Patent Publication Number: US-2023135927-A1

Title: Torque and angle of rotation detection system

Description:
TECHNICAL FIELD 
     The invention relates to a torque and angle of rotation detection system that includes a rotor unit, a stator unit and strain gauges. 
     BACKGROUND OF THE INVENTION 
     Industrial measurement technology serves to detect physical parameters such as a torque, angle of rotation and the like of industrially manufactured products. For example, test stand technology is used for measuring the torque and angle of rotation of rotating components such as internal combustion engines, electric motors, gearboxes, pumps, and the like. In addition, the torque and angle of rotation of rotating components is also measured in chip removing machining of workpieces. 
     A system for detecting torque and angle of rotation known as KiTorq and documented in the data sheet 4550A 000-880d-08.20 is available from the applicant. KiTorq is considered as prior art for the purposes of the present invention. KiTorq features a rotor unit and a stator unit. The rotor unit is designed as a flange which can be attached to any rotating component via a screw connection. The rotor unit is configured for rotational speeds of up to 20000 min- 1 . The stator unit, on the other hand, is stationary. It is separated from the rotor unit with respect to an axis of rotation by a radial air gap. 
     The rotor unit comprises strain gauges. The strain gauges comprise a measuring grid and a bridge circuit. When an electrical voltage is applied to the measuring grid, the measuring grid exhibits an electrical resistance. The electrical resistance changes upon expansion or compression of the measuring grid, which change in electrical resistance generates measurement signals in the bridge circuit. In this way, the strain gauges detect the torque that acts onto the rotor unit. The strain gauges detect the torque in a dynamic manner generating up to 10,000 measurement signals per second with a sampling rate of up to 35 kSample. The measurement signals have a resolution of 24 bit. 
     The rotor unit comprises a plurality of dipole magnets which are spaced apart from each other. The stator unit comprises a magnetic field sensor that measures the magnetic fields of the dipole magnets during rotation of the rotor unit. The system counts the magnetic fields measured, and since the distance between the dipole magnets is known, determines the angle of rotation traveled by the rotor unit therefrom. 
     The rotor unit comprises a rotor antenna and the stator unit comprises a stator antenna for the transmission of the measurement signals from the rotor unit to the stator unit. Transmission of the measurement signals occurs in a contactless manner by the rotor antenna sending the measurement signals to the stator antenna. The transmission frequency of 13.56 MHz in the Industrial Scientific and Medical (ISM) band is used for this purpose, and a data transmission rate of up to 1.4 Mbitsec -1  is achieved. 
     For the operation of the strain gauges and the rotor antenna, the rotor unit must be supplied with electrical power. The stator unit comprises a primary coil, and the rotor unit comprises a secondary coil for this purpose. The primary and secondary coils are inductively coupled to one another. A primary electrical voltage in the primary coil generates a secondary electrical voltage in the secondary coil. Inductive coupling of the primary and secondary coils occurs in a contactless manner in the ISM band with carrier frequencies in the range of 115 kHz to 130 kHz. 
     The dipole magnets consist of a magnetized mixture of ferrite powder/rubber. With less than 200 mT, the remanence of the dipole magnets is relatively weak. A remanence being that weak is easily disturbed by external magnetic fields which may, thus, falsify the determination of the angle of rotation. 
     To achieve inductive coupling, the secondary coil comprises an iron powder/resin mixture. The iron powder/resin mixture can be mixed quickly and applied easily to the rotor unit in a curved shape using a spatula where it rapidly hardens. In particular, the same iron powder/resin mixture may be used for rotor units having different radii of curvature. Thus, the use of the iron powder/resin mixture leads to cost-effective production with high variability. However, the freshly mixed iron powder/resin mixture contains air inclusions, which persist even until after the iron powder/resin mixture has cured and result in a low magnetic permeability. As a consequence, the inductive coupling between the primary coil and the secondary coil has a low efficiency. 
     For the reasons mentioned above, the dipole magnets and the magnetic field sensor as well as the primary and secondary coils must be arranged in close proximity to each other. The radial air gap between the stator unit and the rotor unit is only 1.0 mm in width and must comply with a tight tolerance range for the radial air gap of +/-0.5 mm. To comply with this narrow tolerance range for the radial air gap, the rotor unit is manufactured with a balance quality grade of G 2.5 according to DIN ISO 1940-1, which, however, makes the production of KiTorq complex and expensive. 
