Fuel injector nozzles
AssigneeOrbital Engine Company (Australia) Pty. Limited
InventorsRobert Max Davis, Jorge Manuel Pereira Dasilva
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AssigneeOrbital Engine Company (Australia) Pty. Limited
InventorsRobert Max Davis, Jorge Manuel Pereira Dasilva
Estimating the term…
An internal combustion engine fuel injector having a selectively openable nozzle (10) through which a fuel is delivered to the combustion chamber of the engine. The nozzle (10) comprises a port (12) having an internal annular surface (13) and a valve member (20) having an external annular surface coaxial with respect the internal annular surface. Sealing contact between the valve member and the port is provided therebetween along a circular seat line substantially coaxial to the respective annular surfaces. The annular surfaces are configured so that when the internal and external annular surfaces are in sealing contact along the circular seat line, the seat line is located adjacent the downstream end of the passage for delivery of fuel with respect to the direction of the flow of fuel through the passage. The maximum width of the passage between the annular surfaces is not substantially more than 30 microns.
An internal combustion engine fuel injector having a selectively openable nozzle through which fuel is delivered to a combustion chamber of the engine, said nozzle comprising a port having an internal annular surface and a valve member having an external annular surface co-axial with respect to the internal annular surface, said valve member being axially movable relative to the port to selectively provide between said internal and external annular surfaces a continuous passage for the delivery of fuel therethrough or sealing contact therebetween along a circular seat line substantially co-axial to the respective annular surfaces to prevent the delivery of fuel therebetween, said annular surfaces-being relatively configured so that when the internal and external annular surfaces are in sealing contact along said circular seat line said seat line is located adjacent the downstream end of the passage with respect to the direction of the flow of fuel through the passage, and the maximum width of the passage between said annular surfaces is not substantially more than 30 microns.
Dependencies are inferred from the claim text.