GB1123886A - Double opposed axial-flow elastic fluid turbines - Google Patents

Double opposed axial-flow elastic fluid turbines

Info

Publication number
GB1123886A
GB1123886A GB19623/67A GB1962367A GB1123886A GB 1123886 A GB1123886 A GB 1123886A GB 19623/67 A GB19623/67 A GB 19623/67A GB 1962367 A GB1962367 A GB 1962367A GB 1123886 A GB1123886 A GB 1123886A
Authority
GB
United Kingdom
Prior art keywords
annular wall
radial
shrouds
seals
rows
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
GB19623/67A
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.)
CBS Corp
Original Assignee
Westinghouse Electric Corp
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 Westinghouse Electric Corp filed Critical Westinghouse Electric Corp
Publication of GB1123886A publication Critical patent/GB1123886A/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
    • F01D25/26—Double casings; Measures against temperature strain in casings
    • 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
    • F01D3/00—Machines or engines with axial-thrust balancing effected by working-fluid
    • F01D3/02—Machines or engines with axial-thrust balancing effected by working-fluid characterised by having one fluid flow in one axial direction and another fluid flow in the opposite direction
    • 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
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

1,123,886. Elastic-fluid turbines. WESTINGHOUSE ELECTRIC CORP. April 28, 1967 [June 28, 1966], No. 19623/67. Heading F1T. A central admission double opposed-flow axialflow plastic-fluid turbine comprises a pair of rows of stator vanes 16, 20, Fig. 5, co-operating with a pair of rows of first-stage rotor blades 18 and having shrouds 40, 42 which jointly define in part an annular space 28 into which the motive fluid is admitted, a stationary annular wall 44 spanning the axial space between the rows of stator vanes and having axially opposed peripheral marginal portions 45, 46 disposed in lapping relation with the shrouds 40, 42 with seals 50, 51 interposed between them, the seals being carried by either the shrouds or, as shown, the marginal portions. The seals 50, 51, which permit relative thermal expansion of the parts, are of arcuate segmental form, and located in peripheral grooves 47, 48, each segment being pressed outwards by a leaf spring 52, Figs. 4 and 5, located in the groove. The upper and lower halves 44a, 44b of the annular wall 44 are provided with pairs of diametricallyopposed radial struts 61, 55 respectively which are bolted together to unite the two halves. Each strut 55 has a slot 58 engaged by a key 59 and a bolt 57 carried by a flange 56 fixed to the lower half 21b of the outer casing of the turbine whereby movement of the strut is restricted in all but the radial direction. Additionally, each annular wall half 44a, 44b has a vertical dowel (69), Fig.3 (not shown), engaging a radial bore in a member (67) carried by the outer casing and permitting radial movement only. Radial expansion of the annular wall 44 is thereby allowed.
GB19623/67A 1966-06-28 1967-04-28 Double opposed axial-flow elastic fluid turbines Expired GB1123886A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US561207A US3408045A (en) 1966-06-28 1966-06-28 Turbine nozzle seal structure

Publications (1)

Publication Number Publication Date
GB1123886A true GB1123886A (en) 1968-08-14

Family

ID=24241073

Family Applications (1)

Application Number Title Priority Date Filing Date
GB19623/67A Expired GB1123886A (en) 1966-06-28 1967-04-28 Double opposed axial-flow elastic fluid turbines

Country Status (2)

Country Link
US (1) US3408045A (en)
GB (1) GB1123886A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2512106A1 (en) * 1981-09-03 1983-03-04 Sud Ouest Ind Cie Fse Develop Axial flow thermodynamic turbine - has central inlet between two sets of vaned wheels on common shaft
GB2425809A (en) * 2005-05-06 2006-11-08 Gen Electric Mounting a diaphragm within a steam turbine casing
CN109477398A (en) * 2016-08-16 2019-03-15 通用电器技术有限公司 Axial turbine with a diaphragm divided into two halves at a horizontal joint plane

