DEVICE FOR GENERATING ELECTRICAL ENERGY FROM A ROTATIONAL MOVEMENT

Abstract

The invention relates to a device (1) for generating electrical energy from a rotational movement, comprising a stator (3) which can rotate about a rotational axis and a rotor (4) which can rotate about the rotational axis (2) and is connected to the stator (3), which rotor comprises a centre of gravity (5) located outside the rotational axis (2), wherein in the stator (3) a coil is arranged for inducing an electrical voltage when the stator (3) is rotated relative to the rotor (4), wherein an electrical circuit (7) is connected to the coil, said circuit comprising an energy store (6) for rectifying the voltage induced in the coil. In order to achieve a maximum energy yield under various conditions of use, according to the invention, the device (1) is configured to detect a position of a plane defined by the rotational axis (2) and the centre of gravity (5) of the rotor (4) and to influence the position of the plane by means of a current flow through the coil, so that a deflection of the plane from the vertical can be limited by the current flow during a rotation of the stator (3). The invention also relates to a use of a such a device (1).

Claims

1. An apparatus (1) for generating electrical energy from a rotational movement, comprising a stator (3) that can rotate about a rotation axis (2) and a rotor (4) that can rotate about the rotation axis (2) and is connected to the stator (3), which rotor comprises a center of gravity (5) located outside the rotation axis (2), wherein in the stator (3) a coil is arranged for inducing an electrical voltage when the stator (3) is rotated relative to the rotor (4), wherein an electrical circuit (7) is connected to the coil, said circuit comprising an energy store (6) for rectifying the voltage induced in the coil, characterized in that the apparatus (1) is configured to detect a position of a plane defined by the rotation axis (2) and the center of gravity (5) of the rotor (4) and to influence the position of the plane by means of a current flow through the coil, so that a deflection of the plane from a vertical line can be limited by the current flow when the stator (3) rotates.

2. The apparatus (1) according to claim 1, characterized in that a deflection of the plane is limited to a deflection angle (8) of maximally 180, in particular maximally 90, from a resting position.

3. The apparatus (1) according to claim 1 , characterized in that a distance (10) of the center of gravity (5) of the rotor (4) from the rotation axis (2) is equal to more than 10%, preferably more than 20%, in particular more than 40%, of a maximum distance (9) of the rotor (4) from the rotation axis (2).

4. The apparatus (1) according to claim 1, characterized in that the stator (3) is embodied for a rotation about the rotation axis (2) at a rotational speed of more than 100 rpm, preferably more than 500 rpm, in particular more than 1500 rpm.

5. The apparatus (1) according to claim 1, characterized in that a tilt sensor is provided to detect a slope of the rotation axis (2).

6. The apparatus (1) according to claim 1, characterized in that the apparatus (1) is embodied to limit a current through the coil depending on a slope of the rotation axis (2).

7. The apparatus (1) according to claim 1, characterized in that a deflection of the plane can be influenced by means of energy from the energy store (6).

8. The apparatus (1) according to claim 1, characterized in that two to six, in particular three, coils are provided in the stator (3).

9. The apparatus (1) according to claim 1, characterized in that the circuit (7) comprises at least one transistor, in particular a MOSFET (11, 12), for rectifying the voltage induced in the coil.

10. The apparatus (1) according to claim 9, characterized in that an operational amplifier (13) connected to the transistor and to an intermediate circuit and the coil is provided, so that a switching of the transistor by the operational amplifier (13) can occur depending on a voltage between the coil and the intermediate circuit.

11. The apparatus (1) according to claim 9, characterized in that a microcontroller is provided for controlling the transistor.

12. The apparatus (1) according to claim 1, characterized in that a voltage converter, in particular a step-up converter, is provided to transform an output voltage of the intermediate circuit into a higher value.

13. A rim, in particular an automobile rim, having an apparatus (1) for generating electrical energy from a rotational movement, characterized in that the apparatus (1) is embodied according to claim 1.

14. The rim according to claim 13, characterized in that the apparatus (1) is arranged in the center of the rim so that a rotation axis (2) of the rim coincides with the rotation axis (2) of the apparatus (1).

