JP3327167B2 - Fuel injection nozzle - Google Patents

Description

DETAILED DESCRIPTION OF THE INVENTION

[0001]

BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a fuel injection nozzle, and more particularly to a structure of a fuel injection nozzle.

[0002]

2. Description of the Related Art In order to improve the exhaust emission of a diesel engine, for example, Japanese Patent Application Laid-Open No. 8-261111 discloses a fuel injection nozzle in which the effective area of a fuel injection port is gradually increased in accordance with the lift amount of a needle valve. Proposed. Specifically, as shown in FIG. 3 of the above-mentioned publication, the fuel injection port in this case has the fuel injection port as a long hole, and its major axis direction is directed in the vertical direction, which is the axial direction of the nozzle body, or One in which the major axis direction of the long hole is oriented in the horizontal direction at an angle of 90 ° with respect to the axis of the nozzle body has been proposed. Further, in FIG. 5 of the above publication, for the same purpose, a plurality of nozzles are provided at different positions in the vertical direction of the nozzle body so that the nozzles are sequentially opened from the lower nozzles as the needle valve lifts. What has been proposed.

[0003]

However, in the case where the fuel injection port is a long hole and its major axis is directed in the vertical direction, the lift amount of the needle valve must be increased in order to change the injection port from the fully closed state to the fully open state. In addition to this problem, in a direct injection type diesel engine, there is also a problem that the collision position of the fuel spray with respect to the side wall surface of the piston cavity widens in the depth direction, thereby deteriorating the exhaust emission. Further, in the case where the fuel injection port is a long hole and its major axis is directed in the horizontal direction, the fuel spray spreads greatly horizontally in the fully opened state, and the high-speed air swirl flow in the combustion chamber causes the adjacent fuel to spread as shown in FIG. There is a problem in that the spray F interferes with an excessively rich mixture region (shaded lines in FIG. 9), which causes the generation of smoke.

Further, when a plurality of nozzles are provided at different positions in the vertical direction of the nozzle body, the collision position of the fuel spray with respect to the side wall surface of the piston cavity in the depth direction depends on the positions of the sequentially opened upper and lower nozzles. The fuel spray supplied from the relatively small-diameter orifices, which are spaced apart and isolated, has a weak penetrating power. There is also a problem that the fuel swirl is caused to flow by the air swirl flow without reaching the side wall surface of the piston cavity, so that a good air-fuel mixture is not generated and exhaust emission is deteriorated.

[0005] Accordingly, the present invention is to solve such a problem, and an object of the present invention is to provide a fuel injection nozzle capable of greatly improving exhaust emission.

[0006]

In order to achieve the above object, according to the present invention, a plurality of recesses are formed on an outer peripheral surface of a nozzle body (1) at a plurality of positions on an outer periphery thereof without being driven to rotate.
A fuel injection port (14) opened and closed by a needle valve (2) not formed is formed, and the opening portion of each fuel injection port (14) is extended.
As a hole, the major axis direction is inclined by a predetermined angle (θ) smaller than 90 ° with respect to the axis (L) of the nozzle body (1).
Incline.

In the first aspect of the present invention, when the needle valve rises, the opening of the fuel injection port is opened, and the fuel is injected as a strip spray inclined at a predetermined angle with respect to the axis of the nozzle body. Since the band spray is inclined at a predetermined angle, the collision position of the band spray of the fuel with respect to the side wall surface of the piston cavity can be limited to a limited range in the depth direction. Formation can be realized. Further, even if the amount of rise of the needle valve is limited, the injection port area can be largely changed due to the inclination of the opening. Furthermore, it is possible to prevent the interference of the zonal spray from the adjacent fuel injection port at the time of high speed and high load, thereby avoiding the generation of the rich mixture region, and in the axial direction and the circumferential direction of the combustion chamber. The fuel spray can be widely dispersed. As a result,
A good air-fuel mixture is formed in the combustion chamber, so that proper combustion is realized, and high output of the engine and improvement of exhaust emission are realized.

The opening of each of the fuel injection ports (14) is constituted by a plurality of through holes (141 to 143) which are adjacent to each other and linearly connected, and fuel injected from these through holes (141 to 143) is provided. A substantially identical fuel spray is formed, and the direction in which the through holes (141 to 143) are linearly connected is changed by a predetermined angle smaller than 90 ° with respect to the axis (L) of the nozzle body (1). It may be inclined.

