GB142959A - Internal combustion turbine - Google Patents

Internal combustion turbine

Info

Publication number
GB142959A
GB142959A GB519319A GB519319A GB142959A GB 142959 A GB142959 A GB 142959A GB 519319 A GB519319 A GB 519319A GB 519319 A GB519319 A GB 519319A GB 142959 A GB142959 A GB 142959A
Authority
GB
United Kingdom
Prior art keywords
turbine
shaft
combustion
compressors
eccentric
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
GB519319A
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 GB519319A priority Critical patent/GB142959A/en
Publication of GB142959A publication Critical patent/GB142959A/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)
  • Supercharger (AREA)

Abstract

142,959. Nicholls, R. E. March 3, 1919. Working - fluid supply; arrangement of bearings.-In an internal - combustion turbine, the charge is compressed by three compressors J past valves K<2> and pipes L into three valved combustion chambers A. The discharge valve a<3> of each combustion chamber is periodically opened by an eccentric 11<4> on the turbine shaft 11<7> to deliver the ignited charge to the nozzles F and the turbine F<2>. A spring-loaded sleeve valve a<4> effects a rapid release of the gases on starting. The compressor pistons K are reciprocated by a rotary cam I on the shaft H<8>, which may be connected directly to the shaft H<7> or geared therewith so as to rotate at twice the turbine speed, giving two explosions in each combustion chamber for one revolution of the turbine. The bearing H<1> is arranged outside the casing, and a diaphragm H<6> affords a thrust bearing for the shaft H'. The space between the diaphragm H<6> and a plug H<5> provides an oil bath for the eccentric H<4> or other gear working the valves. 'The number of combustion chambers and compressors may be varied.
GB519319A 1919-03-03 1919-03-03 Internal combustion turbine Expired GB142959A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB519319A GB142959A (en) 1919-03-03 1919-03-03 Internal combustion turbine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB519319A GB142959A (en) 1919-03-03 1919-03-03 Internal combustion turbine

Publications (1)

Publication Number Publication Date
GB142959A true GB142959A (en) 1920-05-20

Family

ID=9791451

Family Applications (1)

Application Number Title Priority Date Filing Date
GB519319A Expired GB142959A (en) 1919-03-03 1919-03-03 Internal combustion turbine

Country Status (1)

Country Link
GB (1) GB142959A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2551006A (en) * 1948-05-19 1951-05-01 Waverly V Johnson Turbine type internal-combustion engine
US2687613A (en) * 1950-04-19 1954-08-31 Craigon Adam Gas turbine power plant
US2856753A (en) * 1955-04-19 1958-10-21 Herzog Richard Internal-combustion turbine engine

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2551006A (en) * 1948-05-19 1951-05-01 Waverly V Johnson Turbine type internal-combustion engine
US2687613A (en) * 1950-04-19 1954-08-31 Craigon Adam Gas turbine power plant
US2856753A (en) * 1955-04-19 1958-10-21 Herzog Richard Internal-combustion turbine engine

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