This is a national stage application filed under 35 U.S.C 371 based on International Application No. PCT/FI2004/000006 filed Jan. 9, 2004, and claims priority under 35 U.S.C 119 of Finnish Patent Application No. 20030054 filed Jan. 15, 2003.
The present invention relates to an arrangement in a fuel injection apparatus.
Common rail injection systems utilizing pressure accumulators are currently commonly used in connection with piston engines. In such systems the fuel stored in injection pressure in the so-called pressure accumulator is injected into the combustion chamber of the engine by controlling the injector valve.
Generally, a flow fuse is used as a safety means in injection systems. The flow fuse is usually arranged between the pressure accumulator and the injection valve. The flow fuse closes the flow path from the accumulator in case of a leak and in case the injection valve is stuck, for example, in the open position, in which case there's a situation when fuel can uncontrollably leak into the cylinder combustion chamber. To avoid this situation, U.S. Pat. No. 3,780,716 and WO 95/17594 disclose a flow fuse restricting the fuel flow volume. Typically the flow fuse includes a cylinder space that further includes a piston apparatus having a spring load acting against the fuel flow direction during injection. During normal action the fuel volume needed for each injection corresponds with the volume displaced by the piston. If, for some reason, the injection valve starts to leak, the piston will move to its other limit position, where it will close the flow.
In a typical common rail system the injection pressure reaches a high pressure level almost instantaneously when the needle of the injector nozzle opens. As a result of this, the fuel mass flow is great right at the beginning of the injection during injection of fuel into the combustion chamber. In such a case the pressure in the combustion chamber can increase too fast for reaching optimum performance.
An aim of the present invention is to produce an arrangement in the fuel injection apparatus minimizing the problems associated with prior art. It is an especial aim of the invention to produce an arrangement for restricting the fuel mass flow in the beginning of the injection phase.
According to the invention, an arrangement in the fuel injection system for controlling the fuel injection comprises a body part with a space arranged therein, through which space the fuel to be injected flows during operation, the space further having an inlet and an outlet opening therein. The arrangement further comprises a piston means, arranged movably in the space and having a channel or the like for creating a flow connection between the fuel inlet and the fuel outlet openings. In this arrangement the piston means can divide the space into the first part, being in connection with the inlet opening, and the second part, being in connection with the outlet opening. The arrangement further comprises a spring or the like for creating a force acting on the piston means in a direction opposite to the main direction of fuel flow. The main characterizing feature of the arrangement is that as the piston means is in the end adjacent the inlet opening or near it, the piston means and the body part delimit at least one third part of the space, the volume of which is dependent on the mutual positions of the piston means and the body part.
Preferably the piston means and the space are cylindrically formed and together they form at least two separate sliding surfaces, formed at different distances in relation to the central axis of the piston means and the space. In the arrangement, the third part of the space and its condition can be defined by means of these sliding surfaces in a preferred way. In the arrangement, when the piston means is in the end adjacent the inlet opening, the volume of the third part of the space is at its smallest, and as the piston means retracts to a certain distance from the end adjacent the inlet opening, the volume of the third space increases and as the piston means retracts beyond the said certain distance, the third and the first parts of the space are combined. The third space part is in continuous flow connection with the fuel inlet opening and/or the first space part. The flow connection is achieved by means of a throttling channel or the like.
The space is preferably cylindrical and it comprises at least two portions having a different diameter, of which portions the one having the smaller diameter is located at the end adjacent the inlet opening. The piston means correspondingly includes two portions having different diameters, with the portion having the smaller diameter being located in the end adjacent the inlet opening and both the longitudinal length of the section of the piston means having the smaller diameter and the longitudinal length of the portion of the space having the smaller diameter are shorter than the length of the stroke of the piston means.
As the piston means is located in the end adjacent the outlet opening, the piston means joins to the body part so as to close the flow path to the inlet opening. Because of this, the arrangement according to the invention also functions as a so-called flow fuse.
The arrangement according to the invention allows limiting the mass flow of the fuel injected in the beginning of the injection while allowing a sufficient injection pressure during the actual injection. Further, the arrangement according to the invention also preferably produces a fuel flow fuse.
In the following the invention is described by way of example and with reference to the appended schematic drawings, of which
The space 6 and the piston means 9 are cylindrical. The piston means 9 comprises a portion 9.2 having a larger diameter, the diameter PD2 of which corresponds with the diameter CD2 of the portion 5.2 of the space. Both the space 6 and the piston means 9 comprise portions 5.1, 9.1, the diameters of which are smaller. The diameter of the portion 9.1 of the piston means having the smaller diameter is marked with reference PD1. The diameter of the portion 5.1 of the body part having the smaller diameter is marked with reference CD1.
