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GB216737A - Improvements relating to elastic fluid turbines - Google Patents

Improvements relating to elastic fluid turbines

Info

Publication number
GB216737A
GB216737A GB19818/23A GB1981823A GB216737A GB 216737 A GB216737 A GB 216737A GB 19818/23 A GB19818/23 A GB 19818/23A GB 1981823 A GB1981823 A GB 1981823A GB 216737 A GB216737 A GB 216737A
Authority
GB
United Kingdom
Prior art keywords
improvements relating
elastic fluid
rings
fluid turbines
diaphragms
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
GB19818/23A
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.)
Metropolitan Vickers Electrical Co Ltd
Original Assignee
Metropolitan Vickers Electrical Co Ltd
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 Metropolitan Vickers Electrical Co Ltd filed Critical Metropolitan Vickers Electrical Co Ltd
Priority to GB19818/23A priority Critical patent/GB216737A/en
Publication of GB216737A publication Critical patent/GB216737A/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
    • 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
    • F01D25/246—Fastening of diaphragms or stator-rings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B21/00—Means for preventing relative axial movement of a pin, spigot, shaft or the like and a member surrounding it; Stud-and-socket releasable fastenings
    • F16B21/10—Means for preventing relative axial movement of a pin, spigot, shaft or the like and a member surrounding it; Stud-and-socket releasable fastenings by separate parts
    • F16B21/16—Means for preventing relative axial movement of a pin, spigot, shaft or the like and a member surrounding it; Stud-and-socket releasable fastenings by separate parts with grooves or notches in the pin or shaft
    • F16B21/18—Means for preventing relative axial movement of a pin, spigot, shaft or the like and a member surrounding it; Stud-and-socket releasable fastenings by separate parts with grooves or notches in the pin or shaft with circlips or like resilient retaining devices, i.e. resilient in the plane of the ring or the like; Details
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/60—Assembly methods
    • F05D2230/64—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins
    • F05D2230/642—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins using maintaining alignment while permitting differential dilatation

Landscapes

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

Abstract

216,737. Baumann, K., and Metropolitan-Vickers Electrical Co., Ltd. Aug. 2, 1923. Casings.-In a multistage impulse turbine the diaphragms which are made with radial clearance in the casing are centred by flexible rings 3, Fig. 1. The rings are formed with staggered recesses 6, Fig. 2, on their inner and outer surfaces, with saw-cuts 7, Fig. 3, or with recesses 6 and slots 8, Fig. 6, so that the rings can bend to accommodate expansion of the diaphragms.
GB19818/23A 1923-08-02 1923-08-02 Improvements relating to elastic fluid turbines Expired GB216737A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB19818/23A GB216737A (en) 1923-08-02 1923-08-02 Improvements relating to elastic fluid turbines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB19818/23A GB216737A (en) 1923-08-02 1923-08-02 Improvements relating to elastic fluid turbines

Publications (1)

Publication Number Publication Date
GB216737A true GB216737A (en) 1924-06-05

Family

ID=10135732

Family Applications (1)

Application Number Title Priority Date Filing Date
GB19818/23A Expired GB216737A (en) 1923-08-02 1923-08-02 Improvements relating to elastic fluid turbines

Country Status (1)

Country Link
GB (1) GB216737A (en)

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2654566A (en) * 1950-02-11 1953-10-06 A V Roe Canada Ltd Turbine nozzle guide vane construction
US4305696A (en) * 1979-03-14 1981-12-15 Rolls-Royce Limited Stator vane assembly for a gas turbine engine
FR2514416A1 (en) * 1981-10-14 1983-04-15 Wallace Murray Corp TURBOCHARGER CONSTRUCTION
EP0251125A1 (en) * 1986-06-24 1988-01-07 Klöckner-Humboldt-Deutz Aktiengesellschaft Centering for a casing
EP0331837A1 (en) * 1988-01-11 1989-09-13 General Electric Company Method and device for mounting guide vanes in turbines
WO1991019078A1 (en) * 1990-06-02 1991-12-12 MTU MOTOREN- UND TURBINEN-UNION MüNCHEN GMBH Guide-vane ring for a gas-turbine engine
EP0486082A1 (en) * 1990-11-16 1992-05-20 General Motors Corporation Bearing support for a gas turbine
EP0716219A1 (en) * 1994-12-07 1996-06-12 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Segmented stator ring for a turbomachine
EP0770761A1 (en) * 1995-10-23 1997-05-02 United Technologies Corporation Rotor blade outer tip seal apparatus
WO1999031357A1 (en) * 1997-12-17 1999-06-24 Pratt & Whitney Canada Corp. Support for a turbine stator assembly
EP1548232A1 (en) * 2003-12-23 2005-06-29 Siemens Aktiengesellschaft Turbomachine comprising a stator vane support and method of mounting stator vanes to the stator vane support

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2654566A (en) * 1950-02-11 1953-10-06 A V Roe Canada Ltd Turbine nozzle guide vane construction
US4305696A (en) * 1979-03-14 1981-12-15 Rolls-Royce Limited Stator vane assembly for a gas turbine engine
FR2514416A1 (en) * 1981-10-14 1983-04-15 Wallace Murray Corp TURBOCHARGER CONSTRUCTION
EP0251125A1 (en) * 1986-06-24 1988-01-07 Klöckner-Humboldt-Deutz Aktiengesellschaft Centering for a casing
EP0331837A1 (en) * 1988-01-11 1989-09-13 General Electric Company Method and device for mounting guide vanes in turbines
US5269651A (en) * 1990-06-02 1993-12-14 Mtu Motoren- Und Turbinen-Union Munchen Gmbh Guide vane ring of a turbine of a gas turbine engine
WO1991019078A1 (en) * 1990-06-02 1991-12-12 MTU MOTOREN- UND TURBINEN-UNION MüNCHEN GMBH Guide-vane ring for a gas-turbine engine
EP0486082A1 (en) * 1990-11-16 1992-05-20 General Motors Corporation Bearing support for a gas turbine
EP0716219A1 (en) * 1994-12-07 1996-06-12 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Segmented stator ring for a turbomachine
FR2728015A1 (en) * 1994-12-07 1996-06-14 Snecma SECTORIZED MONOBLOC DISPENSER OF TURBOMACHINE TURBINE STATOR
US5752804A (en) * 1994-12-07 1998-05-19 Societe Nationale D'etude Et De Construction De Monteurs D'aviation "Snecma" Sectored, one-piece nozzle of a turbine engine turbine stator
EP0770761A1 (en) * 1995-10-23 1997-05-02 United Technologies Corporation Rotor blade outer tip seal apparatus
WO1999031357A1 (en) * 1997-12-17 1999-06-24 Pratt & Whitney Canada Corp. Support for a turbine stator assembly
EP1548232A1 (en) * 2003-12-23 2005-06-29 Siemens Aktiengesellschaft Turbomachine comprising a stator vane support and method of mounting stator vanes to the stator vane support
WO2005066463A1 (en) * 2003-12-23 2005-07-21 Siemens Aktiengesellschaft Turbo machine with a vane support and method for mounting vanes on a vane support

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