According to this, the injected fuel sprays merge to form a strip spray having a width in the direction in which the through holes are continuous.
Therefore, even with such a configuration, the same operation and effect as described above can be obtained, and the processing operation is easier when a plurality of through holes are continuously formed than when a long hole is formed.

A plurality of adjacent through holes (141 to 143) linearly connected to each other are defined by the axis (L) of the nozzle body (1).
May be formed so as to form different angles (θ1 to θ3) with respect to the axis (L) in a vertical plane including the following. Thus, as a collision area of the side wall surfaces of or interfere fuel spray from adjacent spray port to each other or the piston cavities not being spread excessively.

[0011]

BEST MODE FOR CARRYING OUT THE INVENTION

(First Embodiment) FIG. 1 shows a cross section of a nozzle body 1 of a fuel injection nozzle. In the figure, the nozzle body 1 is cylindrical in its entirety, and the diameter of the nozzle body is reduced stepwise from the large-diameter portion 11 at the base end (upper end in the figure) and extends to the distal end. It is 12. A needle valve 2 is housed in the nozzle body 1 so as to be slidable up and down, and a small-diameter orifice area control section 21 formed at the tip thereof is in contact with the inner periphery of the sack section 12, and the sack section A fuel injection hole 14 described later formed through a plurality of locations on the outer periphery of the fuel injection port 12 is closed. The fuel nozzle 2 has a fuel passage 2 at its base end in the horizontal direction.
2 is formed therethrough, and a fuel passage 23 extending from the intermediate position to the front end is formed. The needle valve 2 is urged toward the distal end (downward in the figure) by a spring member (not shown).
Is in pressure contact with the valve seat 15 on the inner periphery of the nozzle body 1. A fuel flow gap 16 extending in the vertical direction is formed between the outer periphery of the intermediate portion 25 of the needle valve 2 and the inner periphery of the nozzle body 1, and the upper end thereof is formed around the needle valve 2 in the large diameter portion 11 of the nozzle body. The fuel tank 17 communicates with the fuel tank 17. A fuel supply passage 18 extends from diagonally above the fuel reservoir 17.
As shown in FIG. 2, each fuel injection port 14 on the outer periphery of the sack portion 12 is a long hole having both ends formed in an arc shape, and its major axis direction is at an angle θ with respect to the axis L of the nozzle body 1. It is inclined.

In the fuel injection nozzle having such a structure, the needle valve 2 is at the lowered position in FIG. 1 in a state where the fuel is not fed to the fuel supply passage 18 at this position. Is pressed against the valve seat 15 to shut off the space between the fuel flow gap 16 and the fuel passage 22 (FIG. 3A), and the fuel injection port 14 is closed by the injection port area control unit 21 so that the fuel injection is stopped. Not done. During low engine load operation, low pressure fuel is pumped into the fuel supply passage 18 and the needle valve 2 rises (lifts) in response to the increase in the pressure in the oil sump 17, as shown in FIG. The part 24 is separated from the valve seat 15 and the fuel nozzle 14 is partially opened by the upward movement of the nozzle area control part 21 so that a required amount of fuel is injected as a band-shaped spray having a predetermined width. During high engine load operation, high pressure fuel is fed to the fuel supply passage 18 and the needle valve 2 moves to the rising end. In this state, as shown in FIG.
The entire fuel nozzle 14 is opened, and the maximum amount of fuel is injected and supplied as a band-shaped spray having the maximum width inclined at an angle θ with respect to the axis L of the nozzle body 1.

In this manner, the fuel is injected and supplied as a band-shaped spray from the long-hole fuel injection port 14, and the width of the band-shaped spray is continuously changed according to the lift amount of the needle valve 2. Thus, stable engine operation is realized because the injected fuel amount does not change suddenly. In addition, when the opening area of the fuel injection port 14 is small, it substantially corresponds to an extremely small injection port diameter, so that the atomization of fuel spray and the turbulent mixing effect are promoted, and the exhaust gas is reduced in particulates. And fuel injection port 1
In the case where the opening area of the nozzle 4 is large, a band-like spray having a sufficient width is formed, so that the momentum of the spray jet increases, and a large spray penetration force required at the time of engine high load and high rotation, which is not affected by the air swirl flow, is obtained. can get.

