GB586553A - Improvements in or relating to turbines - Google Patents

Improvements in or relating to turbines

Info

Publication number
GB586553A
GB586553A GB1433641A GB1433641A GB586553A GB 586553 A GB586553 A GB 586553A GB 1433641 A GB1433641 A GB 1433641A GB 1433641 A GB1433641 A GB 1433641A GB 586553 A GB586553 A GB 586553A
Authority
GB
United Kingdom
Prior art keywords
turbine
compressor
air
blades
ring
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
GB1433641A
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 GB1433641A priority Critical patent/GB586553A/en
Publication of GB586553A publication Critical patent/GB586553A/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • F02C3/073—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 the compressor and turbine stages being concentric

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

586,553. Gas turbines. BAUMANN, K., and METROPOLITAN-VICKERS ELECTRICAL CO., Ltd. Nov. 6, 1941, No. 14336. [Class 110 (iii)] The contra-rotational elements, 9, 10, Fig. 3, of an air-compressor .are driven by contrarotational turbine elements I, II radially outside the compressor. The number of turbine blade rings is less than the number of compressor blade rings. The compressor carries the turbine discs by means of cylindrical parts 13, 14. The air is delivered to a swan-neck combustion chamber and the turbine exhaust passes to an annular discharge 37 which, merges into a propulsion jet. Air is received by a forwardly directed entrance 39 and reaches the air-compressor by way of a number of pipes 40 of stream-line section which cross the discharge 37. Another ring of blades may be carried at the end of a cylindrical extension of the shrouding of the blade ring I and a further ring may be carried by a cylindrical extension of the foundation ring of the blades II. Two compressors may be arranged in series, each being driven by pairs of turbine blades, as shown in Fig. 3, in series. Three compressors may be arranged in series, adjacent compressor rotors being driven by contra-rotational turbine pairs with single turbine blade rings on the end compressor rotors co-operating with fixed guide rings. The turbine elements I. II, Fig. 3, may carry externally directed air blades. Specifications 586,551, 586,552 and 586,560 are referred to.
GB1433641A 1941-11-06 1941-11-06 Improvements in or relating to turbines Expired GB586553A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1433641A GB586553A (en) 1941-11-06 1941-11-06 Improvements in or relating to turbines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1433641A GB586553A (en) 1941-11-06 1941-11-06 Improvements in or relating to turbines

Publications (1)

Publication Number Publication Date
GB586553A true GB586553A (en) 1947-03-24

Family

ID=10039347

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1433641A Expired GB586553A (en) 1941-11-06 1941-11-06 Improvements in or relating to turbines

Country Status (1)

Country Link
GB (1) GB586553A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2711304A (en) * 1948-01-30 1955-06-21 English Electric Co Ltd Plural stage gas turbine
DE1028280B (en) * 1952-04-30 1958-04-17 Sc Techn H C Alfred Buechi Dr Counter-rotating turbo blower or pump driven by counter-rotating gas turbine
US7571607B2 (en) 2006-03-06 2009-08-11 Honeywell International Inc. Two-shaft turbocharger

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2711304A (en) * 1948-01-30 1955-06-21 English Electric Co Ltd Plural stage gas turbine
DE1028280B (en) * 1952-04-30 1958-04-17 Sc Techn H C Alfred Buechi Dr Counter-rotating turbo blower or pump driven by counter-rotating gas turbine
US7571607B2 (en) 2006-03-06 2009-08-11 Honeywell International Inc. Two-shaft turbocharger

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