OPERATING UNIT FOR VEHICLE

Abstract

The operating unit for a vehicle is provided with a housing with a front face and an operating element which is arranged on the front face of the housing and has an operating surface. The operating element is mounted in a spring-elastic manner. Furthermore, at least one sensor is provided for detecting an actuation movement of the operating element. The operating unit additionally has at least one actuator for the feedback movement of the operating element in the case of an actuation movement of the operating element detected by the sensor as well as an analysis and control unit which is connected to the at least one sensor and to the actuator. The actuator is designed as an armature-type electromagnet with a first stator which has a first excitation coil, and an armature as a drive element. Furthermore, the armature is provided with a measuring coil to which a measuring voltage is applied when the magnetic flux generated by the first excitation coil flows through the armature. The first excitation coil and the measuring coil are connected to the analysis and control unit, and with the analysis and control unit it is possible to apply open-loop and/or closed-loop control to the force with which the armature of the actuator can move towards the first stator and/or the deflection movement of the armature out of its rest position and the return movement of the armature back into its rest position are adapted to be controlled and/or regulated.

Claims

1-2. (canceled)

3. An operating unit for a vehicle component, in particular an infotainment system for operating various vehicle components, having a housing having a front face, an operating element arranged on said front face of said housing, which comprises an operating surface, wherein said operating element is spring-elastically mounted, at least one sensor for detecting an actuation movement of said operating element, at least one actuator for a feedback movement of said operating element in the case of an actuation movement of said operating element detected by said sensor, and an analysis and control unit which is connected to said at least one sensor and said actuator, wherein said actuator is configured as an armature-type electromagnet having a first stator comprising a first excitation coil, and an armature as a drive element, said armature is provided with a measuring coil to which a measuring voltage is applied when a magnetic flux generated by said first excitation coil flows through said armature, and said first excitation coil and said measuring coil are connected to said analysis and control unit, wherein by means of said analysis and control unit the force is adapted to be controlled and/or regulated with the aid of which said armature of said actuator is adapted to be moved towards said first stator and/or with the aid of which the deflection movement of said armature out of its rest position as well as the return movement of said armature into its rest position are adapted to be controlled and/or regulated.

4. The operating unit according to claim 3, wherein the armature-type electromagnet comprises a second stator having a second excitation coil, wherein the two stators are arranged on both sides of the armature, and wherein said second excitation coil is also connected to the analysis and control unit, wherein by means of said analysis and control unit the respective force is adapted to be controlled and/or regulated with the aid of which said armature is adapted to be moved into the respective direction towards the first and/or the second stator and/or the deflection movement of said armature out of its rest position as well as the return movement of said armature into its rest position are adapted to be controlled.

Description

[0036] Hereunder the invention is described in detail on the basis of an exemplary embodiment with reference to the drawings in which:

[0037] FIG. 1 schematically shows a side view of an operating unit for a vehicle component having an operating element configured as a display element and spring-elastic mounting as well as an active haptic feedback for actuating the operating element,

[0038] FIG. 2 shows a diagram of an electromagnet configured as an armature-type magnet having a stator and an armature for basically explaining the electromagnetically relevant properties of such an electromagnet,

[0039] FIG. 3 shows a perspective diagram of the actuator configured as a double electromagnet for the active haptic feedback, and

[0040] FIG. 4 shows a possible circuit configuration of the electromagnet as per FIG. 3.

[0041] In FIG. 1 a schematic side view of an operating unit 10 comprising an operating element 12 is shown. In this exemplary embodiment, the operating element 12 is configured as a display assembly having an operating surface 14 on which a plurality of symbol fields 16 are adapted to be represented. As a rule, the operating element 12 is backlit.

[0042] For executing an actuation movement in a vertical movement direction (see double arrow 18) as well as for confirming such an actuation movement in a lateral direction (see double arrow 20 in FIG. 1) the operating element 12 is elastically mounted at a housing 26 via first springs 22 as well as second springs 24. A sensor 28 can determine that the operating element has moved along the vertical movement axis 18. This is ascertained in an analysis and control unit 30, where-upon the latter controls an actuator 32 configured as an electromagnet which comprises a drive element 34. The fixed stator portion 36 of the actuator 32 is supported on the housing 26 while the drive element 34 of the actuator 32 is mechanically coupled with the operating element 12. The effective movement axis of the drive element 34 is shown by the double arrow 38.

[0043] The larger and more complex the design of the operating element 12, the heavier it is and the more installation space it occupies. If it is required that the haptic feedback is the same across the overall operating surface 14, the operating element 12 should exclusively execute a translatory movement for the haptic feedback. Theoretically, this can be realized in a very simple manner in that the drive element 34 of the actuator 32 engages in the center of gravity 40 of the operating element 12. However, the given installation space does not allow for this.

[0044] If it is still intended that the operating element 12 exclusively executes a translatory movement for the haptic feedback, a comparatively simple design solution is to arrange the actuator 32 such that the center of gravity 40 of the operating element 12 lies on the effective movement axis 38 of the drive element 34 of the actuator 32. This is shown in FIG. 1, wherein FIG. 1 also illustrates how the operating element 12 actively moves when an actuation movement is recognized and the actuation of the operating element 12 is confirmed by a haptic feedback. It should be noted here that the second spring elements 24 and/or their effective spring axes 42 ideally lie in a plane in which the center of gravity 40 is also located and in which the effective movement axis 38 of the actuator 32 lies, wherein the effective axes of the actuator 32 and the second springs 24 lie on a common line or extend in parallel to the effective axis 38 of the actuator 32 (in FIG. 1 this is indicated by the dashed double arrows 42).

