a gas turbine unit and a method of manufacturing a conduit

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE0102967A SE520577C2 (en) 2001-09-07 2001-09-07 Conduction for a gas turbine unit and a method for manufacturing a conduit for a gas turbine unit

Publications (3)

Publication Number Publication Date
SE0102967D0 true SE0102967D0 (en) 2001-09-07
SE0102967L SE0102967L (en) 2003-03-08
SE520577C2 SE520577C2 (en) 2003-07-29

Family

ID=20285250

Family Applications (1)

Application Number Title Priority Date Filing Date
SE0102967A SE520577C2 (en) 2001-09-07 2001-09-07 Conduction for a gas turbine unit and a method for manufacturing a conduit for a gas turbine unit

Country Status (2)

Country Link
SE (1) SE520577C2 (en)
WO (1) WO2003023192A1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10325649B4 (en) * 2003-06-06 2014-10-23 Ihi Charging Systems International Gmbh Exhaust gas turbine for an exhaust gas turbocharger

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2801043A (en) * 1954-08-24 1957-07-30 Thompson Prod Inc Turbine supercharger
GB1199158A (en) * 1966-11-25 1970-07-15 Cav Ltd Casings for Radial Flow Fluid Turbines e.g. of Turbo-Superchargers for I.C. Engines
GB1263932A (en) * 1969-06-27 1972-02-16 Cav Ltd Turbo superchargers
GB1426554A (en) * 1972-04-13 1976-03-03 Cav Ltd Turbo superchargers for internal combustion engines
EP0646699B1 (en) * 1993-09-03 1998-04-22 Asea Brown Boveri Ag Method for adapting the radial turbine of a turbocharger on an internal combustion engine

Also Published As

Publication number Publication date
WO2003023192A1 (en) 2003-03-20
SE520577C2 (en) 2003-07-29
SE0102967L (en) 2003-03-08

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Legal Events

Date Code Title Description
NUG Patent has lapsed