GB586564A - Improvements in high speed axial flow elastic fluid turbines, compressors, superchargers and like apparatus - Google Patents

Improvements in high speed axial flow elastic fluid turbines, compressors, superchargers and like apparatus

Info

Publication number
GB586564A
GB586564A GB1847/42A GB184742A GB586564A GB 586564 A GB586564 A GB 586564A GB 1847/42 A GB1847/42 A GB 1847/42A GB 184742 A GB184742 A GB 184742A GB 586564 A GB586564 A GB 586564A
Authority
GB
United Kingdom
Prior art keywords
compressors
superchargers
high speed
axial flow
elastic fluid
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
GB1847/42A
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 GB1847/42A priority Critical patent/GB586564A/en
Publication of GB586564A publication Critical patent/GB586564A/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
    • 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
    • F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
    • 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
    • F01D1/00—Non-positive-displacement machines or engines, e.g. steam turbines
    • F01D1/24—Non-positive-displacement machines or engines, e.g. steam turbines characterised by counter-rotating rotors subjected to same working fluid stream without intermediate stator blades or the like
    • F01D1/26—Non-positive-displacement machines or engines, e.g. steam turbines characterised by counter-rotating rotors subjected to same working fluid stream without intermediate stator blades or the like traversed by the working-fluid substantially axially
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/06—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages
    • F02C3/067—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages having counter-rotating rotors
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Abstract

586,564. Gas turbines ; air compressors. HALL, J. S., JENSON, G., and METROPOLITAN-VICEERS ELECTRICAL CO., Ltd. Feb. 11, 1942, No. 1847. [Class 110 (iii)] The outer rotor of a contra-rotational gas turbine or air compressor is built up of blades 3, 5, 7, Fig. 1,.carried by outer foundation rings 3a, 5a, 7a having axially disposed flanges 9 by which they are secured to distance pieces 11. The inner rotor may be similarly constructed or be, as shown, in accordance with Specification 586,562. In a modification, only one row of rivets 14, Fig. 2, is used for each blade ring, the distance piece 13 being enlarged at 13b to enclose the foundation ring. Specifications 586,552, 586,553, 586,561 and 586,563 also are referred to.
GB1847/42A 1942-02-11 1942-02-11 Improvements in high speed axial flow elastic fluid turbines, compressors, superchargers and like apparatus Expired GB586564A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1847/42A GB586564A (en) 1942-02-11 1942-02-11 Improvements in high speed axial flow elastic fluid turbines, compressors, superchargers and like apparatus

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1847/42A GB586564A (en) 1942-02-11 1942-02-11 Improvements in high speed axial flow elastic fluid turbines, compressors, superchargers and like apparatus

Publications (1)

Publication Number Publication Date
GB586564A true GB586564A (en) 1947-03-24

Family

ID=9729045

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1847/42A Expired GB586564A (en) 1942-02-11 1942-02-11 Improvements in high speed axial flow elastic fluid turbines, compressors, superchargers and like apparatus

Country Status (1)

Country Link
GB (1) GB586564A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2959394A (en) * 1953-12-11 1960-11-08 Havilland Engine Co Ltd Stators of multi-stage axial flow compressors or turbines
US3024968A (en) * 1955-10-21 1962-03-13 Rolls Royce Stator construction for multi-stage axial-flow compressor
US3032260A (en) * 1955-07-12 1962-05-01 Latham Manufactruing Co Rotary apparatus and method of making the same
DE102018109357A1 (en) * 2018-04-19 2019-10-24 Arianegroup Gmbh Multifan segment powerplant

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2959394A (en) * 1953-12-11 1960-11-08 Havilland Engine Co Ltd Stators of multi-stage axial flow compressors or turbines
US3032260A (en) * 1955-07-12 1962-05-01 Latham Manufactruing Co Rotary apparatus and method of making the same
US3024968A (en) * 1955-10-21 1962-03-13 Rolls Royce Stator construction for multi-stage axial-flow compressor
DE102018109357A1 (en) * 2018-04-19 2019-10-24 Arianegroup Gmbh Multifan segment powerplant
DE102018109357B4 (en) 2018-04-19 2023-12-21 Arianegroup Gmbh Method for operating an aircraft with at least one engine comprising a turbomachine

Similar Documents

Publication Publication Date Title
GB589541A (en) Improvements in axial flow turbines, compressors and the like
GB599391A (en) Improvements in and relating to axial flow compressors, turbines and the like machines
GB705387A (en) Improvements relating to radial-flow turbine or centrifugal compressors
GB689270A (en) Improvements in axial flow turbines or compressors
GB586562A (en) Improvements in high speed axial flow elastic fluid turbines, compressors, superchargers and like apparatus
GB586560A (en) Improvements in axial flow compressors and like machines
GB586564A (en) Improvements in high speed axial flow elastic fluid turbines, compressors, superchargers and like apparatus
GB622767A (en) Improvements in or relating to the blades of axial flow compressors and turbines andthe means for fixing them
GB586838A (en) Elastic fluid turbines
GB844020A (en) Stator vane assemblies for axial-flow compressors and turbines
GB561692A (en) Improvements in or relating to thermal power plants
GB586551A (en) Improvements in or relating to internal combustion power turbine plant for propulsion in air
GB780240A (en) Improvements in or relating to the construction of axial flow turbines or compressors
GB652591A (en) Improved blade ring for radial flow elastic fluid turbines or compressors
GB628697A (en) Improvements in and relating to a gas turbine plant
GB586563A (en) Improvements in high speed axial flow elastic fluid turbines, compressors, superchargers and like apparatus
GB586561A (en) Improvements in high speed axial flow elastic fluid turbines, compressors, superchargers and like apparatus
GB585345A (en) Internal-combustion turbine plant
GB908748A (en) Improvements relating to blading of axial flow turbines
GB624777A (en) Improvements in or relating to stator casings for compressors and like machines
GB592615A (en) Improvements in or relating to internal combustion turbine power plants
GB680040A (en) Improvements in or relating to blade supporting rings for preliminary rotor blades of blowers and compressors
GB622415A (en) Improvements in and relating to multi-stage compressors, pumps, turbines, or similar rotary machines or engines
GB586553A (en) Improvements in or relating to turbines
GB600057A (en) Improvements in or relating to the mounting of blades in axial flow compressors, turbines, or the like