[0045] Essentially orthogonally to this plane 44 extends that plane that is spanned by the lateral movement axis 20 of the operating element 12 and the effective movement axis 38 of the drive element 34 of the actuator 32. With reference to FIG. 1 this plane is the drawing plane.

[0046] The purely translatory movement of the operating element 12 for the haptic feedback thus comprises both a lateral and a vertical component. The fact that this feedback movement is not purely lateral is of no importance regarding the fact that the haptic sensation is to be the same across the overall operating surface 14 of the operating element 12. It is crucial that the operating element 12 does not execute any rotatory movement for the haptic feedback, that is that there is a parallel displacement of the operating element 12 in the space.

[0047] As has already been described above, in particular for installation space and cost reasons an electromagnet is often used as an actuator for the haptic feedback of operating elements. The force applied by this electromagnet can be estimated only at an increased effort and essentially depends on the current and the air gap of the electromagnet. The applicable conditions in the case of an electromagnet are hereinafter elucidated on the basis of FIG. 2.

[0048] In FIG. 2 an electromagnet is illustrated whose stator and armature are made of highly permeable materials (usually machining steel or electrical sheet) and whose magnetic field is built up by means of an energized excitation coil.

[0049] The force of such an electromagnet is usually calculated from the excitation current and the size of the air gap. The force progression in the case of the haptic feedback is however very dynamic with frequency components above 1 kHz. Here, the connection between current and force in the case of the normally used machining steels or electrical sheets for guiding the magnetic flux is not trivial and can only be described by a very complex modeling. In addition, the air gap is not exactly known due to the mechanical tolerances and the movement of the operating surface and therefore the force action of the actuator can only be roughly estimated. By the use of the Maxwell tensile strength formula and a measuring coil for determining the magnetic flux density in the air gap this problem can be avoided, wherein, as a rule, a voltage measurement is more inexpensive than a current measurement:

[00001]$F=\frac{B_L^2.Math.A_L}{2.Math..Math.{?}_0}$

(Factuator force, ?.sub.0permeability of the air, A.sub.Lair gap surface, B.sub.Lmagnetic flux density in the air gap)

[0050] The relatively low inhomogeneity of the air gap flux density in practical applications can be accounted for by a correction factor, which, in turn, leads to a simple realization of a force measurement by means of a measuring coil:

[00002]$F?\left(t\right)=\frac{C}{{?}_0.Math.A_L}.Math.{\left(\frac{1}{N_{\mathrm{MS}}}.Math.{?}_0^t.Math.u?\left(t^{}\right).Math.{\mathrm{dt}}^{}\right)}^2$

(ttime, Cair gap correction factor, N.sub.MSnumber of windings of the measuring coil, u(t)induced voltage in the measuring coil)

[0051] The integration of the induced voltage can be digitally carried out with a microcontroller which normally exists in the system. Thus the force is known at any time during the control process.

[0052] FIG. 3 shows a perspective view of the actuator 32. This actuator 32 is configured as a double electromagnet whose drive element 34 serving as an armature 46, which is arranged between a first stator 48 and a second stator 50, can build up a force in two opposite directions along the effective movement axis 38.

[0053] The first and the second stator 48, 50 are fastened to the housing 26, while the armature 46 is fixedly connected to the operating element 12. The first stator 48 comprises a first excitation coil 52, while the second stator 50 is provided with a second excitation coil 54. The armature 46 is surrounded by a measuring coil 56. On both sides of the armature 46 a first and a second air gap 58, 60 are respectively located. Since the force acting upon the armature 46 is respectively to be directed in one direction the excitation coils 52, 54 are not energized simultaneously but alternately. The arrangement of the measuring coil 56 at the armature 46 allows for an exact and inexpensive force measurement in both effective directions along the effective movement axis 38.

[0054] As an example, the control and the analysis of the voltage induced in the measuring coil 56 may be carried out by means of a microcontroller 62 which may form part of the analysis and control unit 30. An example of a circuit configuration including the microcontroller 62 is shown in FIG. 4. The induced voltage in the measuring coil 56 is at first smoothed by a simple low pass 64 to eliminate from the measured signal the PWM clocking (frequency normally >20 kHz) for alternately controlling the two excitation coils 52, 54. Thereafter the microcontroller 62 detects the induced voltage and digitally integrates it. The limiting frequency of the low pass 64 should be sufficiently higher than the highest frequency components of the force progression.

LIST OF REFERENCE NUMERALS

[0055] 10 Operating unit [0056] 12 Operating element [0057] 14 Operating surface of the operating element [0058] 16 Symbol fields [0059] 18 Vertical movement axis of the operating element [0060] 20 Lateral movement axis of the operating element [0061] 22 Spring elements [0062] 24 Spring elements [0063] 26 Housing [0064] 28 Sensor [0065] 30 Control unit [0066] 32 Actuator [0067] 34 Drive element of the actuator [0068] 36 Stator portion of the actuator [0069] 38 Effective movement axis of the actuator [0070] 40 Center of gravity of the operating element [0071] 42 Effective spring axis [0072] 44 Plane [0073] 46 Armature [0074] 48 Stator [0075] 50 Stator [0076] 52 Excitation coil [0077] 54 Excitation coil [0078] 56 Measuring coil [0079] 58 Air gap [0080] 60 Air gap [0081] 62 Microcontroller [0082] 64 Low pass