THROTTLE DEVICE FOR CONTROLLING AN AMOUNT OF FUEL TO BE SUPPLIED TO A FUEL INJECTION NOZZLE, AS WELL AS AN INJECTION DEVICE

Abstract

A throttle device for controlling a fuel quantity to be supplied to a fuel injection nozzle includes a control chamber and a supply device for supplying fuel to the control chamber. The supply device includes an inlet throttle having a length selected such that a fuel flowing through the inlet throttle, when in operation, flows through the inlet throttle in a turbulent flow. An injection device including the throttle device is also provided.

Claims

1-9 (canceled)

10. A throttle device for controlling a fuel quantity to be supplied to a fuel injection nozzle, the throttle device comprising: a control chamber for collecting the fuel; and a supply device for supplying the fuel to said control chamber in a main flow direction; said supply device having an inlet throttle for reducing a pressure of the fuel in said main flow direction, said inlet throttle having a length, and said length of said inlet throttle being selected to cause a fuel flowing through said inlet throttle during operation to flow through said inlet throttle in a turbulent flow.

11. The throttle device according to claim 10, wherein said length of said inlet throttle lies in a length range from 0.1 mm to 0.5 mm.

12. The throttle device according to claim 10, wherein said length of said inlet throttle lies in a length range from 0.15 mm to 0.4 mm.

13. The throttle device according to claim 10, wherein said length of said inlet throttle lies in a length range from 0.2 mm to 0.3 mm.

14. The throttle device according to claim 10, wherein said inlet throttle has a diameter being reduced proportionally to a reduction of said length of said inlet throttle.

15. The throttle device according to claim 10, wherein said length of said inlet throttle lies in a length range from 0.4 mm to 0.5 mm and said inlet throttle has a diameter lying in a diameter range from 171 μm to 176.

16. The throttle device according to claim 10, wherein said length of said inlet throttle lies in a length range from 0.2 mm to 0.3 mm and said inlet throttle has a diameter lying in a diameter range from 166 μm to 170 μm.

17. The throttle device according to claim 10, which further comprises a discharge device for discharging the fuel from said control chamber, said discharge device discharging the fuel from said control chamber in a discharge flow direction being opposite to said main flow direction of the fuel in said supply device.

18. The throttle device according to claim 17, wherein: said discharge device has an outlet throttle for reducing a pressure of the fuel in said discharge flow direction; said discharge device has an outflow region disposed upstream of said outlet throttle in said discharge flow direction; said discharge flow direction has an axis in said outflow region; and said outlet throttle has a longitudinal axis being inclined relative to said axis of said discharge flow direction in said outflow region.

19. The throttle device according to claim 18, wherein said longitudinal axis and said axis of said discharge flow direction of the fuel in said outflow region define an angle of inclination therebetween being less than 50°.

20. The throttle device according to claim 18, wherein said longitudinal axis and said axis of said discharge flow direction of the fuel in said outflow region define an angle of inclination therebetween being less than 45°.

21. The throttle device according to claim 10, wherein said inlet throttle is a non-cavitating throttle.

22. The throttle device according to claim 18, wherein said outlet throttle is a cavitating throttle.

23. The throttle device according to claim 18, wherein said inlet throttle is a non-cavitating throttle and said outlet throttle is a cavitating throttle.

24. An injection device for injecting fuel into a combustion chamber, the injection device comprising: a fuel injection nozzle for injecting the fuel into the combustion chamber; and a throttle device according to claim 10 for controlling a fuel quantity to be supplied to said fuel injection nozzle during operation.

25. The injection device according to claim 24, which further comprises: a housing having an upper region and a lower region; said fuel injection nozzle and said throttle device being disposed in said lower region; a discharge device for discharging the fuel from said control chamber, said discharge device having a valve; and an actuator device for actuating said valve of said discharge device, said actuator device having a piezo stack disposed together with said throttle device and said fuel injection nozzle in said lower region of said housing in a direct vicinity of said throttle device, for introducing waste heat from said piezo stack into said throttle device during operation.

Description

[0034] Advantageous embodiments of the invention will be discussed in more detail below on the basis of the appended drawing, in which:

[0035] FIG. 1 shows an injection device for injecting fuel into a combustion chamber;

[0036] FIG. 2 shows a throttle device which is arranged in the injection device in FIG. 1 and which has an inlet throttle and an outlet throttle; and

[0037] FIG. 3 shows the outlet throttle from FIG. 2 in a non-inclined state and in an inclined state.