     In many cases, after the rotor unit has been attached to a rotating component, there is not enough space in the vicinity of the rotating component for mounting the stator unit adjacent to the rotor unit to arrange the magnetic field sensor in close proximity to the dipole magnets. However, the greater the distance between the magnetic field sensor and the dipole magnets is, then the more error-prone is the measurement of the magnetic fields of the dipole magnets by the magnetic field sensor so that the determination of the angle of rotation may be falsified. 
     OBJECTS AND SUMMARY OF THE INVENTION 
     It is a first object of the present invention to provide a torque and angle of rotation detection system comprising a rotor unit and a stator unit that are separated from one another by a radial air gap with respect to an axis of rotation. The air gap desirably is wider than that known from the prior art according to KiTorq and desirably has a broader tolerance range regarding its width than the prior art according to KiTorq. 
     It is a second object of the invention to suggest a torque and angle of rotation detection system for which the detection of the angle of rotation is not readily disturbed by external magnetic fields. 
     Furthermore, it is a third object of the invention to provide a torque and angle of rotation detection system that is less expensive to manufacture than the prior art according to KiTorq. 
     A fourth object of the present invention is to provide a torque and angle of rotation detection system in which the stator unit can be easily and quickly mounted adjacent to the rotor unit to arrange the magnetic field sensor in close proximity to the dipole magnets. 
     Each of these objects, as well as others, has been achieved by the features described herein. 
     The invention relates to a torque and angle of rotation detection system; comprising a rotor unit which is able to rotate about an axis of rotation; comprising a stator unit arranged in a stationary manner and separated from the rotor unit by an air gap that is radial with respect to the axis of rotation; wherein the rotor unit comprises strain gauges which detect a torque acting onto the rotor unit; wherein the rotor unit comprises a plurality of dipole magnets arranged spaced apart from each other; wherein the stator unit comprises a magnetic field sensor which measures the magnetic fields of the dipole magnets during rotation of the rotor unit; wherein the stator unit comprises a primary coil and the rotor unit comprises a secondary coil; wherein a primary electrical voltage in the primary coil generates a secondary electrical voltage in the secondary coil; wherein each of the dipole magnets has a remanence of more than or equal to 1,000 mT, preferably of more than or equal to 1,400 mT; and wherein the secondary coil comprises a plurality of ferrite elements. 
     According to the invention, the dipole magnets of the rotor assembly have a strong remanence. The remanence of the dipole magnets according to the invention is at least five times higher as compared to that of the magnetized ferrite powder/rubber mixture of the dipole magnets according to KiTorq. It is this strong remanence that enables the measurement of the magnetic fields of the dipole magnets by the magnetic field sensor of the stator unit to be carried out from a greater distance. Moreover, since the remanence is that strong it is not easily disturbed by external magnetic fields. 
     Ferrite elements consist of very pure iron-oxygen compounds pressed into uniform pellets at high pressure. Therefore, ferrite elements are characterized by containing a large proportion of magnetic material and are highly compacted. This is the reason why ferrite elements have a high permeability. Furthermore, ferrite elements achieve an improved efficiency of inductive coupling between the primary and secondary coils as compared to that of the iron powder/resin mixture according to KiTorq. Due to the improved efficiency, inductive coupling can occur over a greater distance. 
     Thus, the combination of dipole magnets having a strong remanence and ferrite elements in the secondary coil of the system according to the invention has the synergistic effect that it is possible to increase the radial air gap between the rotor unit and the stator unit and that it is further possible to increase the tolerance range for the permissible width of the radial air gap. 
     In addition, ferrite elements are inexpensive to purchase making the manufacture of the system cost-effective. 
     In a presently preferred embodiment of the system, the width of the radial air gap is more than/equal to 2.0 mm with a tolerance range for the radial air gap of +/-1.5 mm. 
     Here, the radial air gap is at least twice the size and its allowable radial air gap tolerance range is even three times as large compared to the torque and rotation angle sensing system of the prior art according to KiTorq. 
