Patent Application
20220037965
The present invention relates to a brushless electric motor with integrated positional sensing. Electric motors and positional sensing are well-known in the art: the “brushless” type of electric motor dates from the latter half of the 20th Century and uses solid-state electronics to replace the physical commutator (polarity reversal switch) that allowed brush-type electric motors to function. Positional sensing, dating back to switches that tripped when an element of a larger machine physically engaged them, is likewise well-known in the art.
While brushless motors were a large improvement in many ways, as they have less frictional load and fewer mechanical parts, they have many inefficiencies. Constantly reversing the electromagnets causes electrical inefficiencies, and the windings of the electromagnets can suffer fatigue and/or heat breakdown which causes the motor to become inefficient or stop functioning. While brushless motors are typically more than 50% efficient in terms of mechanical energy out compared to electrical energy in, they do suffer from loss of energy due to various factors such as wire heating, resistance, et cetera. Brushless motors require intricately wound electromagnetic rotor and/or stator magnets which are expensive and inefficient to construct. Electromagnets are also fairly heavy and contribute to parasitic load and/or weight inefficiency.
Historically, positional sensing was done by some external detection means, such as a switch or counter. This adds complexity and expense. Traditional electric motors can also be used to detect countermotion by a load or torque: if something moves the rotor of an electric motor, it will induce a current in the motor. (As is well known to persons of ordinary skill in the art, if you turn a motor, you create a generator.) The current can be detected and used to indicate that the motor is being turned. However, traditional motors do not provide fine enough creation and detection of such currents to precisely identify the position of the motor's rotor or elements affixed to the rotor of the motor. In many applications, such as robotics, it would be extremely useful to be able to precisely detect the position/motion of the rotor of a motor or the elements affixed to the rotor of the motor.
An electric motor with positional sensing which did not use electromagnets and therefore was more efficient and more economical to build would be a useful invention.
An electric motor with positional sensing which did not use electromagnets and was therefore more efficient and economical to power would be a useful invention.
An electric motor with positional sensing which did not use electromagnets and was therefore more durable and reliable would be a useful invention.
An electric motor with positional sensing which did not use electromagnets and was therefore lighter than a motor of equivalent output which did use electromagnets would be a useful invention.
An electric motor with positional sensing which did not require external detection means and produced a precise measurement of the position and/or motion of the motor would be a useful invention.
The present invention addresses these concerns.
Among the many objectives of the present invention is the provision of an electric motor with positional sensing which uses piezoelectric impulse and permanent magnets as a source of generating mechanical energy from electrical energy.
Another objective of the present invention is the provision of an electric motor with positional sensing which does not use electromagnets and is therefore more efficient and economical to construct.
Another objective of the present invention is the provision of an electric motor with positional sensing which does not use electromagnets and is therefore more efficient and economical to operate.
Yet another objective of the present invention is the provision of an electric motor with positional sensing which does not use electromagnets and is therefore more durable and easier to maintain.
Still another objective of the present invention is the provision of an electric motor with positional sensing which does not use electromagnets and is therefore lighter in weight than a traditional brushless electric motor of equivalent output.
The invention also provides an electric motor with positional sensing which does not require external detection means and produces a precise measurement of the position and/or motion of the motor.
Other advantages and objectives of the present invention will become clear by reading the application and the disclosures herein.
Reference will now be made in detail to several embodiments of the invention that are illustrated in accompanying drawings. Whenever possible, the same or similar reference numerals are used in the drawings and the description to refer to the same or like parts or steps. The drawings are in simplified form and are not to precise scale. For purposes of convenience and clarity only, directional terms such as top, bottom, left, right, up, down, over, above, below, beneath, rear, and front, can be used with respect to the drawings. These and similar directional terms are not to be construed to limit the scope of the invention in any manner. The words attach, connect, couple, and similar terms with their inflectional morphemes do not necessarily denote direct or intermediate connections, but can also include connections through mediate elements or devices.
It should be noted that the sizes and configurations of the preferred embodiment(s) described in the drawings are exaggerated for clarity of disclosure: in actual practice, the tolerances between the elements of embodiments of the invention would be much more precise. It is a feature of the invention that it allows such very precise tolerances.
For purposes of this invention, piezoelectric actuators are described as being “electrically connected” to a power supply. Such a connection can be made via physical conductors (wires, PCB conductive paths, conductive inks, et cetera) or by any other reasonable means that allows the power supply to supply energy to the piezoelectric actuators and causes the piezoelectric effect to change the dimensions of the piezoelectric actuators. This includes, but is not limited to, electromagnetic induction or transfer by capacitance. It is required that the means of electrical connection be able to switch the piezoelectric actuators on and off and/or apply a current flow in one direction and then in the other direction fast enough to allow the motor to operate, as will be made clear in the specification below. This will be referred to generally as “rise” time—the period of time it takes to energize the piezoelectric actuator and/or the capacitator powering it—and the “fall” time—the period of time it takes to deenergize the piezoelectric actuator and/or the capacitor powering it.
