OEC orbital corporation limited

Patent app # 20040123833(Nissan/Renault) Good find Ralph. This...

  1. 262 Posts.
    Patent app # 20040123833(Nissan/Renault)

    Good find Ralph. This does not surprise me, as I had heard that
    Renault was going with OCP. Further to this Nissan, whom is now
    doing gasoline engines for theRenault/Nissan Alliance (Renault will
    concentrate on Diesel), was told to forget HPDI and use OCP for all
    future Nissan/Renault Gasoline engines.

    This particular patent(actal # is 20040123833) has several
    embodiments, several of which are just generic BS. The important one
    is the 2nd one, which is Orbital OCP.

    "SECOND EMBODIMENT

    [0077] Referring now to FIGS. 6 and 7, a direct fuel injection spark
    ignition internal combustion engine in accordance with a second
    embodiment will now be explained. In view of the similarity between
    the first and second embodiments, the parts of the second embodiment
    that are identical to the parts of the first embodiment will be
    given the same reference numerals as the parts of the first
    embodiment. Moreover, the descriptions of the parts of the second
    embodiment that are identical to the parts of the first embodiment
    may be omitted for the sake of brevity.

    [0078] FIG. 6 is a partial cross-sectional view of an injection
    portion of the direct fuel injection engine of the second
    embodiment. Basically, the direct fuel injection engine of the
    second embodiment is identical to the first embodiment shown in FIG.
    1, except that an air pump 14 is provided at the end of the intake
    camshaft, and a dual-fluid fuel injection valve 11" is used as the
    fuel injection valve 11. The air pressurized by the air pump 14 is
    conveyed to the dual-fluid fuel injection valve 11" via an air
    conduit 15 and injected into the combustion chamber 4 along with the
    fuel by the dual-fluid fuel injection valve 11". The dual-fluid fuel
    injection valve 11' is configured and arranged to inject the fuel
    and the air separately into the combustion chamber 4 in a
    predetermined ratio by controlling the lift of a needle valve of the
    dual-fluid fuel injection valve 11". When the lift of the needle
    valve is small, the area of the opening of the air nozzle connected
    to the air pump 14 and facing the dual-fluid fuel injection valve
    11' is small or substantially zero (in other words, closed). Thus,
    the ratio of the mass of the air to the mass of the fuel between the
    air and fuel injected into the combustion chamber 4 is small. When
    the lift of the needle valve is large, the area of the opening of
    the air nozzle is large. Thus, the ratio of the mass of the air to
    the mass of the fuel increases. Accordingly, the fuel-air mass ratio
    between the fuel and air injected from the dual-fluid fuel injection
    valve 11" can be easily varied by varying the amount of air injected
    from the dual-fluid fuel injection valve 11". The dual-fluid fuel
    injection valves are conventional components that are well known in
    the art. Since the dual-fluid fuel injection valves are well known
    in the art, these structures will not be discussed or illustrated in
    detail herein.

    [0079] FIG. 7(a) is a diagrammatic chart illustrating the
    relationship between the engine operating load and the injected fuel-
    air mass ratio in accordance with the second embodiment of the
    present invention. FIGS. 7(b)-7(d) are diagrammatic cross-sectional
    views of the combustion chamber 4 illustrating distributions of the
    air-fuel mixture in the combustion chamber 4 under various engine
    operating regions shown in FIG. 7(a).

    [0080] As seen in FIG. 7(a), the direct fuel injection engine is
    configured and arranged to increase the mass ratio of the fuel
    injected to the air when the direct fuel injection engine is
    operating in a low-load stratified combustion region A. By
    increasing the mass ratio of the fuel to the air, the fuel injection
    angle is increased. Thus, as seen in FIG. 7(b), a first air-fuel
    mixture having superior ignitability and combustion stability can be
    formed in the upper center portion of the combustion chamber 4 where
    the spark plug 12 is located before the fuel stream collides against
    the cavity 3a of the piston.

    [0081] On the other hand, as seen in FIG. 7(b), the direct fuel
    injection engine is configured and arranged to decrease the mass
    ratio of the fuel to the air injected into the combustion chamber 4
    when the direct fuel injection engine is operating in the high-load
    stratified combustion region B. When the mass ratio of the fuel to
    the air is decreased, the fuel injection angle becomes smaller.
    Thus, as seen in FIG. 7(c), comparatively large second air-fuel
    mixture mass can be formed from the interior to the exterior of the
    cavity 3a after the fuel stream collides against the bottom surface
    of the cavity 3a and the diffusion and mixing of the fuel stream is
    promoted. As explained above, the fuel-air mass ratio between the
    fuel and air injected from the dual-fluid fuel injection valve 11"
    can be easily varied by varying the amount of air injected.

    [0082] In the homogeneous combustion region C, a homogeneous air-
    fuel mixture fills the combustion chamber 4, as seen in FIG. 7(d).
    In the second embodiment of the present invention, the fuel mass
    ratio to the air in the homogeneous combustion mode is preferably
    set to a relatively large as shown in FIG. 7(a) to achieve a
    relatively large fuel injection angle. However, it is apparent to
    those skilled in the art from this disclosure that the fuel mass
    ratio in the homogeneous combustion region C is not limited to the
    ratio shown in FIG. 7(a). Rather, the fuel mass ratio in the
    homogeneous combustion region C can be set to any value as long as
    the air-fuel mixture that achieves the homogeneous combustion can be
    formed in the combustion chamber as shown in FIG. 7(d) to carry out
    the present invention.

    [0083] FIG. 8 is a flow chart of the control executed in the ECU 13
    of the direct fuel injection engine in accordance with the second
    embodiment. Steps S21-S23 in FIG. 8 are basically identical to steps
    S1-S3 in FIG. 5(a) of the first embodiment. When it is determined in
    step S22 to perform a homogeneous combustion or when it is
    determined in step S23 that the load is smaller than the prescribed
    load (when the direct fuel injection engine is operating in a low-
    load stratified combustion region A), the ECU 13 is configured to
    set the fuel injection angle to be a relatively large angle in step
    S26. Thus, in step S27, the lift of the needle valve of the dual-
    fluid fuel injection valve 11" is reduced to achieve the relatively
    large fuel injection angle by reducing the amount of air and
    increasing the mass ratio of the fuel injected from the dual-fluid
    fuel injection valve 1". When it is determined in step S24 that the
    load is greater than the prescribed load (when the direct fuel
    injection engine is operating in a high-load stratified combustion
    region B), the ECU 13 is configured to set the fuel injection angle
    to be a relatively small angle in step S24. Thus, in step S25, the
    lift of the needle valve of the dual-fluid fuel injection valve 11"
    is increased to achieve a small fuel injection angle by increasing
    the amount of air and decreasing the fuel mass ratio of the fuel
    injected from the dual-fluid fuel injection valve 11".

    [0084] Accordingly, in the second embodiment of the present
    invention, the dual-fluid fuel injection valve 11" is used as a fuel
    injection valve, and the injected liquid-air mass ratio (the mass
    ratio of fuel) is increased or decreased to control the fuel
    injection angle. Thus, the fuel injection angle can be varied merely
    by controlling the dual-fluid fuel injection valve 11" without
    increasing the complexity of the injection valve structure. "


 
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