     In a presently preferred embodiment of the system, the rotor unit comprises a rotor body and a plurality of blind holes, which blind holes are provided on the outside of the rotor body; and wherein the ferrite elements are secured in the blind holes. 
     This securing of the ferrite elements in blind holes is easy to accomplish which makes the manufacture of the system cost-effective. 
     In a presently preferred embodiment of the system, the securing of the ferrite elements in the blind holes is achieved by a form-locking connection. 
     In a presently preferred embodiment of the system, each blind hole comprises an interior space, which interior space comprises at least one inner surface; wherein each ferrite element comprises at least one outer surface; and wherein the inner surface and the outer surface are machined to match one another in size and a mechanical contact of the inner and outer surfaces results in a form-locking connection. 
     The form-locking connection ensures that the ferrite elements do not become detached from the rotor body even under a high centrifugal force of 20000 min -1  and more. This form-locking connection is easy to accomplish and makes the manufacture of the system cost-effective. 
     In a presently preferred embodiment of the system, the rotor unit comprises a coil winding, which coil winding is attached radially to the outside of the ferrite elements. 
     This attachment of the coil winding radially to the outside of the ferrite elements is also easy to accomplish which makes the manufacture of the system cost-effective. 
     In a presently preferred embodiment of the system, the dipole magnets are made of neodymium-iron-boron. 
     Dipole magnets made of neodymium-iron-boron are inexpensive to purchase which also makes the manufacture of the system cost-effective. 
     In a presently preferred embodiment of the system, the rotor unit comprises a rotor body and a groove, which groove is arranged radially in the outside of the rotor body; and wherein the dipole magnets are secured within the groove. 
     This groove is easily fabricated in the rotor body. In this way, the dipole magnets secured in the groove are arranged at substantially the same radial distance from the axis of rotation as the coil winding so that it is possible to cover the dipole magnets and coil winding by a rotor cover of simple design. Thus, the groove contributes to making the manufacture of the system cost-effective. 
     In a presently preferred embodiment of the system, the rotor unit comprises a rotor cover, which rotor cover is attached radially to the outside of the rotor unit. 
     In a presently preferred embodiment of the system, the rotor cover is attached to the rotor unit by a force-locking connection. 
     In a presently preferred embodiment of the system, the rotor cover is clamped onto the rotor unit. 
     In a presently preferred embodiment of the system, the rotor unit comprises a coil winding; and in that the rotor cover clamped onto the rotor unit completely covers the coil winding and the dipole magnets. 
     This rotor cover protects the dipole magnets and the coil winding from mechanical damage. This rotor cover can be easily attached to the rotor unit and makes the manufacture of the system cost-effective. 
     In a presently preferred embodiment of the system, the stator unit is arranged along the axis of rotation with an axial offset tolerance in the range of +/-1.0 mm relative to the rotor unit. 
     The axial offset tolerance corresponds to an axial degree of freedom when the stator unit is mounted adjacent to the rotor unit. The measurement of the magnetic fields of the dipole magnets by the magnetic field sensor is not disturbed when complying with this axial offset tolerance. Due to this axial degree of freedom the stator unit can be mounted adjacent to the rotor unit in an easy and quick manner. 
     In a presently preferred embodiment of the system, the magnetic field sensor generates a magnetic field signal for each magnetic field measured; wherein the stator unit comprises an evaluation unit, which evaluation unit executes an evaluation program; wherein the magnetic field sensor transmits the magnetic field signals to the evaluation unit; and wherein the evaluation program counts the magnetic field signals and multiplies them by the distance of the dipole magnets from each other to determine the angle of rotation that has been traveled by the rotor unit. 
     In a presently preferred embodiment of the system, the strain gauges generate measurement signals for a detected torque; wherein the rotor unit comprises a rotor antenna; wherein the strain gauges transmit the measurement signals to the rotor antenna; wherein the stator unit comprises a stator antenna and an evaluation unit, which evaluation unit executes an evaluation program; wherein the rotor antenna sends the measurement signals to the stator antenna; wherein the stator antenna transmits the measurement signals received from the rotor antenna to the evaluation unit; and wherein the evaluation program determines the torque that acts onto the rotor unit from the transmitted measurement signals. 
    
