Patent ID: 8342430

Claim:
A fuel injection valve comprising: a valve body; a valve seat member which slidably accommodates therein the valve body and has (a) a valve seat on which the valve body is seated during valve closure; and (b) an opening portion formed at a downstream side of the valve seat member; a swirl chamber which is formed into a circular hollow shape at a downstream side of the opening portion of the valve seat member and has a cylindrical inner side surface, the swirl chamber providing swirl to fuel; an orifice nozzle which is formed into a cylindrical shape at a bottom of the swirl chamber, and from which the fuel is jetted; a communication conduit through which the swirl chamber communicates with the opening portion of the valve seat member, the communication conduit extending toward a tangential direction of the swirl chamber and connecting with the swirl chamber; and a fuel inflow prevention wall which is provided at a connecting area between the communication conduit and the swirl chamber, and when setting a first connecting point, a second connecting point, a first straight line, a second straight line and a third straight line, viewed from an axial direction of the swirl chamber, in the swirl chamber, as follows; the first connecting point is a connecting point between the communication conduit and the inner side surface of the swirl chamber on a tangent of the swirl chamber, the second connecting point is a connecting point between the communication conduit and the inner side surface of the swirl chamber, which differs from the first connecting point, the first straight line is a tangent of the orifice nozzle, which is perpendicular to a direction of the tangent of the inner side surface of the swirl chamber on the first connecting point and is closer to the second connecting point, the second straight line is a straight line which passes through the second connecting point and is perpendicular to the direction of the tangent of the inner side surface of the swirl chamber on the first connecting point, and the third straight line is a tangent of the orifice nozzle, which is parallel to the direction of the tangent of the inner side surface of the swirl chamber on the first connecting point and is closer to the first connecting point, the orifice nozzle being positioned at a center side with respect to the second straight line in the swirl chamber, and the fuel inflow prevention wall being set at a first connecting point side with respect to the third straight line with the fuel inflow prevention wall extending from the first straight line to the second straight line.