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GB619173A - Improvements in rotary internal combustion engines - Google Patents

Improvements in rotary internal combustion engines

Info

Publication number
GB619173A
GB619173A GB3484546A GB3484546A GB619173A GB 619173 A GB619173 A GB 619173A GB 3484546 A GB3484546 A GB 3484546A GB 3484546 A GB3484546 A GB 3484546A GB 619173 A GB619173 A GB 619173A
Authority
GB
United Kingdom
Prior art keywords
ducts
combustion
compressor
admitted
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
GB3484546A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to GB3484546A priority Critical patent/GB619173A/en
Publication of GB619173A publication Critical patent/GB619173A/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
    • F02C5/00—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion
    • F02C5/12—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion the combustion chambers having inlet or outlet valves, e.g. Holzwarth gas-turbine plants

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Ignition Installations For Internal Combustion Engines (AREA)

Abstract

619,173. Gas turbine plant. MIDDLETON, V. H. Nov. 25, 1946, Nos. 34845/46 and 18573/47. [Class 110 (iii)] A compressor 12 delivers air to combustion chambers 6 through ducts 13 and the products of combustion are discharged through ducts 9. The ducts 9 and 13 are opened at timed intervals determined by rotary disc valves 7, 10. Fuel is admitted intermittently by means of an injector 15 and ignition is by sparking-plugs 17. The disc valves are carried by a sleeve shaft 4 driven through gearing 14. The combustion products pass into a chamber 20 and issue therefrom through nozzles 21. The turbines are of usual axial flow type, the turbine wheel 23 driving the compressor and shaft 4 and the turbine 24 providing useful power. Secondary air is admitted to the combustion chambers 6 through holes 19.
GB3484546A 1946-11-25 1946-11-25 Improvements in rotary internal combustion engines Expired GB619173A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB3484546A GB619173A (en) 1946-11-25 1946-11-25 Improvements in rotary internal combustion engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3484546A GB619173A (en) 1946-11-25 1946-11-25 Improvements in rotary internal combustion engines

Publications (1)

Publication Number Publication Date
GB619173A true GB619173A (en) 1949-03-04

Family

ID=10370610

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3484546A Expired GB619173A (en) 1946-11-25 1946-11-25 Improvements in rotary internal combustion engines

Country Status (1)

Country Link
GB (1) GB619173A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE945003C (en) * 1953-01-15 1956-06-28 Habil Fritz A F Schmidt Dr Ing Mechanically controlled multi-stage combustion chambers for aircraft jet engines, pulso engines or gas turbines
US2928242A (en) * 1954-12-16 1960-03-15 Phillips Petroleum Co Multi-combustion chamber gas turbine with rotary valving

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE945003C (en) * 1953-01-15 1956-06-28 Habil Fritz A F Schmidt Dr Ing Mechanically controlled multi-stage combustion chambers for aircraft jet engines, pulso engines or gas turbines
US2928242A (en) * 1954-12-16 1960-03-15 Phillips Petroleum Co Multi-combustion chamber gas turbine with rotary valving

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