    
     
       BRIEF DESCRIPTION OF THE SEVERAL VIEWS OF EXEMPLARY DRAWINGS 
       In the following, the invention will be explained in more detail by way of example with reference to the figures in which: 
         FIG.  1    shows a view of a portion of a torque and angle of rotation detection system  1  comprising a rotor unit  10  and a stator unit  20 ; 
         FIG.  2    shows a view looking in the direction of the arrows pointing at portion of the system  1  according to  FIG.  1    in section along dashed line C-C; 
         FIG.  3    shows an enlarged cross-sectional view of the portion of the system  1  according to  FIG.  2   ; 
         FIG.  4    shows an enlarged view of a portion of the rotor unit  10  according to  FIGS.  1  and  2   ; and 
         FIG.  5    shows an enlarged cross-sectional view looking in the direction of the arrows pointing at a portion of the rotor unit  10  according to  FIG.  3    along chain-dashed line D-D. 
     
    
    
     DETAILED DESCRIPTION OF EXEMPLARY EMBODIMENTS OF THE INVENTION 
       FIG.  1    shows a view of a portion of the torque and angle of rotation detection system that is designated generally by the numeral  1 .  FIG.  2    is a representation of the view according to  FIG.  1    in section along line C-C.  FIG.  3    is an enlarged cross-sectional view of a portion of the system  1  as shown in  FIG.  2   .  FIG.  4    is an enlarged view of a portion of the rotor unit  10  as shown in  FIGS.  1  and  2   . In addition,  FIG.  5    is an enlarged cross-sectional view of a portion of the rotor unit  10  according to  FIG.  3    along line D-D. The same reference numerals designate the same features in the figures. 
     System  1  is represented in a three-dimensional coordinate system comprising a rotational axis X, which is normal to the plane in which  FIG.  1    lies, a horizontal axis Y, and a vertical axis Z. The three axes are perpendicular to each other. 
     System  1  comprises a rotor unit that is designated generally by the numeral  10  and a stator unit that is designated generally by the numeral  20 . 
     The rotor unit  10  comprises a rotor body  100  that is hollow-cylindrical in shape. The rotor body  100  is made of a mechanically resistant material such as steel, stainless steel, and the like. The rotor unit  10  is designed as a flange which can be attached to any rotating component by means of a screw connection. The rotor unit  10  is configured for rotational speeds of 20000 min -1  and higher. 
     The stator unit  20  is disposed in a stationary manner. As schematically shown in  FIG.  1   , the nearest surface of the stator  20  is separated from the surface of the outermost peripheral edge of the rotor unit  10  by a radial air gap  30  with respect to the axis of rotation X. The width of the radial air gap  30  is more than/equal to 2.0 mm, and a tolerance  31  for the radial air gap is in the range of +/-1.5 mm. Regardless of this, as schematically shown in  FIG.  2   , there is an axial offset tolerance  32  for an offset relative to the rotor unit  10  along the axis of rotation X. The axial offset tolerance  32  is in the range of +/-1.0 mm. 
     The rotor unit  10  comprises strain gauges  15  schematically shown in  FIG.  2   . The strain gauges  15  comprise a measurement grid and a bridge circuit. When an electrical voltage is applied to the measurement grid, the measurement grid exhibits an electrical resistance. The electrical resistance changes upon expansion or compression of the measurement grid, which change in electrical resistance generates measurement signals in the bridge circuit. The strain gauges  15  detect torque in a dynamic manner generating up to 10,000 measurement signals per second at a sampling rate of up to 35 kSample. The measurement signals have a resolution of 24 bits. The strain gauges  15  detect a maximum nominal torque of 100 Nm and more with an accuracy of within 0.05%. 
     As schematically shown in  FIG.  3   , the rotor unit  10  further comprises a rotor antenna  13  and the stator unit  20  comprises a stator antenna  23 . The strain gauges  15  and the rotor antenna  13  are electrically connected to each other by electrical connecting lines. The strain gauges  15  transmit the measurement signals to the rotor antenna  13  via the electrical connecting lines. The measurement signals are transmitted from the rotor unit  10  to the stator unit  20  in a contactless manner. For this purpose, the rotor antenna  13  sends the measurement signals to the stator antenna  23 . In a presently preferred embodiment, the transmission frequency of 13.56 MHz in the Industrial Scientific and Medical (ISM) band is used and a data transmission rate of up to 1.4 Mbitsec -1  is achieved. 
     As schematically shown in  FIG.  3   , the rotor unit  10  comprises a secondary coil  11  and the stator unit  20  comprises a primary coil  21 . The primary coil  21  and the secondary coil  11  are inductively coupled to each other. A primary electrical voltage in the primary coil  21  generates a secondary electrical voltage in the secondary coil  11 . By inductive coupling, the stator unit  20  supplies electrical power to the rotor unit  10 . Inductive coupling between the primary coil  21  and the secondary coil  11  is contactless and occurs in the ISM band with carrier frequencies in the range of 115 kHz to 130 kHz. 