In the arrangement the piston means 9 and the space 6 are formed so that when the piston means is in the end adjacent the fuel inlet opening 7 they delimit at least a third space 6.3, the volume of which depends on the mutual positions of the piston means 9 and the body part 5. In this case, the position of the piston means can also be determined to be at the end adjacent the first part 6.1 of the space. Firstly, the space 6 comprises at least two portions 5.1, 5.2 having two different diameters CD1, CD2, the portion 5.1 having the smaller diameter CD1 being in the end adjacent the part 6.1 of the first space and additionally the piston means 9 correspondingly comprises two portions 9.1, 9.2 having two different diameters PD1, PD2, the portion 9.1 having the smaller diameter PD1 being located in the end adjacent the first part 6.1 of the space. Now, the longitudinal length L2 of the smaller portion 9.1 of the piston means and the longitudinal length L1 of the part 5.1 of space 6 having the smaller diameter are both separately shorter than the length L3 of the stroke of the piston means 9. Thus, when the portions of the space 6 and the piston means 9 having the smaller diameter are one inside the other, a third part 6.3 of the space 6 is formed by the places where the diameters change. The piston means 9 and the space 6 are cylindrically formed and together they form, by means of their construction and shape, at least two separate sliding surfaces 17, 17′, 18, formed at different distances in relation to the central axis of the piston means and the space. When the piston means retracts from the end adjacent the inlet opening 7 for a certain distance L1 the sliding surface 17, 17′ ceases to exist and the third part 6.3 of the space and the first part 6.1 of the space are combined. The effect this has on the operation of the arrangement is described in the following.
When the piston means 9 is in the initial position, as shown in
The forces mainly determining the movement of the piston means are formed by the pressures prevailing at various parts of the space, and the force of the spring. In other words, the spring force and the force determined by the pressure in the second part 6.2 of the space and the diameter PD2 of the piston means act against the direction of the fuel flow and the forces acting in the direction opposite these forces are the force determined by the pressure in the first part 6.1 of the space and the diameter DP1 of the piston means and the force determined by the pressure in the third part 6.3 and the difference of the diameters DP2−DP1 of the piston means, in a way known as such. As the injection proceeds, the piston means continues its movement while the third part 6.3 of the space increases and the pressure in this volume tends to decrease. The pressure is however equalized by the fuel flow through the flow channels formed by bores 12, 13. Channel 13 is formed as a throttling channel having a relatively small diameter, and it thus allows controlling the speed of pressure equalization between the third part 6.3 and the first part 6.1 of the space. Generally, the factors having an effect on this are flow resistance properties of the flow channel 12, 13. As the above-mentioned equalization of pressure differences slows the movement of the piston means 9, pressure in the second part 6.2 of the space 6 as well as in the outlet opening 8 is in this situation smaller than in the inlet opening 7. Thus, the mass flow of the injected fuel is smaller as well.
The above-mentioned procedure can be illustrated by the equilibrium equation of the forces acting on the piston means.
Pfirst part 6.1·A1+Pthird part 6.3·A3=Psecond part 6.2·A2+spring force
With equilibrium in the equation, the pressure pthird part 6.3 must decrease, as the pressure psecond part 6.2 decreases when the injection nozzle opens. In this situation the areas remain the same and the spring force does not change considerably, either. The pressure level in the third part 6.3 of the space can be controlled by choosing suitable diameters for the various portions 5.1, 5.2, 9.1, 9.2 of the piston means and the space as well as by dimensioning of the flow channel 12, 13.
In
During normal operation the piston means does not reach the position shown in
The invention is not limited to the embodiments described here, but a number of modifications thereof can be conceived of within the scope of the appended claims.
Number | Date | Country | Kind |
---|---|---|---|
20030054 | Jan 2003 | FI | national |
Filing Document | Filing Date | Country | Kind | 371c Date |
---|---|---|---|---|
PCT/FI2004/000006 | 1/9/2004 | WO | 00 | 8/19/2005 |
Publishing Document | Publishing Date | Country | Kind |
---|---|---|---|
WO2004/063558 | 7/29/2004 | WO | A |
Number | Name | Date | Kind |
---|---|---|---|
3780716 | Fenne | Dec 1973 | A |
5692476 | Egler et al. | Dec 1997 | A |
6357415 | Mori | Mar 2002 | B1 |
6374802 | Boecking | Apr 2002 | B1 |
6848424 | Watanabe | Feb 2005 | B2 |
6953052 | Lehtonen | Oct 2005 | B2 |
7066148 | Nishiwaki | Jun 2006 | B2 |
20060090736 | Nishiwaki et al. | May 2006 | A1 |
Number | Date | Country |
---|---|---|
332451 | Jan 1921 | DE |
196 21 021 | Oct 1997 | DE |
196 40 085 | Apr 1998 | DE |
197 47 092 | Apr 1999 | DE |
102 54 465 | Jun 2003 | DE |
Number | Date | Country | |
---|---|---|---|
20060096578 A1 | May 2006 | US |