For purposes of this application, motors will generally have a group of components which remains static relative to a load, and a second group of components which will move relative to the first group of components. The first group of components will be referred to collectively as a stator assembly, and the second group referred to collectively as a rotor assembly. Prefixing a component with the word “rotor” or “stator” indicates which group of components it belongs to in the embodiment/configuration which is currently being described. Piezoelectric actuators in the stator assembly are stator piezoelectric actuators (or simply stator actuators) and magnets affixed to stator piezoelectric actuators are stator magnets, and vice versa with regard to the rotor assembly.
At the same time, for purposes of this application magnets can also be described as falling into one or both of two distinct types independent of whether they are part of the stator assembly or the rotor assembly. Actuator magnets are magnets which have/are having force imposed upon them by a piezoelectric actuator. Response magnets are magnets which have/are having force imposed upon them via magnetic field interactions with actuator magnets. If only one group of magnets is affixed to piezoelectric actuators, those are the actuator magnets, and the rest of the magnets in the motor are response magnets. If multiple groups of magnets are affixed to piezoelectric actuators, magnets affixed to a piezoelectric actuator which is being energized and causing it to impose force on those magnets are actuator magnets, and magnets which are not so affixed, or which are affixed to a piezoelectric actuator which is not being energized, are response magnets. It is possible for any given magnet to be an actuator magnet or a response magnet or both at any given time depending on the motor controller's configuration and energization of the piezoelectric actuators. A rotor magnet or a stator magnet may at any time be an actuator magnet, a response magnet, or both.
By referring to
Stator assembly 19 consists of central hub 18, which supports multiple stator piezoelectric actuators 17. Stator piezoelectric actuators 17 have a magnet mount end 17a and a hub end 17b. Stator piezoelectric actuators 17 are connected to a switching power supply (not shown) which can energize the stator piezoelectric actuators at any reasonable driving frequency. When the stator piezoelectric actuators are energized, they expand, using the principle of piezoelectric expansion, also known as the piezoelectric effect, which is well known to persons of ordinary skill in the art. Stator piezoelectric actuators 17 are constructed so that their expansion is along their long axes: in other words, when the stator piezoelectric actuators are energized, the distance between magnet mount end 17b and hub end 17a increases.
Mounted to magnet mount ends 17b are stator magnets 16, having stator north poles 16a and stator south poles 16b. Any suitable magnet may be used for stator magnets 16, including but not limited to rare-earth magnets, ferromagnets, and/or ceramic magnets containing ferromagnetic and/or rare-earth magnetic particles. Electromagnets may also be used. If electromagnets are used, it is optional, but neither preferred nor required, to allow them to reverse polarity as driven by a solid-state commutator of the type found in traditional brushless electric motors.
It is strongly preferred that the rotor magnets and the stator magnets have the same poles (north and north or south and south) in opposition at their closest points (as shown) but with proper configuration, it is possible to practice the invention with the rotor magnets and the stator magnets having opposite poles (north and south or south and north) in opposition. If opposite poles are put into opposition, the motor may require an external initiating force and/or the stator piezoelectric actuators may be required to be energized in a staggered sequence. If reversible electromagnets are used for either the rotor magnets, the stator magnets, or both, the question of initial polarities is unimportant.
The preferred embodiment pictured in
To practice the invention, stator piezoelectric actuators 17 are energized. This causes the distance between hub end 17b and magnet mount end 17a to increase, pushing stator magnet 16 closer to rotor magnet 15. This increases the magnetic repulsion between the rotor magnet and the stator magnet, disturbing the equilibrium between them. In the configuration shown, it may be necessary to impart a slight initial rotational force and/or to energize the stator piezoelectric actuators in sequence so as to asymmetrically disturb the equilibrium of magnetic forces and allow rotation to begin.
Once the equilibrium between the rotor magnets and the stator magnets is disturbed, the system will have more magnetic potential energy than before, which will cause the rotor magnets to exert a force on inner rotor 14. Inner rotor element 14 is free to rotate, so it will rotate in one direction or the other as impelled by the balance of forces. As will be shown in later figures, control of the shape and orientation of the rotor magnets and/or stator magnets will allow for a preferred direction of rotation.
The switching power supply is controlled by a frequency controller (not shown) which causes it to energize and de-energize stator piezoelectric actuators 17 at a frequency which will continue to convert magnetic potential energy into rotational energy and accelerate inner rotor element 14 in a rotational fashion. It is preferred, but not required, that sensors (not shown) be operably connected to the inner rotor element or otherwise be able to detect its angular velocity, and communicate it to the frequency controller such that the frequency controller can adjust the driving frequency to increase or decrease the force exerted by the stator magnets on the rotor magnets and thus either increase the speed of rotation (under constant load,) increase the applied torque (under increasing load,) or both.