15. The rim according to claim 14, characterized in that a sensor for detecting a physical property of a tire mounted on the rim, in particular a pressure sensor, is provided, which sensor is connected to the apparatus (1) for the purpose of energy supply.

16. The rim according to claim 14, characterized in that a device for wireless data transmission is provided.

17. The rim according to claim 14, characterized in that a compressor for influencing a tire pressure is provided, wherein the compressor is connected to the apparatus (1) for the purpose of energy supply.

18. A use of an apparatus (1) according to claim 1 for generating electrical energy in a wheel of a motor vehicle.

Description

[0033] Additional features, advantages and effects of the invention follow from the exemplary embodiments described below. The drawings which are thereby referenced show the following:

[0034] FIGS. 1 and 2 An apparatus according to the invention in different operating states;

[0035] FIGS. 3 through 5 Various exemplary embodiments of an electrical circuit of an apparatus according to the invention.

[0036] FIGS. 1 and 2 schematically show an exploded view of an apparatus 1 according to the invention for generating electrical energy from a rotational movement in different operating states. As can be seen, the apparatus 1 comprises a rotating electrical machine with a rotor 4 having a roughly semicircular cross-section. Furthermore, a stator 3 is provided that is connected to the rotor 4 such that it can rotate about an rotation axis 2, in which stator three coils, which are not illustrated, are arranged for inducing an electrical voltage during a relative rotation between the rotor 4 and the stator 3. For this purpose, permanent magnets are provided in the rotor 4. In order to also achieve a highest possible electrical voltage with small dimensions and/or low rotational speeds, multiple permanent magnets are normally provided, so that the rotor 4 preferably has a pole pair number of 2 to 20. In the illustrated rotor 4, the pole pair number is twelve.

[0037] To connect the apparatus 1 to a rotating system in which the apparatus 1 is positioned for generating electrical energy, a roughly hollow-cylindrical outer shell 17 is provided. This outer shell 17 can, for example, be arranged in a central recess in a center of a rim of a wheel on a vehicle and connected to the rim in a fixed manner, so that the outer shell 17 rotates along with the rim. In this case, a rotation axis 2 of the rim coincides with a rotation axis 2 of the apparatus 1. The outer shell 17 is connected in a fixed manner to the stator 3 via a connecting element 19, so that when the apparatus 1 is operated in a rotating system such as a rim, the stator 3 has a rotational speed of the rotating system. The designations rotor 4 and stator 3 thus correspond to the nomenclature typical for rotating electrical machines, but in contrast to stationary rotating electrical machines, do not in this case indicate a kinematic behavior of the respective components during operation of the apparatus 1.

[0038] When the apparatus 1 is at a standstill, or during operation in which no moment is transmitted between the rotor 4 and the stator 3 so that current also does not flow through the coils of the stator 3, the rotor 4 is in a resting position as illustrated in FIG. 1, wherein a center of gravity 5 of the rotor 4 is positioned perpendicularly below the rotation axis 2. An imaginary plane which is defined by the rotation axis 2 and the center of gravity 5 of the rotor 4 or contains the rotation axis 2 and the center of gravity 5 thus lies vertically in the resting position, so that a deflection angle in the resting position is 0.

[0039] Due to the roughly semicircular cross-section of the rotor 4, the center of gravity 5 of the rotor 4 does not lie on the rotation axis 2, so that there results a distance 10 between the center of gravity 5 of the rotor 4 and the rotation axis 2. A maximum distance 9 of the rotor 4 from the rotation axis 2 corresponds to a radius of the semicircular cross-section. Typically, a ratio of the distance 10 of the center of gravity 5 to the rotation axis 2 to a maximum distance 9 of the rotor 4 from the rotation axis 2 is greater than 10%, preferably 30% to 50%, in particular approximately 40%. Thus, an especially high moment is necessary to deflect the rotor 4 from the resting position, whereby a high electrical power can be generated with the apparatus 1.

[0040] If electrical energy is generated so that a current flows through the coils, a moment transmitted onto the rotor 4 from the stator 3 causes a deflection of the rotor 4, which can also be referred to as inertial mass. A maximum moment or a maximum power is thereby reached when the imaginary plane is deflected from the resting position by a deflection angle 8 of 90, or when the center of gravity 5 of the rotor 4 is at the same height as the rotation axis 2. An operating state of this type, in which the deflection angle 8 by which the imaginary plane is deflected from an orthogonal line 20 is approximately 90, is shown again in an exploded view in FIG. 2.

