AVIATION GASOLINE ENGINE COOLANT INJECTION SYSTEM

    公开(公告)号:US20190032552A1

    公开(公告)日:2019-01-31

    申请号:US16047580

    申请日:2018-07-27

    Abstract: A set of apparatus to inject distilled-water in solution acting as an engine coolant into the combustion chamber of a high-compression air-cooled piston aircraft engine to mix with aviation gasoline, operating on a minimum 91 motor octane aviation gasoline (leaded or unleaded), thereby improving engine performance, and suppressing early detonation in prescribed operating situations. The apparatus incorporates 1) an ultra-light weight corrosion-resistant engine coolant storage compartment mounted inside the aircraft, 2) stainless steel pipe fittings, 3) controller activated fluid injectors with wide spray nozzles, 4) aircraft-approved wiring and stainless steel plumbing tied to the pump and combustion chamber, 5) a primary and back-up electric pump approved for aviation use, 6) a special formulation of water-based cooling fluid in solution with a non-toxic anti-freezing agent designed for high altitude aircraft use, 7) electric sensors for temperature, pressure and early detonation programmed to a sensory control unit that automatically activates the electric pump to inject coolant only on pre-configured conditions during periods of peak engine performance when early detonation is most likely to occur, 8) a is digital metering display for the pilot instrument panel capable to report cylinder-head temperature, manifold pressure, oxygen (air/fuel ratio) and an aviation approved knock-sensor, and 8) a test switch and automatic operation on-off switch.

    Spark plug size adaptor assembly
    4.
    发明授权

    公开(公告)号:US10594114B2

    公开(公告)日:2020-03-17

    申请号:US15989710

    申请日:2018-05-25

    Abstract: A spark plug assembly configured to allow multi-channel automotive spark-plugs to operate without radio-frequency interference in piston-engine powered aircraft and to greatly reduce or eliminate spark-plug fouling from carbon or lead deposits resulting from combustion of fuel in order to enhance starting and smooth operation of the aircraft engine, and thereby improve the quality of exhaust emissions by assuring a more complete burn of the fuel constituents.

    SPARK PLUG ASSEMBLY
    5.
    发明申请
    SPARK PLUG ASSEMBLY 审中-公开

    公开(公告)号:US20180342855A1

    公开(公告)日:2018-11-29

    申请号:US15989710

    申请日:2018-05-25

    CPC classification number: H01T13/08 H01T13/467

    Abstract: A spark plug assembly configured to allow multi-channel automotive spark-plugs to operate without radio-frequency interference in piston-engine powered aircraft and to greatly reduce or eliminate spark-plug fouling from carbon or lead deposits resulting from combustion of fuel in order to enhance starting and smooth operation of the aircraft engine, and thereby improve the quality of exhaust emissions by assuring a more complete burn of the fuel constituents.

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