Inductive rotary sensors are a type of position sensor used to detect the position and/or speed, for example, of a rotating target. In particular, inductive rotary sensors can be used to detect the position of a gear or another moving element in a mechanical system. They are frequently used in automated control applications, such as automated control applications in automobiles or industrial equipment, for example.
According to aspects of the disclosure, an apparatus is provided, comprising: a transmitting coil; a first receiving coil having a first receiving coil portion and a second receiving coil portion, the first receiving coil portion and the second receiving coil portion being coupled to one another, and the first receiving coil portion and the second receiving coil portion each including N lobes, where N is an integer and N≥1; a second receiving coil having a third receiving coil portion and a fourth receiving coil portion, the third receiving coil portion and the fourth receiving coil portion being coupled to one another, and the third receiving coil portion and the fourth receiving coil portion each including N lobes; wherein the first receiving coil is disposed over the second receiving coil, wherein the transmitting coil is disposed over at least one of the first receiving coil and the second receiving coil, and the transmitting coil has an inner radius that is smaller than an outer radius of the first receiving coil; and wherein, the first receiving coil portion and the third receiving coil portion are arranged to conduct electric current in a first direction, and the second receiving coil portion and the fourth receiving coil portion are arranged to conduct electric current in a second direction that is opposite to the first direction.
According to aspects of the disclosure, a system is disclosed comprising: a transmitting coil; a target having N teeth and N valleys, where N is an integer and N≥1; a first receiving coil having a first receiving coil portion and a second receiving coil portion, the first receiving coil portion and the second receiving coil portion being coupled to one another, and the first receiving coil portion and the second receiving coil portion each including N lobes; a second receiving coil that is disposed over the first receiving coil, the second receiving coil having a third coil portion and a fourth coil portion, the third coil portion and the fourth coil portion being coupled to one another, and the third coil portion and the fourth coil portion each including N lobes; and wherein the transmitting coil is arranged to emit a first magnetic field towards the target and the transmitting coil has an inner radius that is smaller than an outer radius of the first receiving coil, wherein the first receiving coil and the second receiving coil are arranged to sense a second magnetic field that is emitted by the target in response to the first magnetic field, wherein the first receiving coil portion has a shape that is at least in part defined by the equation of:
where R1(θ) is a respective polar coordinate of any point in the first receiving coil portion, Rin is an inner radius of the first receiving coil, and Rout is the outer radius of the first receiving coil, and wherein the second receiving coil portion has a shape that is at least in part defined by the equation of:
where R2(θ) is a respective polar coordinate of any point in the second receiving coil portion, and ϕ is a rotational offset of the first receiving coil portion relative to the second receiving coil portion.
The foregoing features may be more fully understood from the following description of the drawings in which:
As illustrated in
By way of example, in some implementations, such as that shown in
By way of example, in some implementations, the shape of the receiving coil 100 may be represented by Equations 1 and 2 below. More particularly, Equation 1 may define, at least in part, the shape of the first coil portion 110, and Equation 2 may define, at least in part, the shape of the second coil portion 120.
where R110(θ) is any point on the first coil portion 110, R120(θ) is any point on the first coil portion 120, N is a constant that is equal to the number of lobes in each of the coil portions 110 and 120, and ϕ is the rotational offset between the first coil portion 110 and the second coil portion. According to the present example, the rotational offset ϕ may be greater than 0 degrees and less than 360 degrees. In some implementations, the rotational offset ϕ of the receiving coil 100 may be equal to half of the period
of the first and second coil portions. According to the present example, N (i.e., the number of lobes) is equal to four (4). However, it will be understood that N any positive integer that is greater than or equal to 1. In this regard, it will be understood that the present disclosure is not limited to any specific number of lobes being present in each of the first coil portion 110 and the second coil portion 120.
In some respects, imparting a sinusoidal shape of the first coil portion 110 and the second coil portion 120, and rotating the second coil portion 120 relative to the first coil portion 110 may help increase the sinusoidal response in the receiving signals of the receiving coil 100. Furthermore, causing electric current to run in the clockwise direction in one of the coil portions 110 and 120 and the counterclockwise direction in the other one of the coil portions 110 and 120 may cause the net magnetic flux of the receiving coil 100 (absent any magnetic fields from a target) to be equal to zero thus preventing any direct coupling between the receiving coil 100 and a transmitting coil (e.g., transmitting coil 200 shown in
In some implementations, the target 300, the transmitting coil 200, the receiving coil 100-1, and the receiving coil 100-2 may each be centered with one another, and the receiving coil 100-2 may be rotated relative to the receiving coil 100-1 by an angle ρ. According to the example of
By way of example, in one possible implementation, the target 300, the transmitting coil 200, the receiving coil 100-1, and the receiving coil 100-2 may be dimensioned as indicated by Table 1 below.