[0041] The apparatus 1 is embodied to detect and influence a position of the plane by means of a current flow through the at least one coil in the stator 3. For this purpose, a circuit 7 is provided with which a defined current flow through the coils can be achieved in order to influence a position of the imaginary plane. The electronic circuit 7 is connected to the stator 3 in a fixed manner and, like the stator 3, is also embodied for continuous loading with centrifugal forces that can occur at a rotational speed typical for wheels of a motor vehicle. The electrical current 7 is also used to rectify an alternating voltage induced in the coils. For this purpose, an energy store 6, such as a rechargeable battery, capacitor or battery, that is connected to an intermediate circuit is provided. To protect the apparatus 1 against contamination, a lid 18 which tightly seals the outer shell 17 is provided.

[0042] FIG. 3 shows an exemplary embodiment of a circuit 7 of the apparatus 1 illustrated in FIG. 1. On the one hand, three connection points 16 are provided to connect the coils of the stator 3 which are typically connected to form a delta connection or a star connection. On the other hand, an intermediate circuit can be seen, to which circuit an energy store 6, which is not illustrated, is connected. The intermediate circuit thus comprises a first voltage level 14 and a second voltage level 15, wherein a potential difference between the first voltage level 14 and the second voltage level 15 corresponds to a voltage of the energy store 6. To rectify the voltages induced in the coils, two transistors embodied as MOSFETs 11, 12 are provided for each connection point 16, wherein in the exemplary embodiment illustrated, one p-channel MOSFET 12 each is provided between a connection point 16 and the first voltage level 14, which has a higher potential than the second voltage level 15, and one n-channel MOSFET 11 each is provided between a connection point 16 and the second voltage level 15. Enhancement-type MOSFETs 11, 12 are used in each case, wherein a flyback diode 21 is provided parallel to each MOSFET 11, 12.

[0043] To control the MOSFETs 11, 12, one operational amplifier 13 is provided for each MOSFET 11, 12, which amplifier is used as a comparator for comparing a voltage of the connection point 16 with a voltage of the voltage level 14, 15 to which the respective MOSFET 11, 12 connects the connection point 16. Thus, the respective MOSFET 11, 12 is switched, or becomes conductive, by means of the operational amplifier 13 precisely when a voltage between the connection point 16 and the first voltage level 14 is positive or when a voltage between the connection point 16 and the second voltage level 15 is negative. An undesired discharge of the energy store 6 by a current flow from the energy store 6 into the coil is thus prevented.

[0044] In the illustrated circuit 7, a supply of voltage to the operational amplifiers 13 occurs via the intermediate circuit or the energy store 6. If no energy is stored in the energy store 6, the MOSFETs 11, 12 are not switched by the operational amplifiers 13, since a sufficient supply voltage is not available to the operational amplifiers 13 in this case. As a result, a rectification of the voltage induced in the coils takes place via the flyback diodes 21 that are connected in parallel with the MOSFETs 11, 12. Therefore, when the energy store 6 is empty, the circuit only functions starting at a voltage that is higher than a threshold voltage of the diodes, typically starting at approximately 0.7 V. From this point on, the energy store 7 will be charged.

[0045] If energy is stored in the energy store 6, a voltage of this type is not necessary to overcome a threshold voltage of the diodes between the connection point 16 and the first voltage level 14 or second voltage level 15, since the operational amplifiers are supplied with energy from the energy store and can control the MOSFETs with a low voltage drop. Thus, even a voltage of 0.1 V, for example, can be rectified and used for energy consumption. In this manner, a particularly high efficiency can also be achieved at low rotational speeds.