To obtain the benefits of the positional sensing aspect of the invention, the frequency controller is connected to, or integrated with, a counting device, an induced current sensor, or both.
If a counting device is used, the frequency controller is connected to or integrated with the counting device (not shown,) which can detect each instance of a current being induced by the rotor magnets rotating past the stator magnets. The counting device could be as simple as a circuit in the frequency controller which can detect back-currents or it can be a more sophisticated separate device as is appropriate to the application in which the electric motor with positional sensing is being used.
Because the geometry of the rotor magnets and the stator magnets is known, the amount of rotational arc the motor, or any element attached to it, goes through each time the rotor magnets rotate past the stator magnets is also known. For instance, if the rotor magnet/stator magnet pairs each encompass an arc of 10 degrees (or π/18 radians) of the rotation of the motor, each instance of a current induction equals a rotation of 10 degrees (or π/18 radians). To obtain distance moved, the diameter of the circle described by the element whose position is to be measured is multiplied times the number of current inductions and hence the number of fractional rotations. In a device with a positional element located one meter from the center of the rotor, each current induction/movement of the rotor and stator magnets would equate to an angular movement of:
2*π*1 meter*10 degrees/360 degrees=π/16 meters (or ˜19.6 cm)
(Where 2*π*r is the formula for the circumference of a circle with radius r and the circle here has a radius of one meter.)
It is trivial to derive the angular velocity of the positional element once its angular motion is known: the amount of distance traveled in the prior step is simply divided by the time it took for the element to move that distance. If it took 0.1 seconds for the positional element in the prior example to move through an arc of 10 degrees (or π/18 radians) and thus move π/16 meters then the angular velocity would be:
π/16 meters/0.1 seconds=π/1.6 meters/second (or ˜1.96 m/s)
It is required that the counting device be able to keep track of the motion of the motor whether or not the piezoelectric actuators are being energized by the switching power supply in some fashion. It is strongly preferred, but not required, that the counting device be able to separately keep track of both the currents which are induced into the motor by the switching power supply (for causing the actuators to move the stator magnets and thus turn the rotor assembly) and currents which are induced into the motor by countermotion of the load or other elements attached to the rotor assembly which cause it to rotate by the imposition of an external torque. It is optional, but neither preferred nor required, for the frequency counter to interact with the counting device in such a way as to calibrate the number of current inductions the frequency controller has initiated with the number the counting device detects so that the counting device has a redundant source of information it can use to ensure that current inductions are being counted correctly.
If an induced current sensor is used, the frequency controller is connected to or integrated with the counting device (not shown,) which can dynamically detect the induced current of a current being induced by the rotor magnets rotating past the stator magnets. The induced current sensor can be as simple as a circuit in the frequency controller which can detect back-currents or it can be a more sophisticated separate device as is appropriate to the application in which the electric motor with positional sensing is being used.
To use the induced current sensor, the electric motor with positional sensing is operably connected to another motor or other device (hereafter the “calibration load”) which can rotate the electric motor with positional sensing without having to apply power to the piezoelectric actuators. It is strongly preferred to use the calibration load to rotate the rotor assembly, but depending on the needs of the particular application, it is optional to use the calibration load to rotate the stator assembly. Whichever of the rotor/stator assemblies is being rotated, it is required that the other either be held static or that its motion be somehow separately measured to allow for full calibration. The former is strongly preferred.
Once the calibration load is connected (for illustration the following will assume that the stator assembly and the rest of the motor as a whole is being held static and the rotor assembly is being rotated by the calibration load) it is used to accelerate the rotor assembly at a known rate until it is spinning at a known and fixed angular velocity. On a first calibration pass, the induced current sensor is used to dynamically track the current induced in the electric motor with positional sensing by the motion of the rotor magnets past the stator magnets. It is strongly preferred that the motor be rotated for several revolutions to obtain a good set of average values. Because no two of the rotor magnets and/or stator magnets will have exactly the same magnetic strength (this can be varied by design or the inevitable inconsistencies in manufacture can be used) the induced current sensor will track the current being induced as a variable periodic wave (the “base wave.”)
As the base wave will be unique, at sufficient precision of measurement, at each point in the rotation of the rotor assembly to any reasonable level, it can be used to map the magnetic field of the rotor magnets relative to the stator magnets. This data is stored for a later step in the process.
