GB476222A - Guiding means for turbo-machines - Google Patents

Guiding means for turbo-machines

Info

Publication number
GB476222A
GB476222A GB12242/37A GB1224237A GB476222A GB 476222 A GB476222 A GB 476222A GB 12242/37 A GB12242/37 A GB 12242/37A GB 1224237 A GB1224237 A GB 1224237A GB 476222 A GB476222 A GB 476222A
Authority
GB
United Kingdom
Prior art keywords
disc
grooves
ring
turbo
machines
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
GB12242/37A
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.)
Sulzer Escher Wyss GmbH
Original Assignee
Escher Wyss Maschinenfabriken 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 Escher Wyss Maschinenfabriken AG filed Critical Escher Wyss Maschinenfabriken AG
Publication of GB476222A publication Critical patent/GB476222A/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
    • F01D9/00Stators
    • F01D9/02Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/041Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using blades
    • 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
    • F01D9/00Stators
    • F01D9/02Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/042Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

476,222. Turbines. ESCHER WYSS MASCHINENFABRIKEN AKT.-GES. April 29, 1937, No. 12242. Convention date, May 27, 1936. [Class 110 (iii)] In a blade system in which the ends of the blades are separated by shaped distance pieces 7, 8 inserted in grooves in a ring 2 and a disc 3, the distance pieces for the grooves 7 and 8 respectively are differently formed so that the thin bladings are twisted during assembly to produce, preferably, a leaving angle which increases with the radius. The ring 2 is connected to the disc 3 by stream-lined pillars 1.
GB12242/37A 1936-05-27 1937-04-29 Guiding means for turbo-machines Expired GB476222A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH476222X 1936-05-27

Publications (1)

Publication Number Publication Date
GB476222A true GB476222A (en) 1937-12-03

Family

ID=4516163

Family Applications (1)

Application Number Title Priority Date Filing Date
GB12242/37A Expired GB476222A (en) 1936-05-27 1937-04-29 Guiding means for turbo-machines

Country Status (5)

Country Link
BE (1) BE421412A (en)
DE (1) DE658594C (en)
FR (1) FR821330A (en)
GB (1) GB476222A (en)
NL (1) NL46195C (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3942203C2 (en) * 1988-12-29 2001-04-26 Gen Electric Turbine frame arrangement
WO2008081485A1 (en) * 2007-01-04 2008-07-10 Ansaldo Energia S.P.A. 'highly corrosion-resistant fixed blade assembly for a steam turbine, in particular a geothermal impulse turbine'
EP3492701A1 (en) * 2017-12-01 2019-06-05 MTU Aero Engines GmbH Turbomachine flow channel
US11371370B2 (en) 2017-07-19 2022-06-28 MTU Aero Engines AG Flow arrangement for placing in a hot gas duct of a turbomachine

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3942203C2 (en) * 1988-12-29 2001-04-26 Gen Electric Turbine frame arrangement
WO2008081485A1 (en) * 2007-01-04 2008-07-10 Ansaldo Energia S.P.A. 'highly corrosion-resistant fixed blade assembly for a steam turbine, in particular a geothermal impulse turbine'
JP2010515849A (en) * 2007-01-04 2010-05-13 アンサルド エネルジア エス.ピー.エー. High corrosion resistant fixed blade assembly for steam turbines, especially geothermal impulse turbines
US11371370B2 (en) 2017-07-19 2022-06-28 MTU Aero Engines AG Flow arrangement for placing in a hot gas duct of a turbomachine
EP3492701A1 (en) * 2017-12-01 2019-06-05 MTU Aero Engines GmbH Turbomachine flow channel
US11396812B2 (en) 2017-12-01 2022-07-26 MTU Aero Engines AG Flow channel for a turbomachine

Also Published As

Publication number Publication date
BE421412A (en)
DE658594C (en) 1938-04-06
FR821330A (en) 1937-12-02
NL46195C (en)

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