Fuel injector having multiple rows of spray holes with different cross-sectional shapes for flow modulation
A nozzle body of a fuel injector includes a proximal end, a distal end spaced apart from the proximal end, and at least one spray hole positioned at the distal end. The at least one spray hole includes an inlet having a first cross-sectional shape and an outlet having a second cross-sectional shape different from the first cross-sectional shape. In other embodiments, the nozzle body has a first row of spray holes and a second row of spray holes, and a cross-sectional shape of spray holes in the first row is different from the cross-sectional shape of spray holes in the second row.
1 . A nozzle body of a fuel injector, comprising:
a proximal end;
a distal end spaced longitudinally apart from the proximal end; and
a first row of spray holes positioned at the distal end and a second row of spray holes positioned at the distal end longitudinally spaced apart from the first row of spray holes, the first row of spray holes including one or more spray holes having a uniform cross-sectional shape defined by a circle from an inlet end to an outlet end thereof and the second row of spray holes including one or more spray holes that include an inlet having a first cross-sectional shape and an outlet having a second cross-sectional shape different from the first cross-sectional shape, wherein a channel extending between the inlet and outlet in the second row of spray holes includes a transition in cross-sectional shape from the inlet to the outlet, wherein the first and second cross-sectional shapes of the one or more spray holes in the second row of spray holes are configured to reduce disproportionate flow of the fuel flow from the second row of spray holes relative to the first row of spray holes.
2 . The nozzle body of claim 1 , wherein the first cross-sectional shape is one of circular, elliptical, rounded rectangular, rounded triangular, or rounded polygonal.
3 . The nozzle body of claim 1 , wherein the second cross-sectional shape is one of elliptical, rounded rectangular, rounded triangular, or rounded polygonal.
4 . The nozzle body of claim 1 , wherein the first cross-sectional shape is circular and the second cross-sectional shape is one of vertically-oriented elliptical or horizontally-oriented elliptical.
5 . The nozzle body of claim 1 , wherein the first cross-sectional shape is vertically-oriented elliptical and the second cross-sectional shape is horizontally-oriented elliptical.
6 . The nozzle body of claim 1 , wherein the uniform cross-section of the one or more spray holes in the first row of spray holes and the first and second cross-sectional shapes of the one or more spray holes in the second row of spray holes are configured so that fuel flow from the first row of spray holes and fuel flow from the second row of spray holes decreases preferential cavitation of the fuel flow from the second row of spray holes to provide a same fuel flow through the first row of spray holes and through the second row of spray holes during all operating conditions.
7 . The nozzle body of claim 1 , wherein each of the spray holes in the first row of spray holes has a uniform cross-section from the inlet end to the outlet end thereof that is defined by a circle.
8 . The nozzle body of claim 1 , wherein the first cross-sectional shape of the inlet of the one or more spray holes in the second row of spray holes is defined by a circle and the second cross-sectional shape of the outlet is one of elliptical, rounded rectangular, rounded triangular, or rounded polygonal.
9 . The nozzle body of claim 1 , wherein the second row of spray holes is spaced longitudinally from the first row of spray holes toward the distal end of the nozzle body.
10 . A nozzle body of a fuel injector, comprising:
a nozzle sac having a first row of spray holes and a second row of spray holes spaced longitudinally below the first row of spray holes, wherein a cross-sectional shape of the spray holes in the first row is different from a cross-sectional shape of the spray holes in the second row so that fuel flow from the first row of spray holes and fuel flow from the second row of spray holes decreases preferential cavitation to reduce disproportionate flow of the fuel flow from the second row of spray holes relative to the first row of spray holes, wherein a channel extending between an inlet and an outlet in the second row of spray holes includes a transition in cross-sectional shape from the inlet to the outlet.
11 . The nozzle body of claim 10 , wherein the cross-sectional shape of spray holes in the first row is circular and the cross-sectional shape of spray holes in the second row is one of elliptical, rounded rectangular, rounded triangular, or rounded polygonal.
12 . The nozzle body of claim 11 , wherein the first row defines an upper row and the second row defines a lower row positioned longitudinally below the first row.
13 . The nozzle body of claim 10 , wherein the inlet defines a different cross-sectional shape than that of the outlet.
14 . The nozzle body of claim 13 , wherein the channel has a varying diameter along a length thereof.
15 . The nozzle body of claim 10 , wherein the inlet of the at least one spray hole in the second row is defined by a circle and the outlet of the at least one spray hole in the second row is one of elliptical, rounded rectangular, rounded triangular, or rounded polygonal.
16 . The nozzle body of claim 10 , wherein a number of spray holes in the first row is equal to a number of spray holes in the second row.
17 . The nozzle body of claim 16 , wherein the number of spray holes is 10 spray holes.
18 . The nozzle body of claim 10 , wherein the cross-sectional shape of each spray hole in the first row of spray holes is defined by a circle from an inlet end thereof to an outlet end thereof.
19 . The nozzle body of claim 10 , wherein the cross-sectional shape of only part of the spray holes in the second row is different than the cross-sectional shape of the spray holes in the first row.
20 . The nozzle body of claim 10 , wherein a coefficient of discharge of the cross-sectional shape of the spray holes in the second row is configured to provide a same fuel flow from the second row of spray holes as the first row of spray holes under all operating conditions.