Fuel injection valve

A fuel injection valve comprising:

• a nozzle that includes
• a nozzle cylinder portion forming a fuel passage therein,
• a nozzle bottom portion closing one end of the nozzle cylinder portion,
• a plurality of nozzle holes connecting a surface of the nozzle bottom portion on a side of the nozzle cylinder portion with a surface on an opposite side from the nozzle cylinder portion to inject fuel in the fuel passage, and
• an annular valve seat formed around the nozzle holes on the surface of the nozzle bottom portion on the side of the nozzle cylinder portion;
• a needle that is reciprocally movable inside the nozzle, the needle configured to contact with the valve seat to close the nozzle holes and to separate from the valve seat to open the nozzle holes;
• and
• a drive unit that is configured to move the needle in one of a valve opening direction and a valve closing direction, wherein
• a nozzle hole of the plurality of nozzle holes includes
• an inlet opening portion formed on the surface of the nozzle bottom portion on the side of the nozzle cylinder portion,
• an outlet opening portion formed on the surface of the nozzle bottom portion on the opposite side from the nozzle cylinder portion, and
• a nozzle hole inner wall connecting the inlet opening portion with the outlet opening portion,
• an area of the outlet opening portion is larger than an area of the inlet opening portion,
• at least one of the nozzle holes of the plurality of nozzle holes is a non-circular nozzle hole in which a ratio of a longest diameter to a shortest diameter of the outlet opening portion is greater than 1, and at least another one of the nozzle holes of the plurality of nozzle holes is a circular nozzle hole,
• a virtual circular cone is defined as a virtual cone having
• a vertex, which is an intersection point between a nozzle hole axis of the circular nozzle hole and the outlet opening portion, and
• two generatrices, which are in a cross-section along a first virtual plane including the nozzle hole axis of the circular nozzle hole, forming
• θf=θ+0.5×P{circumflex over ( )}0.6
• as an angle therebetween, in which
• θ (deg) is a nozzle hole open angle of the circular nozzle hole of the plurality of nozzle holes and in which the ratio of the longest diameter to the shortest diameter of the outlet opening portion is equal to 1,
• θf (deg) is a spray open angle of fuel to be injected from the circular nozzle hole, and
• P (MPa) is an average pressure of the fuel in the fuel passage when the fuel is injected from the circular nozzle hole,
• a virtual non-circular cone is defined as a virtual cone having
• a vertex, which is an intersection point between the nozzle hole axis of the non-circular nozzle hole and the outlet opening portion,
• two generatrices, which are in a cross-section along a second virtual plane including the nozzle hole axis of the non-circular nozzle hole, forming
• θf1=θ1+0.5×P{circumflex over ( )}0.6+17×e{circumflex over ( )}(−0.13×θ1)
• as a largest angle therebetween, and
• two generatrices, which are in a cross-section along a third virtual plane that includes the nozzle hole axis of the non-circular nozzle hole and intersects with the second virtual plane, forming
• θf2=θ2+0.5×P{circumflex over ( )}0.6
• as a smallest angle therebetween, in which
• θ1 (deg) is the largest nozzle hole open angle of the non-circular nozzle hole,
• θ2 (deg) is the smallest nozzle hole open angle,
• θf1 (deg) is the largest open angle of a fuel spray injected from the non-circular nozzle hole, and
• θf2 (deg) is the smallest open angle of the fuel spray injected from the non-circular nozzle hole, and
• at least two of the nozzle holes of the plurality of nozzle holes, which are adjacent to each other, are formed such that the virtual non-circular cone does not interfere with one of the virtual circular cone and the virtual non-circular cone.