GB118646A - Improvements in or connected with Rotary Internal Combustion Engines. - Google Patents

Improvements in or connected with Rotary Internal Combustion Engines.

Info

Publication number
GB118646A
GB118646A GB806317A GB806317A GB118646A GB 118646 A GB118646 A GB 118646A GB 806317 A GB806317 A GB 806317A GB 806317 A GB806317 A GB 806317A GB 118646 A GB118646 A GB 118646A
Authority
GB
United Kingdom
Prior art keywords
blades
fixed
turbine
cooling
combustion chambers
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
GB806317A
Inventor
John William George
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 GB806317A priority Critical patent/GB118646A/en
Publication of GB118646A publication Critical patent/GB118646A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C11/00—Combinations of two or more machines or engines, each being of rotary-piston or oscillating-piston type
    • F01C11/006—Combinations of two or more machines or engines, each being of rotary-piston or oscillating-piston type of dissimilar working principle
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C1/00—Rotary-piston machines or engines
    • F01C1/30—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members
    • F01C1/40—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and having a hinged member
    • F01C1/44—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and having a hinged member with vanes hinged to the inner member

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

118,646. George, J. W. June 5, 1917. Fixed-abutment type; cooling parts. - In an internal-combustion turbine a rotary compressor having hinged vanes i co-operating with fixed abutments n draws in the gas mixture through the hollow shaft d and the rotor passage c and compresses it through ports s and suitably operated valves r into combustion chambers p arranged with their longitudinal axes oblique to the plane of the turbine wheel t<1> so as to discharge the exploded gases on to the turbine blades t<4> after the solid rim positions t<5>, which alternate with the sets of blades t<4>, have covered the outlets of the combustion chambers. Before discharging into the exhaust chamber y, the gases may pass through further sets of fixed and moving blades as shown. The compressor conduits e may be shaped as fan blades to circulate cooling air, or water-cooling may be used, with or without water jackets.
GB806317A 1917-06-05 1917-06-05 Improvements in or connected with Rotary Internal Combustion Engines. Expired GB118646A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB806317A GB118646A (en) 1917-06-05 1917-06-05 Improvements in or connected with Rotary Internal Combustion Engines.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB806317A GB118646A (en) 1917-06-05 1917-06-05 Improvements in or connected with Rotary Internal Combustion Engines.

Publications (1)

Publication Number Publication Date
GB118646A true GB118646A (en) 1918-09-05

Family

ID=32343154

Family Applications (1)

Application Number Title Priority Date Filing Date
GB806317A Expired GB118646A (en) 1917-06-05 1917-06-05 Improvements in or connected with Rotary Internal Combustion Engines.

Country Status (1)

Country Link
GB (1) GB118646A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3187507A (en) * 1961-11-20 1965-06-08 Jose Ignacio Martin Artajo Thermodynamic machine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3187507A (en) * 1961-11-20 1965-06-08 Jose Ignacio Martin Artajo Thermodynamic machine

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