     The secondary coil  11  and the strain gauges  15  are electrically connected to each other by electrical connecting lines. The secondary coil  11  supplies electrical power to the strain gauges  15  via the electrical connecting lines. The secondary coil  11  and the rotor antenna  13  are electrically connected to each other by electrical connecting lines. The secondary coil  11  supplies electrical power to the rotor antenna  13  via the electrical connecting lines. 
     As schematically shown in  FIG.  3   , the body  100  of the rotor unit  10  defines a plurality of blind holes  12 . The blind holes  12  are disposed radially in the outside of the rotor body  100 . The blind holes  12  are arranged on a circumference at a constant radial distance from the axis of rotation X. In a presently preferred embodiment, each blind hole  12  is defined by a blind hole opening  120  disposed opposite the blind end of the blind hole  12  and defining an entrance permitting access into the blind hole  12 . The blind hole opening  120  is configured and disposed to lie in a plane disposed normal to the axis of rotation X in the rotor body  100 . Each blind hole  12  defines an interior space  121  that elongates between the blind hole opening  120  and the closed blind end of the blind hole  12 . The interior space  121  may be accessed from the outside of the rotor unit  10  through the blind hole opening  120 . 
     As schematically shown in  FIG.  3   , the secondary coil  11  comprises a plurality of ferrite elements  110 . The ferrite elements  110  desirably are manganese-zinc ferrites, nickel-zinc ferrites, and the like. In a presently preferred embodiment, the ferrite elements  110  are made from 3C90 material. The 3C90 material grade exhibits an initial magnetic permeability of more than/equal to 2,000, and in a presently preferred embodiment of more than/equal to 2,300. The initial magnetic permeability is determined in accordance with standard DIN IEC 60401, at a room temperature of 25° C., with a low electric current frequency of less than or equal to 10 kHz and a low peak magnetic flux of less than 0.25 mT. The initial magnetic permeability shows a scatter of +/-20%. For carrier frequencies in the range of 115 kHz to 130 kHz, 3C90 material exhibits low eddy current losses in the range of 165 kWm -3  to 205 kWm -3 . The eddy current loss is determined at a room temperature of 25° C. and a peak magnetic flux of 100 mT. In a presently preferred embodiment, the ferrite elements  110  are cylindrical in shape. It is presently preferred that each ferrite element  110  has a diameter of 2.0 mm and a length of 7.5 mm. In a presently preferred embodiment, the secondary coil  10  comprises one hundred ferrite elements  110 . In a presently preferred embodiment, the distance separating adjacent ones of the ferrite elements  12  from each other is 3.7 mm. 
     The ferrite elements  110  are arranged on the circumference of the blind holes  12  at a constant distance from each other. The ferrite elements  110  are secured in the blind holes  12 . One ferrite element  110  is secured in each blind hole  12 . The ferrite element  110  is inserted in the interior space  121  through the blind hole opening  120 . The ferrite elements  110  are secured in the blind holes  12  by a form-locking connection such as engaging mechanically by a snap-in, click-in and the like, or by a material bond such as adhesive bonding and the like, or by a force-locking connection such as clamping and the like, or by any combination of a form-locking connection, a material bond and a force-locking connection. In a presently preferred embodiment, and as schematically shown in  FIG.  5   , the interior space  121  of each blind hole  12  is defined by at least one inner surface  1001  and the ferrite element  110  is defined by at least one outer surface  1101 , which complements the shape of the opposing inner surface  1001  of the blind hole  12 . The inner surface  1001  and the outer surface  1101  are machined to match each other, and a mechanical contact of the inner surface  1001  and the outer surface  1101  results in a form-locking connection. Thus, when the rotor unit  10  rotates at rotational speeds of 20000 min -1  and higher and a centrifugal force acts onto the ferrite elements  11 , the ferrite element  11  will not become detached from the rotor body  100  since the form-locking connection prevents separation of the ferrite element  11  from the rotor body  100 . 
     As schematically shown in  FIG.  3   , the rotor unit  10  comprises a coil winding  111 . The coil winding  111  is attached radially to the outside of the ferrite elements  110 . The coil winding  111  is arranged on a circumference at a constant radial distance from the axis of rotation X. The coil winding  111  consists of wires made of an electrically conductive material such as copper, and the like. Advantageously, the wires have a circular cross-sectional shape and are 0.4 mm in diameter. 
     The rotor unit  10  comprises a groove  16 . Groove  16  is defined radially in the outside of the rotor body  100 . Groove  16  is arranged on a circumference at a constant radial distance from the axis of rotation X. 
