GB171685A - An internal combustion turbine - Google Patents

An internal combustion turbine

Info

Publication number
GB171685A
GB171685A GB29894/21A GB2989421A GB171685A GB 171685 A GB171685 A GB 171685A GB 29894/21 A GB29894/21 A GB 29894/21A GB 2989421 A GB2989421 A GB 2989421A GB 171685 A GB171685 A GB 171685A
Authority
GB
United Kingdom
Prior art keywords
turbine wheel
chamber
internal combustion
ring
turbine
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
GB29894/21A
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
Publication of GB171685A publication Critical patent/GB171685A/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
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Portable Nailing Machines And Staplers (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

171,685. Schultz, E. J. A. Nov. 19, 1920, [Convention date]. Working-fluid supply.-In an internal combustion turbine, the explosion chambers d are arranged in a stationary member between the turbine wheel e and a ring b rotating therewith. A fan a. geared to rotate at twice the speed of the turbine wheel delivers the explosive mixture to the chamber d through opposite parts in the ring b, which is given a varying thickness as shown to provide expanding delivery passages 5, 15. Sparking-plugs m, n carried by the turbine wheel register with successive orifices in the stationarv chamber d. The walls of the turbine wheel and the combustion chamber may be fitted with ribs for cooling.
GB29894/21A 1920-11-19 1921-11-09 An internal combustion turbine Expired GB171685A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR171685X 1920-11-19

Publications (1)

Publication Number Publication Date
GB171685A true GB171685A (en) 1922-06-22

Family

ID=8877400

Family Applications (1)

Application Number Title Priority Date Filing Date
GB29894/21A Expired GB171685A (en) 1920-11-19 1921-11-09 An internal combustion turbine

Country Status (1)

Country Link
GB (1) GB171685A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2448972A (en) * 1944-10-20 1948-09-07 Edward W Gizara Internal-combusstion engine
US2595505A (en) * 1946-04-20 1952-05-06 Continental Aviat & Engineerin Coaxial combustion products generator, turbine, and compressor
US2616253A (en) * 1945-02-23 1952-11-04 Terce Paul Joseph Jean Constant torque gas turbine with counterrotating elements and speed controlled fuel and air supply

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2448972A (en) * 1944-10-20 1948-09-07 Edward W Gizara Internal-combusstion engine
US2616253A (en) * 1945-02-23 1952-11-04 Terce Paul Joseph Jean Constant torque gas turbine with counterrotating elements and speed controlled fuel and air supply
US2595505A (en) * 1946-04-20 1952-05-06 Continental Aviat & Engineerin Coaxial combustion products generator, turbine, and compressor

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