This application is based on German Patent Application 10 2005 007 543.6 filed Feb. 18, 2005, upon which priority is claimed.
1. Field of the Invention
The invention relates to a fuel injector with direct needle control for an internal combustion engine.
2. Description of the Prior Art
Fuel injectors with a so-called direct needle control are known. Fuel injectors of this kind function properly without a control valve interposed between an electrically triggered actuator and a nozzle needle. The transmission of force between the actuator and the nozzle needle is implemented by means of a hydraulic coupler or hydraulic booster. For these actuators, it is particularly useful to use piezoelectric actuators, which have a direct or inverse triggering, depending on whether or not they are supplied with current in the closed state. With a direct triggering, the piezoelectric actuator is supplied with current in order to open the nozzle needle so that a longitudinal expansion of the piezoelectric actuator, through a pushing motion that is amplified by the booster, triggers an opening of the injection nozzles. In the closed state, the piezoelectric actuator has a shorter longitudinal span. With an inverse triggering, the piezoelectric actuator is supplied with current in the closed state of the nozzle needle so that when the piezoelectric actuator is in its longitudinally expanded state, it holds the nozzle needle closed. When the piezoelectric actuator is triggered to initiate the injection, the power to the piezoelectric actuator is switched off so that a pulling movement of the piezoelectric actuator causes a pressure drop in a control chamber of the hydraulic booster. This hydraulically boosts the stroke motion of the piezoelectric actuator in order to open the nozzle needle.
A fuel injector with direct needle control has already been proposed by patent application DE 10 2004 037 125.3. The fuel injector therein has an actuator booster piston and a nozzle needle booster piston; the actuator booster piston is associated with an actuator coupler chamber and the nozzle needle booster piston is associated with a nozzle needle coupler chamber. Between the actuator coupler chamber and the nozzle needle coupler chamber, a hydraulic throttle restriction is provided that has different flow cross sections for the flow of fuel into and out of the nozzle needle control chamber. A first sliding sleeve for delimiting the actuator coupler chamber is guided axially on the actuator booster piston and another sliding sleeve for delimiting the nozzle needle coupler chamber is guided axially on the nozzle needle booster piston. A compression spring prestresses the sliding sleeves so that they each press with an end surface against a respective sealing surface. The use of sliding sleeves makes it possible to axially decouple the actuator booster piston from the nozzle needle booster piston, permitting the booster pistons to be installed in axially offset positions.
The object of the present invention is to create a fuel injector with two-stage boosting at different boosting ratios.
The object of the invention is attained with the defining characteristics that make it possible to create a compact fuel injector with direct needle control, which functions properly with a small number of moving parts in order to produce the required boosting ratios for a two-stage boosting.
Advantageous modifications of the invention are possible. A two-stage boosting of the actuator stroke with different boosting ratios can be achieved in a particularly suitable fashion if, in a first opening phase of the nozzle needle, the control element is situated in a starting position due to the pressures acting on its control surfaces and if, at the beginning of a second opening phase of the nozzle needle, the changing pressure ratios on the control surfaces of the control element cause the control element to lift away from its starting position so that the volume in the actuator coupler chamber increases, which alters the boosting ratio between the actuator booster piston and the nozzle needle booster piston. The control chamber functions as a pressure reservoir and/or energy storage means so that a pressure threshold is produced in the control chamber in order to initiate the second opening phase. It is particularly advantageous if the control element is provided in the form of a control sleeve that is guided so that it can slide axially on the actuator booster piston and whose first end surface, functioning as a first control surface, is hydraulically coupled to the actuator coupler chamber and whose second end surface, functioning as a second control surface, is associated with the control chamber. In a first opening phase of the nozzle needle, the first end surface is situated in its starting position. In a second opening phase of the nozzle needle, the first end surface lifts away from its starting position so that in the second opening phase of the nozzle needle, the actuator coupler chamber acts on an effective surface comprised of the pressure surface of the booster piston and the first end surface. The actuator booster piston is suitably embodied in the form of a stepped piston having both the first pressure surface and the second pressure surface. Moreover, in a suitable embodiment form of the fuel injector, the coupler chamber associated with the actuator pressure booster piston is hydraulically connected to a nozzle needle coupler chamber associated with the nozzle needle booster piston. A sliding sleeve is guided on the actuator booster piston in order to embody the control chamber and coupler chamber associated with the actuator booster piston.
The invention will be better understood and further objects and advantages thereof will become more apparent from the ensuing detailed description of preferred embodiments, taken in conjunction with the drawings, in which:
The fuel injector shown in
The chamber 18 contains a piezoelectric actuator 20 that acts on a hydraulic booster 30. The hydraulic booster 30 has an actuator booster piston 31 drive-coupled to the piezoelectric actuator 20 and likewise contained in the chamber 18. The actuator booster piston 31 is embodied in the form of a stepped piston that has a first piston section 32 with a diameter d1 and a second piston section 33 with a diameter d2, where d2>d1. The hydraulic booster 30 also has a sliding sleeve 34 guided on the second piston section 33, a control sleeve 35 guided axially between the sliding sleeve 34 and the first piston section 32, an actuator coupler chamber 36, and a control chamber 37. According to
The control sleeve 35 functions as a control element 40 that will be described below generally in connection with
Another compression spring 49 also supported on the actuator booster piston 31 prestresses the sliding sleeve 34. It pushes against the sliding sleeve 34 in
The hydraulic booster 30 also has a nozzle needle booster piston 51 with a diameter d3, which is connected to the nozzle needle 13 and has a nozzle needle pressure surface 52 facing into a nozzle needle coupler chamber 53. The nozzle needle booster piston 51 has an additional sliding sleeve 54 axially guided on it, which a closing spring 56 presses against the nozzle needle surface 24 of the intermediate body 19 so that this additional sliding sleeve 54 delimits the nozzle needle coupler chamber 53. The hydraulic connection 22 connects the nozzle needle coupler chamber 53 to the actuator coupler chamber 36. The hydraulic connection 22 can function as a throttle. The use of sliding sleeves 34 and 54 on the booster pistons 31 and 51 axially decouples the actuator booster piston 31 from the nozzle needle booster piston 51.
