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GB586552A - Improvements in or relating to internal combustion turbine plant - Google Patents

Improvements in or relating to internal combustion turbine plant

Info

Publication number
GB586552A
GB586552A GB14095/41A GB1409541A GB586552A GB 586552 A GB586552 A GB 586552A GB 14095/41 A GB14095/41 A GB 14095/41A GB 1409541 A GB1409541 A GB 1409541A GB 586552 A GB586552 A GB 586552A
Authority
GB
United Kingdom
Prior art keywords
blading
air
foundation ring
turbine
relating
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
GB14095/41A
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 GB14095/41A priority Critical patent/GB586552A/en
Priority to ES175221A priority patent/ES175221A1/en
Publication of GB586552A publication Critical patent/GB586552A/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
    • 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
    • F01D5/022—Blade-carrying members, e.g. rotors with concentric rows of axial blades
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

586,552. Gas turbines. BAUMANN, K., and METROPOLITAN-VICKERS ELECTRICAL CO., Ltd. Nov. 1, 1941, No. 14095. Drawings to Specification. [Class 110 (iii)] In a thrust-augmentor such as described in Specification 560,551, [Group XXVIII], one or each of the air blading stages is mounted on a foundation ring at the base of the blading which is carried by the turbine through the medium of an axially extending member. The member may be of re-entrant or swan-neck form and may be rigidly attached, as by riveting or welding, to the turbine part and foundation ring, or be articulated to them, or secured to them by radial tapered pins. One stage of the air blading may be combined with a turbine stage as a multiple tier structure. The foundation ring of the air blading may be made of a light alloy and be mounted within a protecting structure arranged to secure circulation of cooling air. Cylindrical extensions of the supporting members may provide heat shields. Specifications 583,111 and 586,559 also are referred to.
GB14095/41A 1941-11-01 1941-11-01 Improvements in or relating to internal combustion turbine plant Expired GB586552A (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
GB14095/41A GB586552A (en) 1941-11-01 1941-11-01 Improvements in or relating to internal combustion turbine plant
ES175221A ES175221A1 (en) 1941-11-01 1946-10-08 A PUSH INCREMENTER FOR AN INTERNAL COMBUSTION TURBINE INSTALLATION

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB14095/41A GB586552A (en) 1941-11-01 1941-11-01 Improvements in or relating to internal combustion turbine plant

Publications (1)

Publication Number Publication Date
GB586552A true GB586552A (en) 1947-03-24

Family

ID=10034888

Family Applications (1)

Application Number Title Priority Date Filing Date
GB14095/41A Expired GB586552A (en) 1941-11-01 1941-11-01 Improvements in or relating to internal combustion turbine plant

Country Status (2)

Country Link
ES (1) ES175221A1 (en)
GB (1) GB586552A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3110153A (en) * 1950-09-05 1963-11-12 Aerojet General Co Gas generator turbojet motor
FR2601069A1 (en) * 1986-07-02 1988-01-08 Rolls Royce Plc TURBINE.
EP0900920A3 (en) * 1997-09-08 2000-03-22 General Electric Company Sealing device between a blade platform and two stator shrouds
US6454535B1 (en) 2000-10-31 2002-09-24 General Electric Company Blisk
WO2021074508A1 (en) * 2019-10-17 2021-04-22 Safran Aircraft Engines Improved ferrule for counter-rotating turbine impeller

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3110153A (en) * 1950-09-05 1963-11-12 Aerojet General Co Gas generator turbojet motor
FR2601069A1 (en) * 1986-07-02 1988-01-08 Rolls Royce Plc TURBINE.
EP0900920A3 (en) * 1997-09-08 2000-03-22 General Electric Company Sealing device between a blade platform and two stator shrouds
US6454535B1 (en) 2000-10-31 2002-09-24 General Electric Company Blisk
WO2021074508A1 (en) * 2019-10-17 2021-04-22 Safran Aircraft Engines Improved ferrule for counter-rotating turbine impeller
FR3102215A1 (en) * 2019-10-17 2021-04-23 Safran Aircraft Engines improved counter-rotating turbine impeller ferrule
CN114555926A (en) * 2019-10-17 2022-05-27 赛峰飞机发动机公司 Improved shroud for counter-rotating turbine wheel
US20240093638A1 (en) * 2019-10-17 2024-03-21 Safran Aircraft Engines Improved ferrule for counter-rotating turbine impeller
US12085014B2 (en) 2019-10-17 2024-09-10 Safran Aircraft Engines Ferrule for counter-rotating turbine impeller

Also Published As

Publication number Publication date
ES175221A1 (en) 1946-11-16

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