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GB594206A - Improvements in internal combustion turbine plant for propulsion - Google Patents

Improvements in internal combustion turbine plant for propulsion

Info

Publication number
GB594206A
GB594206A GB1655545A GB1655545A GB594206A GB 594206 A GB594206 A GB 594206A GB 1655545 A GB1655545 A GB 1655545A GB 1655545 A GB1655545 A GB 1655545A GB 594206 A GB594206 A GB 594206A
Authority
GB
United Kingdom
Prior art keywords
turbine
compressor
propulsion
turbine plant
internal combustion
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
GB1655545A
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
Filing date
Publication date
Application filed by Metropolitan Vickers Electrical Co Ltd filed Critical Metropolitan Vickers Electrical Co Ltd
Publication of GB594206A publication Critical patent/GB594206A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/06Gas-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
    • F02C3/067Gas-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

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)

Abstract

594,206. Gas turbines. SMITH, D. M., and METROPOLITAN - VICKERS ELECTRICAL CO., Ltd. June 28, 1945, No. 16555. [Class 110 (iii)] [Also in Group XXXIII] In a gas turbine plant comprising an axial flow compressor 1, an annular combustion chamber or annularly arranged group of chambers 2, a turbine 4a driving the compressor and a two-stage turbine 8a, 9a in axial alignment, and in which each stage of the turbine 8a, 9a is directly coupled to an element of a contrarotational tractor air-screw 12, 13, the two shafts 10, 11 connecting the turbine stages 8a, 9a to the air-screw elements 12, 13 pass through the compressor 1 anc combustion chamber 2 and thus pass through the shaft 5 coupling the compressor to the compressor turbine.
GB1655545A 1945-06-28 Improvements in internal combustion turbine plant for propulsion Expired GB594206A (en)

Publications (1)

Publication Number Publication Date
GB594206A true GB594206A (en) 1947-11-05

Family

ID=1732385

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1655545A Expired GB594206A (en) 1945-06-28 Improvements in internal combustion turbine plant for propulsion

Country Status (1)

Country Link
GB (1) GB594206A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4976102A (en) * 1988-05-09 1990-12-11 General Electric Company Unducted, counterrotating gearless front fan engine
GB2431435A (en) * 2005-10-19 2007-04-25 Gen Electric A turbine engine assembly comprising a contra-rotating fan assembly discharging air directly into the high pressure compressor
US10815881B2 (en) 2017-09-20 2020-10-27 General Electric Company Counter rotating turbine with reversing speed reduction assembly
US11428160B2 (en) 2020-12-31 2022-08-30 General Electric Company Gas turbine engine with interdigitated turbine and gear assembly

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4976102A (en) * 1988-05-09 1990-12-11 General Electric Company Unducted, counterrotating gearless front fan engine
GB2431435A (en) * 2005-10-19 2007-04-25 Gen Electric A turbine engine assembly comprising a contra-rotating fan assembly discharging air directly into the high pressure compressor
US7685808B2 (en) 2005-10-19 2010-03-30 General Electric Company Gas turbine engine assembly and methods of assembling same
GB2431435B (en) * 2005-10-19 2010-09-22 Gen Electric Gas turbine engine assembly
US10815881B2 (en) 2017-09-20 2020-10-27 General Electric Company Counter rotating turbine with reversing speed reduction assembly
US11428160B2 (en) 2020-12-31 2022-08-30 General Electric Company Gas turbine engine with interdigitated turbine and gear assembly

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