According to the example of
According to the example of
In some implementations, the number of teeth in the target of the system 400 may be equal to the number of lobes in each coil portion of the receiving coils of the system 400. In general, the magnetic field generated by the eddy current on the target teeth will induce a signal that is dependent on the magnetic flux. Moreover, the magnetic flux through each of the receiving coils 110-1 and 110-2 is dependent on the overlapping between the teeth of the target of the sensing element 410 and the lobes of each of the receiving coils 100-1 and 100-2. As noted above, each receiving coil is composed of a first coil portion (e.g., a clockwise coil portion that is the same or similar to the coil portion 110, discussed above with respect to
The sensing element 410 may be used to measure the rotational displacement and/or speed of the target 300. In some implementations, the sensing element 410 may be part of a sensor 600, which is discussed further below with respect to
Vc=K1 cos(θel)*sin(2πfrt) (3)
Vs=K2 sin(θel)*sin(2πfrt) (4)
where, K1 is a coupling coefficient associated with the receiving coil 100-1, K2, is a coupling coefficient of the receiving coil 100-2, θel is the electrical angle of the target 300 in the target's electrical period, fr is the resonant frequency of the LC tank 610, and t is time. According to the present disclosure, the electrical angle of the target 300 indicates the angular position of the target 300 in its electrical period. The coupling coefficient K1 indicates the proportion of the flux of the reflected magnetic field 614, which is sensed by the receiving coil 100-1. And the coupling coefficient K2 indicates the proportion of the magnetic flux of the reflected magnetic field 614 that is sensed by the receiving coil 100-2. In other words, the coupling coefficients may indicate the proportion of energy transmitted by the target 300 that is received by the receiving coil 100-1 and 100-2, respectively.
As is discussed further below, the signal Vc can be demodulated to produce a signal Vc_demod, and the signal Vs can be demodulated to produce a signal Vs_demod. Signals Vs_demod and Vc_demod may be described by Equations 5 and 6:
Vc_demod=cos(θel) (5)
Vs_demod=sin(θel) (6)
The electrical angle of the target 300 may be based on the mechanical angle of the target 300 (with respect to the sensor 600) and the number of lobes in each portion of the receiving coils 100-1 and 100-2. The relationship between the electrical angle of the target 300 and the mechanical angle of the target 300 can be described by Equation 7 below:
θel=N*θmech (7)
where N is the number of turns in each coil portion of the receiving coils 100-1 and 100-2 and θmech is the mechanical angle of the target 300. According to the present disclosure, the mechanical angle of the target 300 indicates the orientation of the axis B-B of the target 300 relative to the sensor 600 and/or the sensing element 400. According to the example of
Although in the example of
Additionally or alternatively, in some implementations, the interface circuit 820 may calculate internally the angle θel and reconstruct the signals to be sent in output, (i.e., Vc_demod and Vs_demod) from this calculated angle. In this regard, the interface circuit 820 may generate a constant signal amplitude based on the different peaks of the signals Vc and Vs, thus losing the amplitude variation of different peaks in input, and transmitting a reference position through a pulse. The interface circuit may also shift the demodulated signals by adding or subtracting a programmable reference angle.
The electrical angle θel of the target 300 may be used by the ECU 830 to determine the speed and/or mechanical angle of the target 300. Based on the speed and/or mechanical angle of the target 300, the ECU 830 may adjust the speed of (or stop) the electric motor 810. It will be understood that the present disclosure is not limited to any specific method for using the speed and/or mechanical angle of the target 300. Although in the example of
The interface circuit 820 may be configured to generate a reference pulse. The reference pulse may be generated based on the signal Vc_demod. The signal Vc_demod may include N peaks in each full rotation (i.e., 360° rotation) of the target 300, wherein N is the number of lobes in each coil portion of the receiving coils 100-1 and 100-2. In each set of N peaks, that are generated during a given full rotation of the target 300, one of the peaks would have a higher amplitude than the rest (e.g., peak 702B, which is shown in
The interface circuit 820 may provide each reference pulse Pref to the ECU 830. In some implementations, the interface circuit 820 may output each reference pulse Pref over line 834, which is also used by the interface circuit 820 to receive power from the ECU 830. In some respects, outputting each reference pulse Pref over the line 834 is advantageous because it permits the use of the same wiring harnesses (or other wiring interfaces) that are used by older-generation interface circuits. In other words, outputting the pulses Pref over the line 834 allows for backward compatibility between the wiring interface (and/or wiring harness) of the interface circuit 820 and the wiring interfaces of electronic circuitry that is used in conjunction with older-generation interface circuits, which lack the capability of generating a reference pulse.
In some implementations, each reference pulse Pref may have an amplitude of 10 mA and a width of 10 us. However, it will be understood that the present disclosure is not limited to any specific amplitude or width for the reference pulses Pref. For example, in some implementations, the width and/or amplitude of each reference pulse Pref may be programmable. Furthermore, in high-speed applications, each reference pulse Pref can be replaced by a signal pattern (e.g., a sine or a sawtooth pattern) that is transmitted over one full revolution of the target 300. As can be readily appreciated, the signal pattern may be transmitted once in each set of M consecutive revolutions of the target 300, where M is an integer greater than 1.