Further, in the present embodiment, since the long hole of the fuel injection port 14 is inclined by a predetermined angle θ with respect to the axis L of the nozzle body 1, the following operation and effect can be obtained. That is, the vertical direction along the axis L (θ = 0)
°) compared to positioning the long hole of the fuel injection port 14
By inclining the long hole by an appropriate angle θ larger than °, it is possible to limit the collision position of the fuel strip spray to the piston cavity side wall surface within a limited range in the depth direction. It is possible to realize a proper mixture formation. Further, even when the lift amount of the needle valve 2 (d in FIG. 3C) is limited, the injection hole area can be largely changed by the inclination of the long hole by the appropriate angle θ. Further, as compared with the case where the long hole of the fuel injection port 14 is positioned in the horizontal direction (θ = 90 °) orthogonal to the axis L, the long hole of the fuel injection port 14 is inclined by an appropriate angle θ smaller than 90 °. By doing so, it is possible to prevent the interference of the zonal spray from the adjacent fuel injection ports 14 at the time of high speed and high load, thereby avoiding the generation of the rich mixture region and the axial direction of the combustion chamber. The fuel spray can be widely dispersed in the direction. As a result,
A good air-fuel mixture is formed in the combustion chamber, so that proper combustion is realized, and high output of the engine and improvement of exhaust emission are realized.

In this embodiment, the needle valve 2
In addition to performing the lift by the fuel pressure, the lift can be performed mechanically or electrically, and furthermore, by hydraulic pressure.

(Second Embodiment) The shape of the long hole of the fuel injection port 14 is not limited to that in the first embodiment, but is shown in FIG.
Various shapes as shown in (A) to (E) can be adopted. That is, FIGS. 4A and 4D are shapes suitable for obtaining a sufficient fuel increase rate in the early stage of injection, and FIG. 4B is a shape suitable for suppressing the fuel increase rate in the initial or late period of injection. FIG. 4C shows a shape suitable for suppressing the fuel increase rate at the beginning of the injection, and FIG. 4E shows a shape suitable for obtaining a curved band spray. In addition, the inclination angle θ of the curved elongated hole is an angle formed by a straight line connecting both ends thereof with the axis L of the nozzle body 1.

(Third Embodiment) FIG. 5 shows the appearance of a sack portion 12 at the tip of the nozzle body 1 in this embodiment. In the figure, fuel injection holes 14 are formed at a plurality of positions in the circumferential direction on the outer periphery of the sack portion 12, and each fuel injection hole 14 has a plurality (three in this embodiment) of small-diameter circular through-holes 141 to 143.
It consists of. Through hole 1 constituting fuel injection port 14
41 to 143 are linearly adjacent to each other, and the direction of the inclination is inclined by a predetermined angle θ with respect to the axis L of the nozzle body 1. In such a structure, the needle valve 2
Rises, the through hole 1 below each fuel injection port
Opened sequentially from 41. At this time, the through holes 1 of each nozzle 14
The fuel sprays injected from the through holes 141 to 143 join together to form a band spray having a width in the direction in which the through holes 141 to 143 are connected. Therefore, also in the present embodiment, the same operation and effect as those of the first embodiment can be obtained, and the processing operation is easier when a plurality of circular through holes are continuously formed than when a long hole is formed. It is.

(Fourth Embodiment) Through Holes 1 Constituting Each Orifice
It is not always necessary that all of 41 to 143 have the same diameter as in the third embodiment, and for example, FIGS.
As shown in (1), the through holes 141 to 143 can be of different diameters so as to obtain desired injection characteristics when sequentially opened. 6A is suitable for suppressing the fuel increase rate in the early and late stages of the injection, FIG. 6B is suitable for suppressing the fuel increase rate in the early stage of the injection, and FIG.
(C) is suitable for obtaining a sufficient fuel increase rate at the beginning of the injection. In FIG. 7D, the through holes 141 to 143 are shown.
Are arranged close to each other in the form of an arc curve, thereby obtaining a curved band-shaped spray as in the case of FIG. 4E of the second embodiment.

(Fifth Embodiment) Each of the through holes 141 to 143 constituting the injection port in the third and fourth embodiments is
As shown in FIGS. 7A to 7C, a different angle θ1 with respect to the axis L in the vertical plane including the axis L of the nozzle body 1
Through .theta.3. For example, if the angle θ1 of the through hole 141 at the lowermost position is maximized, the angle θ2 of the through hole 142 at the intermediate position, and the angle θ3 of the through hole 143 at the uppermost position are sequentially reduced, the operation and effect of the first embodiment can be obtained. In addition, the collision position of the spray when all of the through holes 141 to 143 are opened can be narrowed to substantially the same depth on the side wall surface of the piston cavity, and a more favorable air-fuel mixture can be formed.

