The present invention relates to a hysteresis brake, especially for an electric camshaft adjuster.
Passive, (drive-free) electric camshaft adjusters which can change the phase position of a camshaft are known from the prior art. An electric camshaft adjuster of this type is described, for example, in German patent document DE 102 47 650 A1 and includes a brake and a lever mechanism. An alternative embodiment of the electric camshaft adjuster with a brake and a summing gear mechanism is described in German patent document DE 103 55 560.
For the electric camshaft adjusters, hysteresis brakes can be used which operate contactlessly and in a manner free from wear. In order to adjust the phase position of the camshaft, knowledge of the angular position of a rotor of the hysteresis brake is required.
In order to measure the angular position of the camshaft or of the hysteresis brake, angle of rotation sensors which are known from the prior art may be used, such as are described, for example, in German patent documents DE 195 31 621 A1 and DE 100 34 927 A1. These angle of rotation sensors require a transmitter element rotating together with a rotor and a fixed sensor unit for producing a measuring signal from which angle and/or rotational speed information is determined. The measurement principle may be optical or magnetic.
It is an object of the present invention to provide a hysteresis brake, especially for an electric camshaft adjuster, which permits simple determination of angle and/or rotational speed information items.
This and other objects and advantages are achieved by the hysteresis brake according to the present invention, a first embodiment of which includes a sensor for enabling a moveable rotor and/or a hysteresis band to receive a secondary magnetic flux caused by a main magnetic flux. An evaluation and control unit evaluates the secondary magnetic flux received and determines angular and/or rotational speed information for a camshaft from detected changes of the secondary magnetic flux.
Alternatively, a second embodiment of the hysteresis brake according to the invention includes a sensor for enabling an excitation coil to receive a main magnetic flux, and an evaluation and control unit which evaluates the main magnetic flux received, detects changes in the main flux and determines angle and/or rotational speed information from the detected changes. The changes in the main flux are caused by changes of the magnetic resistance that are caused by a rotor and/or a hysteresis band. In this alternative embodiment, instead of the changes of the secondary flux, the changes in the main magnetic flux are evaluated to determine the angle and/or rotational speed information.
The embodiments of the hysteresis brake according to the present invention have the advantage that, by using the secondary magnetic flux or the main magnetic flux to determine the angle and rotational speed information, a sensor can be constructed in a simple manner, since separate transmitter elements are not required. The use of components which are required in any case for the function of the hysteresis brake for the angle and/or rotational speed determination makes it possible to reduce the cost for fixing, cabling and contact connection. The components used merely have to be adapted in their configuration to the additional task.
To determine the angle and/or rotational speed, the rotor and/or the hysteresis band of the hysteresis brake may be geometrically designed in such a manner that the magnetic flux through the sensor changes cyclically as the rotor and/or hysteresis band rotates.
In a refinement of the hysteresis brake, the rotor may include a ferromagnetic ring which has a rectangular toothed profile with at least one elevation and/or cut-out and/or one or more apertures.
Additionally or alternatively, the hysteresis band may have at least one rectangular and/or round apertures and/or one or more regions with thinner and/or thicker walls.
The toothed profile and/or the apertures and/or the regions with thinner and/or thicker walls give rise to different values for the magnetic resistance and therefore for the secondary or main magnetic flux detected. This is the case, because with a high magnetic resistance alternate cyclically with regions with a low magnetic resistance. These cyclic changes of the magnetic flux can be detected by a simple sensor and can be evaluated by the evaluation and control unit. The required refinement of the rotor or hysteresis band can be undertaken in a simple manner during production of the components.
In a refinement of the first embodiment of the hysteresis brake, the sensor for receiving the secondary magnetic flux may be integrated in the stator, e.g., in the outer stator part.
The sensor may include at least one sensor coil with a ferromagnetic core, and/or at least one Hall sensor which receive the secondary magnetic flux and pass it on in the form of a voltage signal to the evaluation and control unit.