The ECU 830 may use the pulse Pref to determine the mechanical angle θmech of the target 300. As noted above, rotary inductive sensors (such as the sensor 600) may generate several sine/cosine periods per revolution of a target, and they may not allow detecting absolute angle position. One full rotation can be identified by counting the number of sine/cosine periods, but depending on the starting position of the target, the revolution start and end will be different, which makes it difficult to find a reliable reference point for counting the number of sine/cosine periods. Using the reference pulses Pref to determine the mechanical angle θmech of the target 300 is advantageous because the reference pulses Pref can establish a clear reference point for counting the sine/cosine periods in each revolution of the target 300, thereby preventing errors in the electrical angle information from affecting the final calculation of the mechanical angle θmech.
More particularly, the ECU 830 may determine the mechanical angle θmech of the target 300 in accordance with Equation 9 below:
where N is the number of lobes in each of the coil portions of receiving coils 100-1 and 100-2, and k is the number of peaks since the generation of the last pulse Pref. According to the example of
According to the present example, the interface circuit 820 determines (at step 940) the amplitude of a reference peak of the selected signal. As noted above, in some implementations, the reference peak of the selected signal may be the peak having the highest amplitude among all peaks that occur in the selected signal during a particular (full) revolution of the target 300. Although in the present example the reference peak is a positive peak, alternative implementations are possible in which the reference peak is a negative peak (or another type of peak). In such implementations, the reference peak may have the lowest amplitude among all negative peaks that are generated during a particular (full) revolution of the target. In some implementations, the instant value of the signal Vc_demod may match the amplitude of the reference peak (identified at step 950) when the instant value is equal to the amplitude or within a predetermined distance from the amplitude.
According to the present example, the process 900 is executed in the digital domain. In this regard, it will be understood that the process 900 may be performed by processing circuitry that is part of the interface circuit 820. The processing circuitry may include a general-purpose processor, a special-purpose processor, an Application-Specific Integrated Circuit (ASIC), a Field-Programmable Gate Array, and/or any other suitable type of processing circuitry. Furthermore, it will be understood that in some implementations, the process 900 may be performed in the analog domain, by using analog circuitry. In this regard, it will be understood that the present disclosure is not limited to any specific implementation of the interface circuit 820.
In some implementations, when the interface circuit 820 is in the active state 1030, the interface circuit 820 may execute steps 960 and 970 of the process 900. Under the nomenclature of the present disclosure, the sensor 600 may be considered to be activated, when the electric motor 810 starts turning, when the interface circuit 820 is powered on, and/or when any other suitable type of event is detected. As can be readily appreciated, the interface circuit 820 may transition from the inactive state 1010 to the calibration state 1020 when the sensor 600 is powered on or otherwise activated. The interface circuit 820 may transition from the calibration state 1020 to the active state 1030 after the interface circuit 820 has identified the amplitude of a reference peak in a signal of interest. The calibration circuit may transition from the active state 1030 back into the inactive state 1010 when the interface circuit 820 is powered off.
The system may be implemented, at least in part, via a computer program product, (e.g., in a non-transitory machine-readable storage medium such as, for example, a non-transitory computer-readable medium), for execution by, or to control the operation of, data processing apparatus (e.g., a programmable processor, a computer, or multiple computers). Each such program may be implemented in a high-level procedural or object-oriented programming language to work with the rest of the computer-based system. However, the programs may be implemented in assembly, machine language, or Hardware Description Language. The language may be a compiled or an interpreted language, and it may be deployed in any form, including as a stand-alone program or as a module, component, subroutine, or another unit suitable for use in a computing environment. A computer program may be deployed to be executed on one computer or multiple computers at one site or distributed across multiple sites and interconnected by a communication network. A computer program may be stored on a non-transitory machine-readable medium that is readable by a general or special purpose programmable computer for configuring and operating the computer when the non-transitory machine-readable medium is read by the computer to perform the processes described herein. For example, the processes described herein may also be implemented as a non-transitory machine-readable storage medium, configured with a computer program, where upon execution, instructions in the computer program cause the computer to operate in accordance with the processes. A non-transitory machine-readable medium may include but is not limited to a hard drive, compact disc, flash memory, non-volatile memory, volatile memory, magnetic diskette and so forth but does not include a transitory signal per se.
Having described preferred embodiments, which serve to illustrate various concepts, structures and techniques, which are the subject of this patent, it will now become apparent that other embodiments incorporating these concepts, structures and techniques may be used. Accordingly, it is submitted that the scope of the patent should not be limited to the described embodiments but rather should be limited only by the spirit and scope of the following claims.
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