turning now to the figures , fig1 depicts a cross - sectional of a nozzle 20 constructed in accordance with the teachings of the present invention . the nozzle 20 is formed at a lower end of a low pressure fuel injector which is used to deliver fuel to a cylinder 10 of an engine , such as an internal combustion engine of an automobile . an injector body 22 defines an internal passageway 24 having a needle 26 positioned therein . the injector body 22 defines a longitudinal axis 15 , and the internal passageway 24 extends generally parallel to the longitudinal axis 15 . a lower end of the injector body 22 defines a nozzle body 32 . it will be recognized by those skilled in the art that the injector body 22 and nozzle body 32 may be integrally formed , or alternatively the nozzle body 32 may be separately formed and attached to the distal end of the injector body 22 by welding or other well known techniques . in either case , the nozzle body 32 defines a valve seat 34 leading to a valve outlet 36 . the needle 26 is translated longitudinally in and out of engagement with the valve seat 34 preferably by an electromagnetic actuator or the like . in this manner , fuel flowing through the internal passageway 24 and around the needle 26 is either permitted or prevented from flowing to the valve outlet 36 by the engagement or disengagement of the needle 26 and valve seat 34 . the nozzle 20 further includes a metering plate 40 which is attached to the nozzle body 32 . it will be recognized by those skilled in the art that the metering plate 40 may be integrally formed with the nozzle body 32 , or alternatively may be separately formed and attached to the nozzle body 32 by welding or other well known techniques . in either case , the metering plate 40 defines a nozzle cavity 42 receiving fuel from the valve outlet 36 . the nozzle cavity 42 is generally defined by a bottom wall 44 and a side wall 46 which are formed into the metering plate 40 . the metering plate 40 further defines a plurality of exit cavities 50 receiving fuel from the nozzle cavity 42 . each exit cavity 50 is radially spaced from the longitudinal axis 15 and meets the nozzle cavity 42 at an exit orifice 52 . as can also be seen in fig1 , the metering plate 40 includes an annular wall 56 extending around each exit orifice 52 . similarly , the nozzle body 32 provides an annular wall 54 extending around the entrance orifice 38 . [ note : the nozzle cavity 42 meets the valve outlet 36 at an entrance orifice 38 ] accordingly , it will be seen that fuel flowing through the valve outlet 36 must flow downwardly and radially outwardly around the annular wall 54 , and then upwardly and radially outwardly around the other annular wall 56 in order to reach the exit cavity 50 . in this manner , atomization of the fuel is enhanced by adding turbulence to the fuel flowing through the metering plate 40 . it will be recognized that the annular walls 54 , 56 can be either continuous or intermittent . turning to fig2 , another embodiment of the annular wall 56 has been depicted and denoted as 56 a . it can be seen from the figure that the annular wall 56 a follows a zig - zag or star - shape around the perimeter of the exit orifice 52 . it will be recognized by those skilled in the art that the other annular wall 54 may also take this shape . it can also be seen that the exit orifice 52 also takes the zig - zag shape . by way of this structure , additional turbulence is added to the fuel flow through the metering plate 40 to further enhance atomization . turning now to fig3 , yet another embodiment of the annular wall 56 is shown and is denoted as 56 b . in this embodiment , the annular wall 56 b includes vertical serrations 57 . these serrations 57 and the annular walls 56 b further increase the turbulence of the fuel flowing through the metering plate 40 , thereby improving the atomization of the fuel . turning now to fig4 , still yet another embodiment of the metering plate 40 is shown which increases the turbulence and enhances atomization of the fuel . as shown , the bottom wall 44 of the nozzle cavity 42 includes serrations 58 formed in an area circumscribing each exit orifice 52 in exit cavity 50 . more particularly , the serrations 58 rise above the level of the bottom wall 44 of the nozzle cavity 42 . in essence , the serrations 58 form a plurality of annular walls extending around each exit orifice 52 . it can also be seen that the serrations 58 stop short of the exit orifice 52 and leave a generally planar area 59 extending around the exit orifice 52 . a related embodiment is shown in fig5 and 6 . in this embodiment , an area 60 of the bottom wall 44 adjacent each exit orifice 52 includes a plurality of linear grooves 62 . as shown in fig6 , the grooves 62 extend downwardly into the nozzle body 40 . the grooves extend in a direction not aligned with the radial axis 55 of the adjacent exit orifice 52 , and preferably is generally perpendicular to the radial axis 55 . as best seen in fig6 , the exit orifice 52 will inherently take a serrated or zig - zag shape corresponding to the grooves 62 formed into the bottom wall 44 . the grooved area may be square or rectangular in shape , or may also generally circular in shape to correspond with the shape of the exit orifice 52 . in this manner , the fuel flow will encounter the series of grooves 62 as it flows radially outward to the exit orifice 52 and exit cavity 50 , thereby increasing the turbulence thereof and promoting atomization of the fuel flowing to the engine cylinder 10 . the foregoing description of various embodiments of the invention has been presented for purposes of illustration and description . it is not intended to be exhaustive or to limit the invention to the precise embodiments disclosed . numerous modifications or variations are possible in light of the above teachings . the embodiments discussed were chosen and described to provide the best illustration of the principles of the invention and its practical application to thereby enable one of ordinary skill in the art to utilize the invention in various embodiments and with various modifications as are suited to the particular use contemplated . all such modifications and variations are within the scope of the invention as determined by the appended claims when interpreted in accordance with the breadth to which they are fairly , legally , and equitably entitled .