GB290014A - Internal combustion turbine - Google Patents

Internal combustion turbine

Info

Publication number
GB290014A
GB290014A GB852927A GB852927A GB290014A GB 290014 A GB290014 A GB 290014A GB 852927 A GB852927 A GB 852927A GB 852927 A GB852927 A GB 852927A GB 290014 A GB290014 A GB 290014A
Authority
GB
United Kingdom
Prior art keywords
compressor
chambers
valves
delivers
combustion 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
GB852927A
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 GB852927A priority Critical patent/GB290014A/en
Publication of GB290014A publication Critical patent/GB290014A/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
    • F02C5/02—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion characterised by the arrangement of the combustion chamber in the chamber in the plant

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

290,014. Monnier, E. March 28, 1927. Jet-wheels; cooling parts; working-fluid supply. -In an internal-combustion turbine wherein stator combustion chambers 5<a> - - 5<d> co-operate with peripheral rotor buckets 14, a centrifugal compressor 1 delivers air past non-return valves into the double casing 2, where it circulates around the explosion chambers and the exhaust passage, passing then through a carburettor into a supercompressor 4 which delivers the charge through valves 12<a> - - 12<d> into the combustion chambers. Two power rotors may be provided, arranged one on either side of the super-compressor 4. Cooling-air is drawn by the compressor 1 through the interior of the power rotors which have helical spokes 28. The inlet valves 12<a> - - 12<d> are rotatably actuated by cam grooves 20<a> in the rotor. Separate groups of explosion chambers may be fed by separate supercompressors.
GB852927A 1927-03-28 1927-03-28 Internal combustion turbine Expired GB290014A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB852927A GB290014A (en) 1927-03-28 1927-03-28 Internal combustion turbine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB852927A GB290014A (en) 1927-03-28 1927-03-28 Internal combustion turbine

Publications (1)

Publication Number Publication Date
GB290014A true GB290014A (en) 1928-05-10

Family

ID=9854171

Family Applications (1)

Application Number Title Priority Date Filing Date
GB852927A Expired GB290014A (en) 1927-03-28 1927-03-28 Internal combustion turbine

Country Status (1)

Country Link
GB (1) GB290014A (en)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2426098A (en) * 1942-09-03 1947-08-19 Armstrong Siddeley Motors Ltd Compound internal-combustion turbine plant
US2487514A (en) * 1943-01-16 1949-11-08 Jarvis C Marble Turbine rotor cooling
US2508685A (en) * 1944-09-12 1950-05-23 Adolphe C Peterson Combustion gas turbine
US2578481A (en) * 1946-03-25 1951-12-11 Rolls Royce Gas turbine power plant with auxiliary compressor supplying cooling air for the turbine
US2801519A (en) * 1951-02-17 1957-08-06 Garrett Corp Gas turbine motor scroll structure
US2898736A (en) * 1957-05-06 1959-08-11 Robert F Ely Plural combustion products generators in ring coaxial with a turbine
US3078671A (en) * 1959-08-03 1963-02-26 Houten Inc Van Gas turbine power plant
US3089307A (en) * 1960-06-17 1963-05-14 Melvin M Kollander Rotary jet engine
FR2871850A1 (en) * 2004-06-18 2005-12-23 Claude Louis Adam Toric engine cooling system for terrestrial vehicle, has conduits with openings to allow air flow into openings of two semi hollow toroids, and suction of gas produced by engine through openings of toroids by movement of sectioned toroids
WO2006008353A1 (en) * 2004-06-18 2006-01-26 Claude-Louis Adam Revolving toroidal motor

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2426098A (en) * 1942-09-03 1947-08-19 Armstrong Siddeley Motors Ltd Compound internal-combustion turbine plant
US2487514A (en) * 1943-01-16 1949-11-08 Jarvis C Marble Turbine rotor cooling
US2508685A (en) * 1944-09-12 1950-05-23 Adolphe C Peterson Combustion gas turbine
US2578481A (en) * 1946-03-25 1951-12-11 Rolls Royce Gas turbine power plant with auxiliary compressor supplying cooling air for the turbine
US2801519A (en) * 1951-02-17 1957-08-06 Garrett Corp Gas turbine motor scroll structure
US2898736A (en) * 1957-05-06 1959-08-11 Robert F Ely Plural combustion products generators in ring coaxial with a turbine
US3078671A (en) * 1959-08-03 1963-02-26 Houten Inc Van Gas turbine power plant
US3089307A (en) * 1960-06-17 1963-05-14 Melvin M Kollander Rotary jet engine
FR2871850A1 (en) * 2004-06-18 2005-12-23 Claude Louis Adam Toric engine cooling system for terrestrial vehicle, has conduits with openings to allow air flow into openings of two semi hollow toroids, and suction of gas produced by engine through openings of toroids by movement of sectioned toroids
WO2006008353A1 (en) * 2004-06-18 2006-01-26 Claude-Louis Adam Revolving toroidal motor

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