     The rotor unit  10  comprises a plurality of dipole magnets  14  having a remanence of at least 1,000 mT, preferably of at least 1,400 mT. In a presently preferred embodiment, the dipole magnets  14  are made of neodymium-iron-boron. In a presently preferred embodiment, the dipole magnets  14  are secured in the groove  16 . The dipole magnets  14  are secured by means of material bonding such as adhesive bonding and the like, or by a force-locking connection such as clamping and the like, or a combination of material bonding and a force-locking connection. The dipole magnets  14  are arranged at a constant distance from each other on the circumference of the groove  16 . In a presently preferred embodiment, the rotor unit  10  comprises seventy-two dipole magnets  14 . In a presently preferred embodiment, the distance between the dipole magnets  14  is 5.0 mm. It is presently preferred that the dipole magnets  14  are cuboidal in shape. In a presently preferred embodiment, the size of each dipole magnet  14  is 3.0×3.0×4.0 mm 3 . Thus, each dipole magnet  14  desirably has an axial length of 3 mm along the axis of rotation X. This axial length of 3 mm allows for an axial degree of freedom when mounting the stator unit  20  adjacent to the rotor unit  10 . The reason for this is that it is no longer necessary to mount the magnetic field sensor  24  of the stator unit  20  in close proximity to the dipole magnets  14 , but rather it may be mounted with an axial offset tolerance  32  in the range of +/-1.0 mm without affecting the measurement of the magnetic fields of the dipole magnets  14  by the magnetic field sensor  24 . 
     As schematically shown in  FIG.  3   , the rotor unit  10  comprises a rotor cover  17 . The rotor cover  17  is attached radially to the outside of the rotor unit  10 . The rotor cover  17  is attached to the rotor unit  10  by a force-locking connection such as clamping and the like. The rotor cover  17  is made of a material that has high tensile strength and rigidity such as carbon fiber reinforced plastic (CFRP), glass fiber reinforced plastic (GFRP), and the like. The rotor cover  17  is arranged on a circumference at a constant radial distance from the axis of rotation X. The rotor cover  17  is ribbon-shaped, which defines a long narrow strip that bends to conform to the outside of the rotor unit  10 . Advantageously, the rotor cover  17  may be clamped onto the rotor unit  10  by elastic deformation. Advantageously, the rotor cover  17  clamped onto the rotor unit  10  completely covers the coil winding  111  and the dipole magnets  14 . Advantageously, a radially outer end of the dipole magnets  14  is located at substantially the same radial distance from the axis of rotation X as radially outer ends of the coil winding  111 . Thus, the rotor cover  17  clamped onto the rotor unit  10  is in direct mechanical surface contact on the outside in a radial direction with the coil winding  111  and in direct mechanical surface contact with the dipole magnets  14 . The rotor cover  17  is configured and disposed to protect the coil winding  111  and the dipole magnets  14  from mechanical damage. 
     As schematically shown in  FIG.  3   , the stator unit  20  comprises a magnetic field sensor  24  that measures the magnetic fields of the dipole magnets  14  during rotation of the rotor unit  10 . The magnetic field sensor  24  desirably is a Hall effect sensor, a magneto-resistive sensor and the like. For each magnetic field measured, the magnetic field sensor  24  generates a magnetic field signal. In a presently preferred embodiment, the magnetic field signal is a digital signal. 
     As schematically shown in  FIG.  3   , the stator unit  20  comprises an evaluation unit  25 . The evaluation unit  25  desirably is an electrical circuit comprising at least one data processor and at least one data memory. The evaluation unit  25  comprises at least one evaluation program. The evaluation program is stored in the data memory and can be loaded from the data memory into the data processor. The evaluation unit  25  executes the evaluation program loaded into the data processor. 
     The stator antenna  23  and the evaluation unit  25  are electrically connected to each other by electrical connecting lines. The stator antenna  23  transmits the measurement signals received from the rotor antenna  13  to the evaluation unit  25  via the electrical connecting lines. The evaluation program loaded into the data processor is configured to calculate the torque that acts onto the rotor unit  10  from the transmitted measurement signals. 
     The magnetic field sensor  24  and the evaluation unit  25  are electrically connected to each other by electrical connecting lines. The magnetic field sensor  24  transmits the magnetic field signals to the evaluation unit  25  via the electrical connecting lines. The evaluation program loaded into the data processor is configured to count the magnetic field signals transmitted. The magnitude of the distance between the dipole magnets  14  is stored in the data memory. From the data memory, the evaluation program loaded into the data processor is configured to read the magnitude of the distance of the dipole magnets  14  from each other which the evaluation is configured to multiply by the number of magnetic field signals counted, thereby determining the angle of rotation traveled by the rotor unit  10 . 
     The system  1  is useful in industrial measurement technology in a variety of ways. Thus, system  1  may be used for measuring the torque and the angle of rotation in test stand technology, for example. However, system  1  may also be used in chip-removing machining of workpieces for measuring the torque and the angle of rotation of rotating components. 
     
