GB111124A - Improvements in Internal Combustion Engines for Aeroplanes and the like. - Google Patents

Improvements in Internal Combustion Engines for Aeroplanes and the like.

Info

Publication number
GB111124A
GB111124A GB1354716A GB1354716A GB111124A GB 111124 A GB111124 A GB 111124A GB 1354716 A GB1354716 A GB 1354716A GB 1354716 A GB1354716 A GB 1354716A GB 111124 A GB111124 A GB 111124A
Authority
GB
United Kingdom
Prior art keywords
cylinders
ports
pump
piston
sleeve
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
GB1354716A
Inventor
Arthur Harold Wilks
Percy Harold Hartshorne
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 GB1354716A priority Critical patent/GB111124A/en
Publication of GB111124A publication Critical patent/GB111124A/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
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B57/00—Internal-combustion aspects of rotary engines in which the combusted gases displace one or more reciprocating pistons
    • F02B57/08—Engines with star-shaped cylinder arrangements
    • F02B57/10—Engines with star-shaped cylinder arrangements with combustion space in centre of star

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Reciprocating Pumps (AREA)

Abstract

111,124. Wilkes, A. H., and Hartshorne, P. H. Sept. 25, 1916. Two-stroke-cycle engines; driving-gear; cylinders, construction of.-In a revolving-cylinder engine, oppositely moving pistons f<2>, f<3> compress pump charges in the closed ends of the cylinders and drive through stationary cam tracks c. The cylinders rotate with the central shaft e<2> inside a fixed aluminium casing b<2> having inlet ports which register with ports g<5> in an aluminium or other casing carrying the cylinder liners. The piston f<3> reciprocates in a sleeve f<4> on the piston f<2>, the sleeve controlling the transfer ports i<2>, i<3> from the pump ends of the cylinders and the exhaust port k. Combustible mixture enters the pump spaces when the ports g<2> g<3> are uncovered by the pistons at the ends of the compression strokes.
GB1354716A 1916-09-25 1916-09-25 Improvements in Internal Combustion Engines for Aeroplanes and the like. Expired GB111124A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1354716A GB111124A (en) 1916-09-25 1916-09-25 Improvements in Internal Combustion Engines for Aeroplanes and the like.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1354716A GB111124A (en) 1916-09-25 1916-09-25 Improvements in Internal Combustion Engines for Aeroplanes and the like.

Publications (1)

Publication Number Publication Date
GB111124A true GB111124A (en) 1917-11-22

Family

ID=32248981

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1354716A Expired GB111124A (en) 1916-09-25 1916-09-25 Improvements in Internal Combustion Engines for Aeroplanes and the like.

Country Status (1)

Country Link
GB (1) GB111124A (en)

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