When the injection nozzles 16 are closed, the sealing seat 15 of the nozzle needle 13 is closed. The system pressure supplied to the chamber 18 and pressure chamber 25 via the fuel inlet is equally present in all of the pressure chambers. The sliding sleeves 34, 54 and the control sleeve 35 are provided with leakage gaps so that the system pressure is present in the actuator coupler chamber 36, the control chamber 37, and the nozzle needle coupler chamber 53. In this state, the hydraulic booster 30 is pressure-balanced and the piezoelectric actuator 20 is supplied with a voltage that brings the piezoelectric actuator 20 into its loaded state in the vertical direction. The system pressure present in the nozzle needle coupler chamber 53 acts on the nozzle needle booster piston 51 in the closing direction. As a result, in this state of the piezoelectric actuator 20, the sealing seat 15 of the nozzle needle 13 is closed. The nozzle needle is also acted on by the closing spring 56, which keeps the nozzle needle 13 closed in the no-current state.
If the voltage in the piezoelectric actuator 20 is reduced or if the piezoelectric actuator 20 is relaxed by means of a current, then this likewise reduces the length of the piezoelectric actuator 20 in the vertical direction. The piezoelectric actuator 20 is consequently an inversely operated actuator. The actuator booster piston 31, which the compression spring 49 prestresses toward the piezoelectric actuator 20, thus likewise moves in the vertical direction due to the reduced vertical length of the piezoelectric actuator 20. Due to this outwardly directed, pulling movement of the actuator booster piston 31, the pressure surface 38 of the first piston section 32 enlarges the volume in the actuator coupler chamber 36, which results in a pressure reduction therein, which determines an opening pressure for a first opening phase for the opening of the nozzle needle 13. The hydraulic connection 22 transmits the opening pressure into the nozzle needle coupler chamber 53 so that the opening pressure likewise acts on the nozzle needle pressure surface 52. This establishes a first boosting ratio for the opening of the nozzle needle 13, which exists due to the ratio of the surface areas of the pressure surfaces 38 and 52; the boosting ratio of the first opening phase is determined by the surface area ratio d12/d32. At the same time as the pulling movement of the actuator booster piston 31, the second piston section 33 and the upward motion of the second pressure surface 48 facing into the control chamber 37 increase the volume in the control chamber 37, thus decreasing the pressure in the control chamber 37 as well. The control chamber 37 thus functions as a pressure reservoir and an energy storage means in the form of hydraulic spring. As the stroke of the nozzle needle 51 increases, the pressure in the nozzle needle coupler chamber 53 rises again due to the pressure migration at the sealing seat 15 of the nozzle needle 13, while the pressure in the control chamber 37 continues to fall. This leads to conditions that permit the control sleeve 35 to lift away from the actuator surface 23, thus freeing the first end surface 44 of the control sleeve 35, which then functions as a first control surface 47 acting on the actuator coupler chamber 36. The actuator coupler chamber 36 is now radially delimited by the sliding sleeve 34. The actuator coupler chamber 36 consequently acts on an effective pressure surface area composed of the actuator pressure surface 38 of the first piston section 32 and the first end surface 44 of the control sleeve 35. Because the inner diameter of the sliding sleeve 34 is guided against the diameter d2 of the second piston section 33 and the control sleeve 35 is situated between the sliding sleeve 34 and the piston section 32, where the outer diameter of the control sleeve 35 is guided against the inner diameter of the sliding sleeve 34, the combined effective pressure surface area is determined by the outer diameter of the control sleeve 35, which corresponds to the diameter d2. The combined effective pressure surface area produces a jump in the boosting, which acts on the nozzle needle pressure surface 52 of the nozzle needle booster piston 51 in the form of a second boosting ratio. As a result, the stroke of the piezoelectric actuator 20 is transmitted to the nozzle needle 13 with a more powerful boosting that results from the surface area ratio of the combined effective pressure surface areas to the pressure surface 52; the surface area ratio d22/d32 determines the second boosting ratio. As a result, the nozzle needle 13 is moved at a faster speed and for a greater stroke distance.
The boosting ratios for the first opening phase and second opening phase of the nozzle needle 13 will now be explained in greater detail in conjunction with the equivalent hydraulic circuit diagram shown in
Supplying the piezoelectric actuator 20 with current causes the piezoelectric actuator 20 to start elongating again, which is transmitted by the actuator booster piston 31 to the control chamber 37 and the actuator coupler chamber 36. Next, assisted by the compression spring 43, the end surface 44 of the control sleeve 35 is pressed against the surface 23, thus producing the actuator coupler chamber 36 beneath the actuator pressure surface 38. At the same time, the pressure surface 38 of the first piston section 32 increases the pressure in the actuator coupler chamber 36, which the hydraulic connection 22 transmits to the nozzle needle coupler chamber 53; due to the pressure increase in the nozzle needle coupler chamber 53, the nozzle needle booster piston 51 presses the nozzle needle 13 against the sealing seat 15, thus disconnecting the injection nozzles 16 from the pressure chamber 25. At the same time, a pressure-balanced state arises once more in the pressure chambers of the hydraulic booster 30.
The foregoing relates to preferred exemplary embodiments of the invention, it being understood that other variants and embodiments thereof are possible within the spirit and scope of the invention, the latter being defined by the appended claims.
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