GB919042A - Radial flow turbines for compressible working fluids - Google Patents

Radial flow turbines for compressible working fluids

Info

Publication number
GB919042A
GB919042A GB946160A GB946160A GB919042A GB 919042 A GB919042 A GB 919042A GB 946160 A GB946160 A GB 946160A GB 946160 A GB946160 A GB 946160A GB 919042 A GB919042 A GB 919042A
Authority
GB
United Kingdom
Prior art keywords
march
rotor
radial flow
passage
working fluids
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
GB946160A
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 AG
Original Assignee
Sulzer AG
Gebrueder Sulzer 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 Sulzer AG, Gebrueder Sulzer AG filed Critical Sulzer AG
Publication of GB919042A publication Critical patent/GB919042A/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
    • F01D17/00—Regulating or controlling by varying flow
    • F01D17/10—Final actuators
    • F01D17/12—Final actuators arranged in stator parts
    • F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/141—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of shiftable members or valves obturating part of the flow path
    • F01D17/143—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of shiftable members or valves obturating part of the flow path the shiftable member being a wall, or part thereof of a radial diffuser
    • 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
    • F01D15/00—Adaptations of machines or engines for special use; Combinations of engines with devices driven thereby
    • F01D15/005—Adaptations for refrigeration plants
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Centrifugal Separators (AREA)

Abstract

919,042. Elastic-fluid turbines. SULZER FRERES S.A. March 17, 1960 [March 18, 1959], No. 9461/60. Class 110 (3). The rotor 2 of a radial inward flow reaction turbine rotates in a casing which is centrally divided into two parts 2 and 3 and formed with a spiral passage 7 opening directly on to the rotor without the interposition of guide blades. A collection channel 13 into which solid or liquid impurities are thrown by centrifugal force, communicates with the outer periphery of the spiral passage. The impurities are expelled through a pipe 14 when its valve 15 is opened. The cross-section of the passage 7 is substantially hexagonal and the opposite walls 8, parallel to the central division plane of the casing comprise partitions 8 connected to mechanism 10, 11, so as to be displaceable axially relative to the turbine.
GB946160A 1959-03-18 1960-03-17 Radial flow turbines for compressible working fluids Expired GB919042A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH7099459A CH365088A (en) 1959-03-18 1959-03-18 Radial turbine for compressible working media

Publications (1)

Publication Number Publication Date
GB919042A true GB919042A (en) 1963-02-20

Family

ID=4530690

Family Applications (1)

Application Number Title Priority Date Filing Date
GB946160A Expired GB919042A (en) 1959-03-18 1960-03-17 Radial flow turbines for compressible working fluids

Country Status (2)

Country Link
CH (1) CH365088A (en)
GB (1) GB919042A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3628177A1 (en) * 1986-08-20 1988-02-25 Klein Schanzlin & Becker Ag MANIFOLD HOUSING FOR FLOWING MACHINES WITH RADIAL FLOW

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3628177A1 (en) * 1986-08-20 1988-02-25 Klein Schanzlin & Becker Ag MANIFOLD HOUSING FOR FLOWING MACHINES WITH RADIAL FLOW

Also Published As

Publication number Publication date
CH365088A (en) 1962-10-31

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