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    • 8. 发明专利
    • Improvements relating to Internal Combustion Engines.
    • GB134416A
    • 1919-11-06
    • GB2124518
    • 1918-12-19
    • PORTER JAMES ROBERTSON
    • PORTER JAMES ROBERTSON
    • F02B57/08
    • 134,416. Porter, J. R. Dec. 19, 1918. Valve-gear.-Aircraft &c. are propelled by one or more rotating-cylinder engines which gear with a rotating tank L carrying radial hollow rods M. and tubes N in which fuel is vaporized by the heat of exhaust gases escaping through valves in the cylinder heads. Each two-stroke-cycle engine A comprises a number of radial cylinders having exhaust valves Q actuated by a cam-ring N carried by the rotating fuel-tank L. Terminal admission ports U open into a common crank case.. to which combustible mixture is fed through a stationary hollow crank C having an air inlet K and a supply pipe E for combustible communication with a chamber F open to the fuel tank. The engines may be geared to the rotating tank by toothed wheels, or by sprocket-wheels and chains. Alternatively, the engagement of the valve stems with recesses in the ring N may rotate the tank, or a ring may be provided in which the recesses are dispensed with. Specification 111,374, [Class 4, Aeronautics], is referred to.