[0046] FIG. 4 shows a further exemplary embodiment of a circuit 7 of an apparatus 1 according to FIG. 1. In contrast to the circuit 7 illustrated in FIG. 3, in this case only n-channel MOSFETs 11 are provided both between the connection points 16 and the first voltage level 14 and also between the connection points 16 and the second voltage level 15. Furthermore, an additional system voltage level 22 is provided which is connected to the intermediate circuit by a voltage converter, such as what is referred to as a step-up converter, which is not illustrated. As a result of the voltage converter, a higher voltage is present at the system voltage level 22 than at the first voltage level 14 of the intermediate circuit. In the illustrated circuit 7, a positive supply voltage for the operational amplifiers 13 is not, in contrast to the circuit 7 illustrated in FIG. 3, supplied by the first voltage level 14, but rather by the system voltage level 22. As is the case with the circuit 7 illustrated in FIG. 3, the second voltage level 15 can be used as a negative supply voltage for the operational amplifiers 13.

[0047] Because the operational amplifiers 13 in this case are not supplied with energy via the intermediate circuit, but rather via the system voltage level 22, a switching of the MOSFETs 11, 12 is, compared to the circuit 7 illustrated in FIG. 1, already possible at an intermediate circuit voltage that is lower than the threshold voltage of the diodes, even when the energy store 6 is empty. Thus, even with an empty energy store, a particularly high efficiency is already achieved starting at an intermediate circuit voltage of approximately 0.1 V, the threshold voltage of the MOSFETs.

[0048] By means of the step-up converter, a consistent voltage of approximately 2.8 V to 4.1 V is achieved at the system voltage level 22 starting at an intermediate circuit voltage of approximately 0.1 V, depending on the configuration. When the rotational speed or relative speed between the rotor 4 and stator 3 increases, the voltage in the intermediate circuit increases due to the increasing voltage in the coils of the stator 3, as a consequence of which a voltage difference between the system voltage level 22 and the intermediate circuit or the first voltage level 14 decreases as the rotational speed increases. If this voltage difference is less than 0.6 V, the MOSFETs 11 connected to the first voltage level 14 can no longer be switched by the operational amplifiers 13, whereby a voltage drop occurs. This is advantageous, since an excessive amount of energy is available anyway at high rotational speeds, so that damage to electrical consumers can be avoided.

[0049] FIG. 5 shows a further exemplary embodiment of a circuit 7 for an apparatus 1 according to FIG. 1. Similar to the circuit 7 illustrated in FIG. 3, p-channel MOSFETs 12 are once again provided between the connection points 16 and the first voltage level 14, and n-channel MOSFETs 11 are once again provided between the connection points 16 and the second voltage level 15. Unlike in the circuit 7 according to FIG. 3, a direct current voltage converter or step-up converter is provided in this circuit 7, which converter transforms a voltage of the intermediate circuit between the first voltage level 14 and second voltage level 15 to a higher level, so that a system voltage level 22 having a higher voltage is provided in order to supply the operational amplifiers 13 with energy even at a low intermediate circuit voltage. In this embodiment, as a result of the higher system voltage level 22, the n-channel MOSFETs 11 are already switched at a low intermediate circuit voltage, but a negative supply voltage for the operational amplifiers 13 would be required to switch the p-channel MOSFETs 12, for which reason the p-channel MOSFETs 12 between the connection points 16 and the first voltage level 14 are only switched by the operational amplifiers 13 at higher rotational speeds.

[0050] An apparatus 1 according to the invention enables a generation of electrical energy by a rotational movement with particularly high efficiency, since even low voltages which are achieved at low rotational speeds and with a small size can be utilized. As a result of the preferred use of a rotating electrical machine that is embodied to be brushless, high reliability, long service life, low wear and a particularly high efficiency are achieved. For example, what is referred to as a brushless direct current motor can be used. In addition, with an apparatus 1 according to the invention, it is ensured that a co-rotation by the rotor 4, and thus damage to the same from centrifugal forces, is prevented. The apparatus 1 can thus also be used in a wheel of a motor vehicle, for example, to supply energy to a tire pressure sensor and to a compressor for influencing the tire pressure. Compared to apparatuses 1 from the prior art, which generate electrical energy using a piezoelectric effect, a significantly greater energy yield can be achieved with an apparatus 1 according to the invention. As a result of the small installation footprint that can be achieved, the apparatus 1 according to the invention can be installed in the center of a rim on a motor vehicle, whereby an imbalance of the wheel is not increased and a visual appearance is not impaired.