GB785002A - Rotor for a compressor, turbine or like fluid flow machine - Google Patents

Rotor for a compressor, turbine or like fluid flow machine

Info

Publication number
GB785002A
GB785002A GB1137055A GB1137055A GB785002A GB 785002 A GB785002 A GB 785002A GB 1137055 A GB1137055 A GB 1137055A GB 1137055 A GB1137055 A GB 1137055A GB 785002 A GB785002 A GB 785002A
Authority
GB
United Kingdom
Prior art keywords
discs
rotor
turbine
compressor
flanges
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
GB1137055A
Inventor
Leonard Islip
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.)
Power Jets Research and Development Ltd
Original Assignee
Power Jets Research and Development 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 Power Jets Research and Development Ltd filed Critical Power Jets Research and Development Ltd
Priority to GB1137055A priority Critical patent/GB785002A/en
Publication of GB785002A publication Critical patent/GB785002A/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
    • 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)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

785,002. Turbine and compressor rotors. POWER JETS (RESEARCH & DEVELOPMENT), Ltd. March 12, 1956 [April 20, 1955], No. 11370/55. Class 110 (3). A rotor for a turbine or compressor comprises at least two axially successive discs having on their adjacent faces annular, axially-abutting locating faces, the face on one disc being formed with a circumferentially-extending annular rib having oppositely-tapered flanks which engages between the flanks of a correspondingly tapered circumferentially extending groove formed in the face of the other disc. In the multi-stage axial-flow compressor rotor shown, the end discs 1a each have a single cylindrical flange 3 and the intermediate discs 1 each have two cylindrical flanges 3 on opposite sides thereof, the abutting faces of the flanges being formed with interengaging circumferentially-extending ribs and grooves 7 of screw-thread profile. The flanges 3 are formed with a plurality of bosses 4 which are bored to receive through bolts 5 which serve to retain the discs together. The two end discs have bearer members 6 for supporting the rotor in bearings.
GB1137055A 1955-04-20 1955-04-20 Rotor for a compressor, turbine or like fluid flow machine Expired GB785002A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1137055A GB785002A (en) 1955-04-20 1955-04-20 Rotor for a compressor, turbine or like fluid flow machine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1137055A GB785002A (en) 1955-04-20 1955-04-20 Rotor for a compressor, turbine or like fluid flow machine

Publications (1)

Publication Number Publication Date
GB785002A true GB785002A (en) 1957-10-23

Family

ID=9984996

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1137055A Expired GB785002A (en) 1955-04-20 1955-04-20 Rotor for a compressor, turbine or like fluid flow machine

Country Status (1)

Country Link
GB (1) GB785002A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3745628A (en) * 1971-07-29 1973-07-17 Westinghouse Electric Corp Rotor structure and method of construction
US5288210A (en) * 1991-10-30 1994-02-22 General Electric Company Turbine disk attachment system
EP0919701A1 (en) * 1997-06-12 1999-06-02 Mitsubishi Heavy Industries, Ltd. Sealing structure for joint surfaces of flanges of gas turbine
US20130017092A1 (en) * 2011-07-11 2013-01-17 General Electric Company Rotor assembly for gas turbines
RU2498080C2 (en) * 2008-05-29 2013-11-10 Снекма Radial ring flange, connection of rotor wheel or stator elements and gas-turbine engine
RU2514462C2 (en) * 2008-11-07 2014-04-27 Снекма Radial ring flange, low-pressure turbine for gas turbine engine and gas turbine engine

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3745628A (en) * 1971-07-29 1973-07-17 Westinghouse Electric Corp Rotor structure and method of construction
US5288210A (en) * 1991-10-30 1994-02-22 General Electric Company Turbine disk attachment system
EP0919701A1 (en) * 1997-06-12 1999-06-02 Mitsubishi Heavy Industries, Ltd. Sealing structure for joint surfaces of flanges of gas turbine
EP0919701B1 (en) * 1997-06-12 2003-10-15 Mitsubishi Heavy Industries, Ltd. Sealing structure for joint surfaces of flanges of gas turbine
RU2498080C2 (en) * 2008-05-29 2013-11-10 Снекма Radial ring flange, connection of rotor wheel or stator elements and gas-turbine engine
RU2514462C2 (en) * 2008-11-07 2014-04-27 Снекма Radial ring flange, low-pressure turbine for gas turbine engine and gas turbine engine
US20130017092A1 (en) * 2011-07-11 2013-01-17 General Electric Company Rotor assembly for gas turbines

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