It should be noted that in an engine which does not form an air-fuel mixture by colliding with the side wall surface of the piston cavity, but which forms a proper air-fuel mixture by ensuring the spatial dispersion of the spray itself, Angle θ1 to θ3 to θ1 <θ
By setting as 2 <θ3, the spray can be diffused widely in the depth direction of the piston cavity.

As described above, in the present embodiment, each through hole 1 with respect to the nozzle body 1 in the vertical plane including the axis L is provided.
Since the inclination angles .theta.1 to .theta.3 of 41 to 143 are set to be appropriately different, the collision area on the side wall surface of the piston cavity is not excessively widened, and the fuel sprays from the adjacent injection ports do not interfere with each other. I can do it.

(Sixth Embodiment) As shown in FIG. 8, the lower end of the fuel passage 23 in the nozzle area control unit 21 is
If the fuel flow is formed so as to be inclined and opened toward 4, the fuel flow is smoothly guided to the injection port without causing separation at the injection port entrance. In particular, since the fuel flow can be jetted along the fuel injection port 14 even when the lift amount of the needle valve 2 is small (arrow in FIG. 8A), the jetting direction of the spray can be stabilized.

[0023]

As described above, according to the fuel injection nozzle of the present invention, exhaust emission can be greatly improved.

[Brief description of the drawings]

FIG. 1 is an overall vertical sectional view of a nozzle body according to a first embodiment of the present invention.

FIG. 2 is a side view of a sack portion at a tip end of a nozzle body.

FIG. 3 is a longitudinal sectional view of a sack portion at a tip end of a nozzle body.

FIG. 4 is a schematic front view of a fuel injection port in a second embodiment of the present invention.

FIG. 5 is a side view of a sack portion at a tip end of a nozzle body in a third embodiment of the present invention.

FIG. 6 is a schematic front view of a fuel injection port according to a fourth embodiment of the present invention.

FIG. 7 is a longitudinal sectional view of a sack portion at a tip end of a nozzle body in a fifth embodiment of the present invention.

FIG. 8 is a half sectional view of a sack portion at a tip end of a nozzle body in a sixth embodiment of the present invention.

FIG. 9 is a diagram showing a distribution of fuel spray by a conventional fuel injection nozzle.

[Explanation of symbols]

DESCRIPTION OF SYMBOLS 1 ... Nozzle main body, 14 ... Fuel nozzle, 141, 142, 1
43: through hole, 2: needle valve, L: axis.

────────────────────────────────────────────────── ─── Continuation of the front page (72) Inventor Yoshihiro Hotta 41, 1-Cham Yokomichi, Nagakute-cho, Aichi-gun, Aichi Prefecture Inside Toyota Central Research Laboratory Co., Ltd. (56) References JP 8-218981 (JP, A) JP-A-7-224739 (JP, A) JP-A-62-103457 (JP, A) JP-A-53-113923 (JP, A) JP-A-10-122098 (JP, A) JP-A-10-252605 (JP, A) (58) Fields investigated (Int. Cl. ⁷ , DB name) F02M 61/18 350 F02M 61/18 330 F02M 61/10

Claims (3)

(57) [Claims] A rotary drive is provided at a plurality of locations on the outer periphery of a nozzle body.
The vertical movement to the fuel injection port that is opened and closed by not having a knee <br/> dollars valve recesses in the outer circumferential surface without being moving to form an opening portion of each fuel injection port as long holes, the major axis of the nozzle body A fuel injection nozzle which is inclined by a predetermined angle smaller than 90 ° with respect to an axis. 2. A fuel injection port which is opened and closed by a needle valve is formed at a plurality of locations on the outer periphery of a nozzle body, and an opening portion of each fuel injection port is constituted by a plurality of close-through linear through-holes. The fuel injected from the holes forms substantially the same fuel spray, and the direction in which the through holes are linearly connected is inclined by a predetermined angle smaller than 90 ° with respect to the axis of the nozzle body. A fuel injection nozzle. 3. A fuel injection port, which is opened and closed by a needle valve, is formed at a plurality of locations on the outer periphery of the nozzle body, and an opening portion of each fuel injection port is constituted by a plurality of close-through linear holes. The fuel injected from the holes forms substantially the same fuel spray, and the holes are connected in a line.
Direction is smaller than 90 ° with respect to the axis of the nozzle body.
A fuel injection nozzle which is inclined at a predetermined angle, and wherein each of the through holes is formed so as to form a different angle with respect to the axis in a vertical plane including the axis of the nozzle body.