GB191218415A - An Internal Combustion Turbine Engine. - Google Patents

An Internal Combustion Turbine Engine.

Info

Publication number
GB191218415A
GB191218415A GB191218415DA GB191218415A GB 191218415 A GB191218415 A GB 191218415A GB 191218415D A GB191218415D A GB 191218415DA GB 191218415 A GB191218415 A GB 191218415A
Authority
GB
United Kingdom
Prior art keywords
internal combustion
turbine engine
combustion turbine
rotor
sections
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
Inventor
Arthur Pope
David Hercules Robertson
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
Application granted granted Critical
Publication of GB191218415A publication Critical patent/GB191218415A/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
    • F02C5/04—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 the combustion chambers being formed at least partly in the turbine rotor

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Filling Or Emptying Of Bunkers, Hoppers, And Tanks (AREA)

Abstract

18,415. Pope, A., and Robertson, D. H. Aug. 10. Jet-wheels; rotors; working-fluid supply.- Explosive mixture is supplied through a valve A to pockets H in the rotor and is ignited by the plug L. The rotor is divided radially into sections F which are mounted on projections O on a boss on the shaft and are pressed outwards by springs E or by pressure of the fluid which passes through channels D to the back of the sections. A water jacket surrounds the working chamber.
GB191218415D 1912-08-10 1912-08-10 An Internal Combustion Turbine Engine. Expired GB191218415A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB191218415T 1912-08-10

Publications (1)

Publication Number Publication Date
GB191218415A true GB191218415A (en) 1912-12-19

Family

ID=32642822

Family Applications (1)

Application Number Title Priority Date Filing Date
GB191218415D Expired GB191218415A (en) 1912-08-10 1912-08-10 An Internal Combustion Turbine Engine.

Country Status (1)

Country Link
GB (1) GB191218415A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2519700A1 (en) * 1981-10-21 1983-07-18 Lippis Mario Variable output turbine engine - has rotor defining triangular combustion chambers with inlet and exhaust orifices

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2519700A1 (en) * 1981-10-21 1983-07-18 Lippis Mario Variable output turbine engine - has rotor defining triangular combustion chambers with inlet and exhaust orifices

Similar Documents

Publication Publication Date Title
GB191218415A (en) An Internal Combustion Turbine Engine.
US3949711A (en) Rotary engine with graphite housing
GB271268A (en) Improvements in or relating to internal combustion turbines
GB116770A (en) Improvements in Internal Combustion Turbines.
GB191006185A (en) Improvements in and relating to Internal-combustion Turbines.
GB191214458A (en) Improvements in Reversible Rotary Motors.
GB107892A (en) Improvements in or relating to Rotary Internal Combustion Engines.
GB137719A (en) Improvements in internal combustion turbines
GB191109410A (en) An Improved Rotary Engine.
GB296564A (en) Improvements in rotary engines and pumps
GB191026118A (en) Improvements in Rotary Internal Combustion Engines.
GB191408707A (en) Improvements in Direct Acting Internal Combustion Turbines.
GB191224567A (en) Improvements in or relating to the Lubrication of Rotary Explosion Engines.
GB191506615A (en) Improvements in Rotary Valves for Internal Combustion Engines.
GB131176A (en) Improvements in Rotary Internal Combustion Engines.
GB189824851A (en) A New or Improved Rotary Motor.
GB191022872A (en) Improvements in Rotary Engines.
GB191408433A (en) Improvements in and relating to Hydraulic Turbines.
GB191007375A (en) Improvements in Internal Combustion Turbines.
GB151448A (en) Improvements in rotary engines, compressors and pumps
GB191108010A (en) An Improved Rotary Motor.
GB191320938A (en) Improvements in and relating to Gas Turbines.
GB191028174A (en) Improvements in and relating to Rotary Engines.
GB191205546A (en) Improvements in Roatry Internal Combustion Engines.
GB447111A (en) Improvements in or relating to power plants