In a further refinement, the sensor for determining the direction of rotation may include a second sensor coil with a ferromagnetic core, and/or a second Hall sensor which produce a further voltage signal which may be phase-displaced by 90° in relation to the other voltage signal.
The first and second sensor coils produce, for example, voltage signals with different amplitudes which can be transmitted to the evaluation and control unit on a common connecting line. Due to the different amplitudes, the signals can easily be differentiated in the evaluation and control unit, and, in spite of the second sensor coil, the number of lines and contact connections remains the same as in the embodiment with only one sensor coil.
In a refinement of the second embodiment, the sensor for receiving the main magnetic flux may be arranged in the region of the excitation coil.
The sensor for receiving the main magnetic flux may include, for example, at least one sensor coil and/or a Hall sensor.
In a further refinement, the excitation coil carries out the function of the sensor and receives the main magnetic flux which is passed on in the form of a voltage signal to the evaluation and control unit. As a result, the components for determining the angle and/or rotational speed information can be further reduced.
In a further refinement of the hysteresis brake, the evaluation and control unit allows for an operationally induced change of the main magnetic flux, for example when producing a different braking torque, during the determination of the angle and/or rotational speed information in the form of interference signals.
The hysteresis brake according to the present invention may be used, for example, in an electric camshaft adjuster.
Other objects, advantages and novel features of the present invention will become apparent from the following detailed description of the invention when considered in conjunction with the accompanying drawings.
As is apparent from
The functioning of the hysteresis brake according to the present invention is described below with reference to
As is furthermore apparent from
As is apparent from
During rotation of the hysteresis band 4.1, regions with and without an aperture 4.2 are located in an alternating manner between the sensor coil 6.1 and the opposite elevation of the inner stator part 3.1. The magnetic resistance and therefore the secondary magnetic flux 7.1 through the sensor coil 6.1 changes accordingly. If, for example, an aperture 4.2 is located between sensor coil 6.1 and inner stator part 3.1, then, on account of the poor conductivity of air, the magnetic resistance is high and the magnetic flux 7.1 is small. If a region of the hysteresis band 4.1 without an aperture is located between the sensor coil 6.1 and the inner stator part 3.1, then, on account of the better conductivity of the hysteresis material, the magnetic resistance is low and the magnetic flux 7.1 is large. The change of the magnetic flux 7.1 through the sensor coil 6.1 leads, in accordance with the law of induction, to the abovementioned voltage at the sensor coil 6.1.
An optional, second sensor coil 6.2 makes it possible to additionally produce a voltage signal which may be displaced by 90°. As a result, direction of rotation information items can be determined by the evaluation and control unit. In addition, the resolution of the sensor 6 is increased. The arrangement of the second sensor coil 6.2 corresponds to the arrangement of the first sensor coil 6.1 apart from the fact that the second sensor coil 6.2 is arranged in a different depression of the outer stator part 3.2.
The two sensor coils 6.1, 6.2 may have different numbers of turns, as a result of which the amplitudes of the voltages induced differ in accordance with the ratio of the number of turns. The voltage signals of the two sensor coils 6.1, 6.2 can be passed via the same lines to the evaluation and control unit 5, since the latter can differentiate the voltage signals on the basis of their different amplitudes. As a result, in spite of the second sensor coil, the number of lines and contact connections remains the same as in the embodiment with one sensor coil.
Instead of the sensor coil 6.1, 6.2, sensors which directly measure the magnetic flux, such as Hall sensors, may be used.
As is furthermore apparent from
During rotation of the rotor 4, a tooth of the toothed profile 4.3 and a cut-out are located in an alternating manner in front of the sensor coils 6.1, 6.2. The magnetic resistance and therefore the magnetic flux 7.1 through the sensor coils 6.1, 6.2 change accordingly. If an aperture is located in front of the sensor coils 6.1, 6.2, then, on account of the poor conductivity of air, the magnetic resistance is high and the magnetic flux 7.1 is small. If a tooth is located in front of the sensor coils 6.1, 6.2, then, on account of the better conductivity of the ferromagnetic material of the ring 4.3, the magnetic resistance is low and the magnetic flux 7.1 is large.
