CH284189A - Axial turbine. - Google Patents

Axial turbine.

Info

Publication number
CH284189A
CH284189A CH284189DA CH284189A CH 284189 A CH284189 A CH 284189A CH 284189D A CH284189D A CH 284189DA CH 284189 A CH284189 A CH 284189A
Authority
CH
Switzerland
Prior art keywords
axial turbine
turbine
axial
Prior art date
Application number
Other languages
German (de)
Inventor
Limited Ruston Hornsby
Original Assignee
Ruston & Hornsby 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 Ruston & Hornsby Ltd filed Critical Ruston & Hornsby Ltd
Publication of CH284189A publication Critical patent/CH284189A/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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/08—Heating, heat-insulating or cooling means
    • F01D5/081—Cooling fluid being directed on the side of the rotor disc or at the roots of the blades
    • F01D5/084—Cooling fluid being directed on the side of the rotor disc or at the roots of the blades the fluid circulating at the periphery of a multistage rotor, e.g. of drum type
    • 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
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/001—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between stator blade and rotor
    • 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
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/005—Sealing means between non relatively rotating elements
    • F01D11/006—Sealing the gap between rotor blades or blades and rotor
    • F01D11/008—Sealing the gap between rotor blades or blades and rotor by spacer elements between the blades, e.g. independent interblade platforms
    • 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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/06—Rotors for more than one axial stage, e.g. of drum or multiple disc type; Details thereof, e.g. shafts, shaft connections
    • F01D5/066—Connecting means for joining rotor-discs or rotor-elements together, e.g. by a central bolt, by clamps

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
CH284189D 1949-04-29 1950-04-28 Axial turbine. CH284189A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB284189X 1949-04-29

Publications (1)

Publication Number Publication Date
CH284189A true CH284189A (en) 1952-07-15

Family

ID=10275321

Family Applications (1)

Application Number Title Priority Date Filing Date
CH284189D CH284189A (en) 1949-04-29 1950-04-28 Axial turbine.

Country Status (4)

Country Link
US (1) US2743080A (en)
CH (1) CH284189A (en)
GB (1) GB667194A (en)
NL (1) NL72215C (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2901214A (en) * 1954-04-12 1959-08-25 Arthur J Slemmons Turbine wheel and shaft assembly
FR2295226A1 (en) * 1974-12-16 1976-07-16 Europ Turb Vapeur Turbine rotor disc mounting - uses tongue and groove dowel to accommodate radial displacements

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1044527B (en) * 1955-07-16 1958-11-20 Canadian Patents Dev Device for connecting a hollow turbine shaft, in particular in the case of a gas turbine engine, with a cantilevered turbine impeller
US3692429A (en) * 1971-02-01 1972-09-19 Westinghouse Electric Corp Rotor structure and method of broaching the same
US3745628A (en) * 1971-07-29 1973-07-17 Westinghouse Electric Corp Rotor structure and method of construction
DE2140816A1 (en) * 1971-08-14 1973-03-01 Motoren Turbinen Union ROTOR FOR FLOW MACHINERY
FR2404134A1 (en) * 1977-09-23 1979-04-20 Snecma ROTOR FOR TURBOMACHINES
US5031400A (en) * 1988-12-09 1991-07-16 Allied-Signal Inc. High temperature turbine engine structure
FR2690202B1 (en) * 1992-04-17 1995-07-07 Alsthom Gec IMPROVEMENTS ON HIGH PRESSURE MODULES OF TURBINE ROTOR TURBINE WITH VAPOR INTAKE OF VERY HIGH CHARACTERISTICS.
GB2293628B (en) * 1994-09-27 1998-04-01 Europ Gas Turbines Ltd Turbines
US20130017092A1 (en) * 2011-07-11 2013-01-17 General Electric Company Rotor assembly for gas turbines
US10385861B2 (en) * 2012-10-03 2019-08-20 Praxair Technology, Inc. Method for compressing an incoming feed air stream in a cryogenic air separation plant
US10443603B2 (en) 2012-10-03 2019-10-15 Praxair Technology, Inc. Method for compressing an incoming feed air stream in a cryogenic air separation plant
US9371835B2 (en) * 2013-07-19 2016-06-21 Praxair Technology, Inc. Coupling for directly driven compressor
CN107269316A (en) * 2017-08-17 2017-10-20 中南大学 A kind of disc of conical profile structure of gas turbine central draw bar type rotor

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB599809A (en) * 1945-01-15 1948-03-22 Bristol Aeroplane Co Ltd Improvements in axial flow compressors, turbines and the like
GB319622A (en) * 1928-09-24 1930-12-18 Vladimir Kalabek Gas turbine
NL66706C (en) * 1944-10-06
US2497151A (en) * 1946-03-04 1950-02-14 Armstrong Siddeley Motors Ltd Multidisk rotor
US2430185A (en) * 1946-07-25 1947-11-04 Continental Aviat & Engineerin Turbine rotor
GB612097A (en) * 1946-10-09 1948-11-08 English Electric Co Ltd Improvements in and relating to the cooling of gas turbine rotors

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2901214A (en) * 1954-04-12 1959-08-25 Arthur J Slemmons Turbine wheel and shaft assembly
FR2295226A1 (en) * 1974-12-16 1976-07-16 Europ Turb Vapeur Turbine rotor disc mounting - uses tongue and groove dowel to accommodate radial displacements

Also Published As

Publication number Publication date
NL72215C (en)
US2743080A (en) 1956-04-24
GB667194A (en) 1952-02-27

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