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE312813B (en) * 1967-07-11 1969-07-28 Stal Laval Turbin Ab
US3529901A (en) * 1968-11-18 1970-09-22 Westinghouse Electric Corp Turbine motive fluid inlet seal structure
US4479756A (en) * 1978-08-21 1984-10-30 Roy E. Roth Company Multi-stage pump
US4871295A (en) * 1983-04-19 1989-10-03 Ormat Turbines (1965) Ltd. Modular rankine cycle vapor turbine
US4764084A (en) * 1987-11-23 1988-08-16 Westinghouse Electric Corp. Inlet flow guide for a low pressure turbine
US4863341A (en) * 1988-05-13 1989-09-05 Westinghouse Electric Corp. Turbine having semi-isolated inlet
EP2772617B1 (en) 2013-02-27 2018-11-28 Ansaldo Energia Switzerland AG Rotary flow machine with support means
WO2014210409A1 (en) * 2013-06-28 2014-12-31 Exxonmobil Upstream Research Company Systems and methods of utilizing axial flow expanders
EP3014077B1 (en) 2013-06-28 2018-01-17 Mitsubishi Heavy Industries Compressor Corporation Axial flow expander

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL302648A (en) *

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2512106A1 (en) * 1981-09-03 1983-03-04 Sud Ouest Ind Cie Fse Develop Axial flow thermodynamic turbine - has central inlet between two sets of vaned wheels on common shaft
GB2425809A (en) * 2005-05-06 2006-11-08 Gen Electric Mounting a diaphragm within a steam turbine casing
US7329098B2 (en) 2005-05-06 2008-02-12 Geenral Electric Company Adjustable support bar with adjustable shim design for steam turbine diaphragms
GB2425809A8 (en) * 2005-05-06 2010-07-07 Gen Electric Adjustable support bar with adjustable shim designfor steam turbine diaphragms
CN109477398A (en) * 2016-08-16 2019-03-15 通用电器技术有限公司 Axial turbine with a diaphragm divided into two halves at a horizontal joint plane
CN109477398B (en) * 2016-08-16 2022-02-15 通用电器技术有限公司 Axial turbine with a diaphragm divided into two halves at a horizontal joint plane

Also Published As

Publication number Publication date
US3408045A (en) 1968-10-29

Similar Documents

Publication Publication Date Title
GB1220904A (en) Diaphragm seal structure
GB1473719A (en) Turbomachines
GB1410658A (en) Turbomachinery rotors
GB1523668A (en) Turbomachinery stator assembly
GB1306575A (en) Segmented seal assembly for axial flow turbines
GB1241358A (en) Static seal structure
GB1277212A (en) A sealing device
GB1109457A (en) Segmented diaphragm assembly for turbines
GB1020900A (en) A seal between the rotor blades and the casing of axial-flow turbo-machines
GB1484936A (en) Gas turbine engines
GB1123886A (en) Double opposed axial-flow elastic fluid turbines
GB1461965A (en) Axial flow turbine structure
GB1249682A (en) Elastic fluid utilizing machine
GB1344221A (en) Vane rings
GB753316A (en) Improvements relating to radial-flow turbines or compressors
GB1095830A (en) Bladed rotor for a fluid flow machine such as a gas turbine engine
GB831412A (en) Improvements relating to axial-flow turbines
GB1010300A (en) Elastic-fluid turbines with multiple casings
GB689270A (en) Improvements in axial flow turbines or compressors
GB1335145A (en) Turbine casing for a gas turbine engine
GB867759A (en) Stator vane assemblies for axial-flow compressors or turbines
GB1018168A (en) Improvements in stator assembly
US3844675A (en) Plural shell axial turbine for operation with high pressure, high temperature steam
GB1511019A (en) Stator construction for an axial flow compressor
GB1454861A (en) Reversible turbine assemblies