GB467630A - Improvements in or relating to internal combustion turbines - Google Patents

Improvements in or relating to internal combustion turbines

Info

Publication number
GB467630A
GB467630A GB2811036A GB2811036A GB467630A GB 467630 A GB467630 A GB 467630A GB 2811036 A GB2811036 A GB 2811036A GB 2811036 A GB2811036 A GB 2811036A GB 467630 A GB467630 A GB 467630A
Authority
GB
United Kingdom
Prior art keywords
valve
ports
chambers
blades
rotor
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
GB2811036A
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.)
GEORGES METTETAL
Original Assignee
GEORGES METTETAL
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 GEORGES METTETAL filed Critical GEORGES METTETAL
Priority to GB2811036A priority Critical patent/GB467630A/en
Publication of GB467630A publication Critical patent/GB467630A/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)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

467,630. Internal-combustion turbines. METTETAL, G. Oct. 16, 1936, No. 28110. [Class 110 (iii)] An internal-combustion turbine comprises a rotor 2 provided with a circular row of blades 3, a number of circularly arranged combustion chambers 4<a>, 4<b>, and a sleeve valve 5 between the blades and the chambers 4<a>, 4<b>. The fuel is supplied to the chambers 4<a>, 4<b> by a compressor 9 free on the rotor shaft 1 and provided with blades 10 which draw in air through ports 11 and fuel through jets 14, and force the mixture through ports 6 in the valve 5 when the ports o register with the ports 20 of the chambers. The combustion gases are delivered through ports 21 in the chambers when they register with the ports 7 on the valve 5, and after acting on the rotor blades 3, strike the oppositely arranged blades 8 on the valve and drive the valve in the opposite direction to the rotor. The compressor 9 is driven by the shaft 1 through gear train 16, 15, 12, and the shaft 1 is additionally driven by the valve through a toothed ring 18 on the valve driving the wheel 16 through a wheel 17.
GB2811036A 1936-10-16 1936-10-16 Improvements in or relating to internal combustion turbines Expired GB467630A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2811036A GB467630A (en) 1936-10-16 1936-10-16 Improvements in or relating to internal combustion turbines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2811036A GB467630A (en) 1936-10-16 1936-10-16 Improvements in or relating to internal combustion turbines

Publications (1)

Publication Number Publication Date
GB467630A true GB467630A (en) 1937-06-21

Family

ID=10270423

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2811036A Expired GB467630A (en) 1936-10-16 1936-10-16 Improvements in or relating to internal combustion turbines

Country Status (1)

Country Link
GB (1) GB467630A (en)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2460523A (en) * 1945-12-20 1949-02-01 Svenska Turbinfab Ab Combined gas turbocompressor and gas turbine
US2485813A (en) * 1945-04-30 1949-10-25 Bert G Carison Compressor-turbine engine
US2538179A (en) * 1945-09-04 1951-01-16 Grace K Weinhardt Rotary power generator
US2583872A (en) * 1947-08-02 1952-01-29 United Aircraft Corp Gas turbine power plant, including planetary gearing between a compressor, turbine, and power consumer
US2589239A (en) * 1945-05-16 1952-03-18 Malcolm Mitchell Turbine-compressor unit
US2594765A (en) * 1945-10-06 1952-04-29 Esther C Goddard Resonance combustion apparatus
US2630677A (en) * 1947-01-20 1953-03-10 Donald W Seifert Axial flow jet motor with reversely rotating continuous combustion type combustion products generator and turbine
DE1029618B (en) * 1952-05-06 1958-05-08 Sc Techn H C Eth Alfred Buechi Turbine jet engine
US2928239A (en) * 1954-03-16 1960-03-15 Arthur W Goldstein Impelled charge gas explosion turbine with constant volume, pressure raising combustion chambers
EP0185846A2 (en) * 1984-08-20 1986-07-02 Gerhard Kielhorn Gas-turbine with intermittent combustion

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2485813A (en) * 1945-04-30 1949-10-25 Bert G Carison Compressor-turbine engine
US2589239A (en) * 1945-05-16 1952-03-18 Malcolm Mitchell Turbine-compressor unit
US2538179A (en) * 1945-09-04 1951-01-16 Grace K Weinhardt Rotary power generator
US2594765A (en) * 1945-10-06 1952-04-29 Esther C Goddard Resonance combustion apparatus
US2460523A (en) * 1945-12-20 1949-02-01 Svenska Turbinfab Ab Combined gas turbocompressor and gas turbine
US2630677A (en) * 1947-01-20 1953-03-10 Donald W Seifert Axial flow jet motor with reversely rotating continuous combustion type combustion products generator and turbine
US2583872A (en) * 1947-08-02 1952-01-29 United Aircraft Corp Gas turbine power plant, including planetary gearing between a compressor, turbine, and power consumer
DE1029618B (en) * 1952-05-06 1958-05-08 Sc Techn H C Eth Alfred Buechi Turbine jet engine
US2928239A (en) * 1954-03-16 1960-03-15 Arthur W Goldstein Impelled charge gas explosion turbine with constant volume, pressure raising combustion chambers
EP0185846A2 (en) * 1984-08-20 1986-07-02 Gerhard Kielhorn Gas-turbine with intermittent combustion
EP0185846A3 (en) * 1984-08-20 1987-05-27 Gerhard Kielhorn Gas-turbine with intermittent combustion
US4702072A (en) * 1984-08-20 1987-10-27 Gerhard Kielhorn Internal combustion engine

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