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GB586556A - Improvements in internal combustion turbine plant for propulsion - Google Patents

Improvements in internal combustion turbine plant for propulsion

Info

Publication number
GB586556A
GB586556A GB471/42A GB47142A GB586556A GB 586556 A GB586556 A GB 586556A GB 471/42 A GB471/42 A GB 471/42A GB 47142 A GB47142 A GB 47142A GB 586556 A GB586556 A GB 586556A
Authority
GB
United Kingdom
Prior art keywords
propulsion
chamber
internal combustion
turbine plant
compressor
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
GB471/42A
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 GB471/42A priority Critical patent/GB586556A/en
Priority to ES175238A priority patent/ES175238A1/en
Publication of GB586556A publication Critical patent/GB586556A/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
    • F02C3/14—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant
    • F02C3/145—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant the combustion chamber being in the reverse flow-type
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/54—Reverse-flow combustion chambers
    • 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)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

586,556. Gas turbines. BAUMANN, K., and METROPOLITAN-VICKERS ELECTRICAL CO., Ltd. Jan. 12, 1942, No. 471. [Class 110 (iii)] The combustion chamber of a gas turbine for aircraft propulsion surrounds the air-compressor. It may be a single annular chamber or an annular assembly of separate chambers. Guiding surfaces 7, 13 are provided for the double reversal of flow involved. Some of the air passes round the combustion chamber, as at 9, and some is caught by the U-shaped guide 41 and directed along the inner side of the chamber. The compressor and turbine may be of the contra-rotational type. Specifications 586,553 and 586,555 are referred to.
GB471/42A 1942-01-12 1942-01-12 Improvements in internal combustion turbine plant for propulsion Expired GB586556A (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
GB471/42A GB586556A (en) 1942-01-12 1942-01-12 Improvements in internal combustion turbine plant for propulsion
ES175238A ES175238A1 (en) 1942-01-12 1946-10-09 AN INTERNAL COMBUSTION TURBINE INSTALLATION

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB471/42A GB586556A (en) 1942-01-12 1942-01-12 Improvements in internal combustion turbine plant for propulsion

Publications (1)

Publication Number Publication Date
GB586556A true GB586556A (en) 1947-03-24

Family

ID=9704937

Family Applications (1)

Application Number Title Priority Date Filing Date
GB471/42A Expired GB586556A (en) 1942-01-12 1942-01-12 Improvements in internal combustion turbine plant for propulsion

Country Status (2)

Country Link
ES (1) ES175238A1 (en)
GB (1) GB586556A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE954465C (en) * 1954-11-05 1956-12-20 Daimler Benz Ag Combustion chamber, especially for smaller gas turbines
DE959695C (en) * 1955-06-28 1957-03-07 Bmw Studiengesellschaft Fuer T Gas turbine with rotary atomization
DE1079895B (en) * 1956-10-02 1960-04-14 Avco Mfg Corp Fuel evaporator for gas turbine combustion chambers
DE1214053B (en) * 1960-09-14 1966-04-07 Snecma Turbine jet engine
US10465907B2 (en) * 2015-09-09 2019-11-05 General Electric Company System and method having annular flow path architecture
EP3620629A1 (en) * 2018-05-23 2020-03-11 General Electric Company Gas turbine engine

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE954465C (en) * 1954-11-05 1956-12-20 Daimler Benz Ag Combustion chamber, especially for smaller gas turbines
DE959695C (en) * 1955-06-28 1957-03-07 Bmw Studiengesellschaft Fuer T Gas turbine with rotary atomization
DE1079895B (en) * 1956-10-02 1960-04-14 Avco Mfg Corp Fuel evaporator for gas turbine combustion chambers
DE1214053B (en) * 1960-09-14 1966-04-07 Snecma Turbine jet engine
US10465907B2 (en) * 2015-09-09 2019-11-05 General Electric Company System and method having annular flow path architecture
EP3620629A1 (en) * 2018-05-23 2020-03-11 General Electric Company Gas turbine engine
US11434831B2 (en) 2018-05-23 2022-09-06 General Electric Company Gas turbine combustor having a plurality of angled vanes circumferentially spaced within the combustor
US11840967B2 (en) 2018-05-23 2023-12-12 General Electric Company Gas turbine engine

Also Published As

Publication number Publication date
ES175238A1 (en) 1946-11-16

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