The magnetic flux 7.1 through the sensor coils 6.1, 6.2 is guided in a secondary magnetic flux 7.1 from the inner stator part 3.1 by the ring 4.3 around the hysteresis band 4.1 and through the sensor coils 6.1, 6.2 to the outer stator part 3.2. The magnetic flux through the sensor coils 6.1, 6.2 is evaluated as in the first exemplary embodiment illustrated in
As is apparent from
In the embodiment according to
As is apparent from
If, for example, an aperture is located between the inner and outer stator part 3.1, 3.2, then, on account of the poor conductivity of air, the magnetic resistance is high and the magnetic flux 7 is small. If a region which does not have apertures is located between the inner and outer stator part 3.1, 3.2, then, on account of the better conductivity of the hysteresis material, the magnetic resistance is low and the magnetic flux 7 is large.
The local change in the magnetic flux leads to a change in the main flux 7. In accordance with the law of induction, the change of the magnetic flux 7 through the sensor coil 6 leads to an induced voltage signal at the sensor coil 6, the temporal sequence of which is processed in the evaluation and control unit 5 to provide angle and rotational speed information.
As is apparent from
As the rotor 4 rotates, an elevation of the ring 4.3 or a cut-out of the ring 4.3 is located in an alternating manner in front of the elevation of the outer stator part 3.2. The magnetic resistance and therefore the magnetic flux through the sensor coil 6 change accordingly.
If a cut-out is located in front of the elevation of the outer stator part 3.2, then, on account of the poor conductivity of air, the magnetic resistance is high and the magnetic flux 7.1 is small. If an elevation of the ring 4.3 is located in front of the elevation of the outer stator part 3.2, then, on account of the better conductivity of the ferromagnetic material, the magnetic resistance is low and the magnetic flux is large.
The secondary magnetic flux 7.1 is then guided in a secondary magnetic flux around the hysteresis band to the opposite stator part. The local change of flux leads, as has already been described, to a change of the main flux 7. The change of the magnetic flux is evaluated, as has already been described, by the evaluation and control unit 5.
The evaluation and control unit 5 allows for an operationally induced change of the main magnetic flux 7 in the hysteresis brake during the determination of the angle and/or rotational speed information items.
The main magnetic flux 7 is changed, for example, if a different braking torque has to be produced in the hysteresis brake. The changing of the main magnetic flux 7 induces an interference voltage signal in the sensor coils 6, 6.1, 6.2 which is superimposed on the measuring signal. Since this interfering influence of the evaluation and control unit 5 is known, the superimposed interference voltage signal can be allowed for in the evaluation of the voltage signal to determine the angle and/or rotational speed information.
Instead of the sensor coils 6, 6.1, 6.2 described, sensors which directly measure the magnetic flux 7, 7.1, such as Hall sensors, may be used.
The hysteresis brake according to the present invention uses the operationally induced main magnetic flux and/or a secondary magnetic flux derived therefrom, and a sensor to determine angle and rotational speed information items. Since separate transmitter elements are not required, the receiver can be constructed in a simple manner. In addition, the cost for fixing, cabling and contact connection can be reduced.
The foregoing disclosure has been set forth merely to illustrate the invention and is not intended to be limiting. Since modifications of the disclosed embodiments incorporating the spirit and substance of the invention may occur to persons skilled in the art, the invention should be construed to include everything within the scope of the appended claims and equivalents thereof.
Number | Date | Country | Kind |
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10 2004 023 392.6 | May 2004 | DE | national |
This application is a national stage of PCT International Application No. PCT/EP2005/004530, filed Apr. 28, 2005, which claims priority under 35 U.S.C. § 119 to German Patent Application No. 10 2004 023 392.6, filed May 12, 2004, the entire disclosures of which are herein expressly incorporated by reference.
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCT/EP05/04530 | 4/28/2005 | WO | 00 | 8/14/2007 |