[0038] FIG. 1 shows an injection device 10 by way of which fuel 12 can be injected into a combustion chamber (not shown). The injection device 10 has a fuel injection nozzle 14 with a valve needle 34, a throttle device 16 with a supply device 18 and with a discharge device 22, and an actuator device 26 with a piezo stack 32. All of said elements of the injection device 10 are arranged in a housing 30, wherein the housing 30 has an upper region 38 and a lower region 40. Here, the actuator device 26, the throttle device 16 and the fuel injection nozzle 14 are arranged together in the lower region 40. Here, the actuator device 26 with the piezo stack 32 is situated in the immediate vicinity of the throttle device 16, such that working heat from the piezo stack 32 can be introduced directly into the throttle device 16.

[0039] To be able to counteract negative effects of said introduction of heat, the throttle device 16 is formed with a special geometry.

[0040] FIG. 2 shows a detailed view of the throttle device 16. The throttle device 16 has a control chamber 20 in which pressurized fuel 12 is stored in order, by way of said pressure, to hold the fuel injection nozzle 14 closed along a force direction 42. The fuel 12 is supplied to the control chamber 20 via a supply device 18 and is discharged from the control chamber 20 via a discharge device 22. The pressure prevailing in the control chamber 20 should, where possible, remain constant in a desired range.

[0041] The supply device 18 has an inlet throttle 44. The fuel 12 flows through the supply device 18 and thus also through the inlet throttle 44 in a main flow direction 46 into the control chamber 20. Via the inlet throttle 44, the pressure in the fuel 12 is lowered from for example 2000 bar to for example approximately 1800 bar. A length L.sub.Z of the inlet throttle 14 is selected such that as high a Reynolds number as possible is obtained and thus a turbulent flow 48 can be realized. In a turbulent flow 48, the throughflow coefficient, which directly influences the mass flow of the fuel 12, is independent of temperature, such that an increased supply of fuel 12 into the control chamber 20 as a result of a temperature increase—for example as a result of a discharge of working heat from the adjacent piezo stack 32—can be avoided. For example, the inlet throttle 44 has a length L.sub.Z in a length range from 0.1 mm to 0.5 mm.

[0042] In the case of a short length L.sub.Z, the mass flow of the fuel 12 increases slightly, such that it is advantageous for a diameter D.sub.Z of the inlet throttle 44 to also be adapted.

[0043] For example, if the length L.sub.Z lies in a range from 0.4 mm to 0.5 mm, a diameter D.sub.Z in a range from 171 μm to 176 μm is expedient. In a further example, the length L.sub.Z may also lie in a range from 0.2 mm to 0.3 mm, wherein, in this case, a diameter D.sub.Z in a range from 161 μm to 170 μm is expedient.

[0044] As can also be seen in FIG. 2, at the control chamber 20, there is arranged a discharge device 22 through which fuel 12 can be discharged from the control chamber 20. The discharge device 22 is in this case arranged at the same face side 52 of the control chamber 20 as the supply device 18. In this way, the fuel 12 is discharged out of the control chamber 20 in a discharge flow direction 54 which is opposite to the main flow direction 76.

[0045] The discharge device 22 also has a throttle in the form of an outlet throttle 56. By way of said throttle, the pressure in the fuel 12 can be reduced along the discharge flow direction 54, for example from approximately 1600 bar upstream of the outlet throttle 56 to approximately 80 bar downstream of the outlet throttle 56.

[0046] Adjacent to the outlet throttle 56, the discharge device 22 has, arranged at the control chamber 20, an outflow region 58 which the fuel 12 flowing out of the control chamber 20 firstly enters before reaching the outlet throttle 56.

[0047] The pressure in the control chamber 20 is defined by the throttle ratio of the inlet throttle 44 and outlet throttle 56, and is thus directly dependent on the respective throughflow coefficients of the two throttles 44, 56. The throughflow coefficients are now influenced in order to prevent the pressure in the control chamber 20 from building up to such an extent that the fuel injection nozzle 14 can no longer open correctly.

[0048] It can be seen in FIG. 3 that the outlet throttle 56 may exist in two alternative embodiments.

[0049] Here, the left-hand illustration shows an outlet throttle 56 which is arranged rectilinearly along the discharge flow direction 54. This means that a longitudinal axis 12 of the outlet throttle 56 runs coaxially with respect to an axis 60 of the discharge flow direction 54 in the outflow region 58.