       
         
           
               
               
             
               
                 List of reference numerals 
               
             
            
               
                 
                   1 
                 
                 system 
               
               
                 
                   10 
                 
                 rotor unit 
               
               
                 
                   11 
                 
                 secondary coil 
               
               
                 
                   100 
                 
                 rotor body 
               
               
                 
                   1001 
                 
                 inner surface 
               
               
                 
                   110 
                 
                 ferrite element 
               
               
                 
                   111 
                 
                 coil winding 
               
               
                 
                   1101 
                 
                 outer surface 
               
               
                 
                   12 
                 
                 blind hole 
               
               
                 
                   120 
                 
                 blind hole opening 
               
               
                 
                   121 
                 
                 interior space 
               
               
                 
                   13 
                 
                 rotor antenna 
               
               
                 
                   14 
                 
                 dipole magnet 
               
               
                 
                   15 
                 
                 strain gauge 
               
               
                 
                   16 
                 
                 groove 
               
               
                 
                   17 
                 
                 rotor cover 
               
               
                 
                   20 
                 
                 stator unit 
               
               
                 
                   21 
                 
                 primary coil 
               
               
                 
                   22 
                 
                 stator cover 
               
               
                 
                   23 
                 
                 stator antenna 
               
               
                 
                   24 
                 
                 magnetic field sensor 
               
               
                 
                   25 
                 
                 evaluation unit 
               
               
                 
                   30 
                 
                 radial air gap 
               
               
                 
                   31 
                 
                 radial air gap tolerance 
               
               
                 
                   32 
                 
                 axial offset tolerance 
               
               
                 c-c 
                 section 
               
               
                 d-d 
                 section 
               
               
                 x 
                 rotational axis 
               
               
                 y 
                 horizontal axis 
               
               
                 z 
                 vertical axis