GB585343A - Combustion chambers of internal-combustion turbine plant - Google Patents

Combustion chambers of internal-combustion turbine plant

Info

Publication number
GB585343A
GB585343A GB13631/42A GB1363142A GB585343A GB 585343 A GB585343 A GB 585343A GB 13631/42 A GB13631/42 A GB 13631/42A GB 1363142 A GB1363142 A GB 1363142A GB 585343 A GB585343 A GB 585343A
Authority
GB
United Kingdom
Prior art keywords
chamber
secondary air
tubes
combustion
passes
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
GB13631/42A
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.)
Armstrong Siddeley Motors Ltd
Original Assignee
Armstrong Siddeley Motors 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 Armstrong Siddeley Motors Ltd filed Critical Armstrong Siddeley Motors Ltd
Priority to GB13631/42A priority Critical patent/GB585343A/en
Publication of GB585343A publication Critical patent/GB585343A/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04—Air inlet arrangements
    • 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)
  • Fuel Cell (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)

Abstract

585,343. Gas turbines. ARMSTRONG SIDDELEY MOTORS, Ltd., and HEPPNER, F. A. M. Sept. 29, 1942, Nos. 13631/42, 15665/42 and 822/43. [Class 110 (iii)] In a contra-rotational gas turbine plant, primary air from the compressor 11 is diverted by centrifugally acting blade portions 19, and passes through an annular space 22, past swirlproducing blades 24 into a combustion chamber 16. The fuel is thrown in a radial sheet, transverse to the current of primary air, from a valve 23 which is opened by the pressure of the fuel supply. Ignition is started by a heater 30 which withdraws into a covering tube when the airpressure on piston 31 overcomes a spring 33. Secondary air passes from the compressor into a chamber 12 and surrounds the tubes 14 which lead from the combustion chamber to the turbine 17. The secondary air enters through perforations 15 and mixes with the combustion products. In the construction shown in Fig., 6, the primary air passes through the space 59 and blades 62 and the secondary air passes through the chamber 65 and holes 64 in tubes 14. In a third form the chamber 65 is continued by a sheet metal extension and the tubes 58 are replaced by an annular passage between annular walls which are corrugated where they reach the sheet metal extension and thereby provide passages for the secondary air to enter the main gas flow. Specifications 561,246, [Group XXXIV], 585,340, 585,342 and 585,346 are referred to.
GB13631/42A 1942-09-29 1942-09-29 Combustion chambers of internal-combustion turbine plant Expired GB585343A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB13631/42A GB585343A (en) 1942-09-29 1942-09-29 Combustion chambers of internal-combustion turbine plant

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB13631/42A GB585343A (en) 1942-09-29 1942-09-29 Combustion chambers of internal-combustion turbine plant

Publications (1)

Publication Number Publication Date
GB585343A true GB585343A (en) 1947-02-05

Family

ID=10026533

Family Applications (1)

Application Number Title Priority Date Filing Date
GB13631/42A Expired GB585343A (en) 1942-09-29 1942-09-29 Combustion chambers of internal-combustion turbine plant

Country Status (1)

Country Link
GB (1) GB585343A (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2604510A (en) * 1949-11-30 1952-07-22 Gen Electric Automatically retractable spark plug for gas turbines
DE944690C (en) * 1948-11-30 1956-06-21 Joseph Szydlowski Combustion chamber arrangement
US2856755A (en) * 1953-10-19 1958-10-21 Szydlowski Joseph Combustion chamber with diverse combustion and diluent air paths
US3011311A (en) * 1955-10-24 1961-12-05 Williams Res Corp Gas turbine
US3077076A (en) * 1960-01-20 1963-02-12 Williams Res Corp Gas turbine combustion chamber
US3086396A (en) * 1960-09-22 1963-04-23 Homer T Armstrong High-temperature probe assembly
US3118278A (en) * 1959-06-26 1964-01-21 Gas turbine power plant
US3169369A (en) * 1963-06-19 1965-02-16 Gen Electric Combustion system

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE944690C (en) * 1948-11-30 1956-06-21 Joseph Szydlowski Combustion chamber arrangement
US2604510A (en) * 1949-11-30 1952-07-22 Gen Electric Automatically retractable spark plug for gas turbines
US2856755A (en) * 1953-10-19 1958-10-21 Szydlowski Joseph Combustion chamber with diverse combustion and diluent air paths
US3011311A (en) * 1955-10-24 1961-12-05 Williams Res Corp Gas turbine
US3118278A (en) * 1959-06-26 1964-01-21 Gas turbine power plant
US3077076A (en) * 1960-01-20 1963-02-12 Williams Res Corp Gas turbine combustion chamber
US3086396A (en) * 1960-09-22 1963-04-23 Homer T Armstrong High-temperature probe assembly
US3169369A (en) * 1963-06-19 1965-02-16 Gen Electric Combustion system

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