[0050] However, in an alternative exemplary embodiment, the outlet throttle 56 is arranged at the outflow region 58 in inclined fashion, that is to say the longitudinal axis 62 runs so as to be inclined with respect to the axis 60 of the discharge flow direction 54 in the outflow region 58. Here, an angle of inclination a is advantageously less than 50° and more advantageously less than 45°. In this way, despite the preferred inclination of the outlet throttle 56, it is furthermore the case that a small structural space may be adequate for the arrangement of the throttle device 16.

[0051] The effect of the inclination of the outlet throttle 56 is illustrated in FIG. 3.

[0052] The outlet throttle 56 is operated as a cavitating throttle 64, by contrast to the inlet throttle 44, which is operated as a non-cavitating throttle 60. Here, “cavitating” means that a gas cushion 70 forms at a wall region 68 of the outlet throttle 56. In a non-inclined outlet throttle 56, shown in the left-hand image in FIG. 3, cross-sectional view B-B, the gas cushion 70 is situated in encircling fashion over the entire wall region 68 of the outlet throttle 56.

[0053] The encircling gas cushion 70 prevents friction effects between the fuel 12 and the wall region 68 of the outlet throttle 56. In this way, the viscosity dependency of the mass flow is reduced or eliminated entirely.

[0054] and the mass flow which flows out of the outlet throttle 56 remains constant even in the event of a temperature increase.

[0055] Now, if the outlet throttle 56 is arranged in inclined fashion, as shown in the cross-sectional view A-A in the right-hand image of FIG. 3, the gas cushion 70 moves to a first subregion 72 of the wall region 68, whereas a second subregion 74 of the wall region 68 is now in direct contact with the fuel 12. In this way, friction effects arise in the outlet throttle 56, and in said region, the mass flow through the outlet throttle 56 is now temperature-dependent. This means that, in the presence of elevated temperature, a greater fuel quantity will also emerge from the outlet throttle 56.

[0056] Altogether, simply through the provision of a predefined length L.sub.Z of the inlet throttle 44, a mass flow difference in an upward direction which is undesired in the event of a temperature increase can be avoided, such that, even in the case of a constant mass flow flowing out at the outlet throttle 56, an undesired pressure increase in the control chamber 20 can be prevented.

[0057] Said effect can additionally be assisted if the outlet throttle 56 is arranged in inclined fashion and, in said region, the previously temperature-independent mass flow then becomes at least partially temperature-dependent, and thus more fuel 12 flows out of the outlet throttle 56 in the presence of elevated temperature than at low temperatures.

[0058] Both geometrical measures—short inlet throttle 44 and inclined outlet throttle 56—therefore contribute individually, but also in combination, to keeping the pressure in the control chamber 20 substantially constant even in the event of a temperature increase, in order to thereby make it possible for the fuel injection nozzle 14 to continue to open as desired.

[0059] Altogether, the throttle ratio of inlet throttle 44 and outlet throttle 56 remains constant over large temperature ranges, such that the pressure in the control chamber can be kept constant.

LIST OF REFERENCE DESIGNATIONS

[0060] 10 Injection device [0061] 12 Fuel [0062] 14 Fuel injection nozzle [0063] 16 Throttle device [0064] 18 Supply device [0065] 20 Control chamber [0066] 22 Discharge device [0067] 24 Valve [0068] 26 Actuator device [0069] 28 Connector element [0070] 30 Housing [0071] 32 Piezo stack [0072] 34 Valve needle [0073] 36 Injection opening [0074] 38 Upper region [0075] 40 Lower region [0076] 42 Force direction [0077] 44 Inlet throttle [0078] 46 Main flow direction [0079] 48 Turbulent flow [0080] 50 Laminar flow [0081] 52 Face side [0082] 54 Discharge flow direction [0083] 56 Outlet throttle [0084] 58 Outflow region [0085] 60 Axis of discharge flow direction in outflow region [0086] 62 Longitudinal axis [0087] 64 Cavitating throttle [0088] 66 Non-cavitating throttle [0089] 68 Wall region [0090] 70 Gas cushion [0091] 72 First subregion [0092] 74 Second subregion [0093] L.sub.Z Length of inlet throttle [0094] D.sub.Z Diameter of inlet throttle [0095] α Angle of inclination