It is optional but strongly preferred to then repeat the calibration steps above with the piezoelectric actuators energized by the stepping power supply, creating measurements of another variable periodic wave, the “energized” wave. This can be done at any reasonable level of energization, but it is required that the calibration load have sufficient power to rotate the motor against the resulting (potentially) increased magnetic attraction/repulsion, especially if the motor starts out from a dead stop. As will be apparent to persons of ordinary skill in the art, the “back-current” which will be measured if the piezoelectric actuators are energized by the power supply will be the sum of the current being induced by the power supply and the current being induced by the calibration load, which will not be in phase, and the measurements must be used accordingly when using the energized wave in later steps.
It is optional to first spin up the motor with the frequency controller and then apply the calibration load with (and against) up to full energization of the piezoelectric actuators. This will create yet another variable periodic wave or waves (the base wave and all of the energized waves collectively the “waves.”) All of the waves should be quite similar to the base wave when adjusted for the current being supplied by the power supply, but will contain additional minute variations. This data is also stored for a later step in the process. It is optional, but not preferred, to use multiple levels of energization, or even to only used an energized level and not measure the base wave.
Once the waves are measured and the data stored, it is used to construct a map of the magnetic fields of the rotor and stator magnets (the “field map.”) To practice the invention using the induced current sensor, the motor is put into operation, and the point on the map of the magnetic fields where the rotor assembly is located is determined at a time or times when the position of the rotor is to be determined. This is known as “resolving” the motor or resolving the rotor position.
It is optional, but strongly preferred, to use some exterior sensor to measure any material external electromagnetic fields, variations in temperature, et cetera, which might affect the nature of the waves when using the positional sensing capability of the motor. While the relative positions of the rotor magnets and stator magnets should produce consistently shaped waves, the actual amplitude and frequency of the waves, and thus the precision of the positional sensing, will vary according to these and other factors which will be apparent to those of ordinary skill in the art.
Although the preferred embodiment is described as an electric motor with positional sensing, which is designed to convert electrical potential from a switching power supply into rotational energy, it will be apparent to persons of ordinary skill in the art that since the piezoelectric effect works both ways—electrical potential can be turned into mechanical force, and mechanical force can be turned into electrical potential—that the preferred embodiment can also serve as a generator of electrical power if an external load forces the inner rotor element to rotate against the magnetic force attempting to hold it in equilibrium. Similarly, the preferred embodiment can also be used as a drive motor which also provides regenerative braking by switching from power in (during drive mode) to power out (during regenerative braking mode.) All of the alternate configurations/embodiments/methods of practice described in this paragraph are applicable to all of the embodiments of the invention disclosed in this application.
Additional embodiments of the electric motor with positional sensing will now be described. All of the additional embodiments are alternate configurations of the physical motor itself: the principles by which each embodiment can be used as an electric motor with positional sensing is identical to that described above.
Electric motor with positional sensing 20 incorporates rotor piezoelectric actuators 27b, analogous to stator piezoelectric actuators 17 in
When either stator piezoelectric actuators 27a or rotor piezoelectric actuators 27b are energized, rotor magnets 25 are pushed toward stator magnets 26, and as in
Depending on the desired method of operation, the stator piezoelectric actuators can be activated in concert with the rotor piezoelectric actuators, or only one or the other group of piezoelectric actuators can be active at any given time. Activating both at once can be used to increase torque/rotational velocity, whereas activating only one or the other can be used for lower output modes. Alternatively, one group of piezoelectric actuators can be wired to deliver input power (motor driving) and the other group wired to receive output power (generation/regenerative braking.) The groups of piezoelectric actuators can also be wired such that some of the actuators in each group are preferentially used to deliver input power and some are preferentially used to receive output power. Finally, all or fewer than all of the piezoelectric actuators in a particular group can be active at any given time to deliver any particular desired amount of input power or receive any particular desired amount of output power, allowing an additional means of controlling power flow and/or reducing electrical fatigue on the individual components as they are cycled in and out of service.
Electric motor with positional sensing 60 comprises rotor assembly 614 and stator assembly 618. Rotably affixing the rotor assembly to the stator assembly is bearing 652 which rotates around central point 611. Mechanically affixed to bearing 652 are one or more stator piezoelectric elements. Shown is a configuration with six such stator piezoelectric elements including stator piezoelectric element 619. Mechanically affixed to the stator piezoelectric elements are stator magnet elements such as stator magnet element 640. The stator magnet elements comprise one or more magnets having a north pole and a south pole, such as stator magnet 617 having stator magnet north pole 617a and stator magnet south pole 617b. There is a gap between the stator magnet elements and one or more rotor magnet elements. Shown is a configuration with six such rotor magnet elements including rotor magnet element 642. Each rotor magnet element includes one or more rotor magnets such as rotor magnet 616, which has rotor magnet north pole 616a and rotor magnet south pole 616b.
To practice the invention, as with prior described embodiments, one or more of the stator piezoelectric actuators, such as stator piezoelectric actuator 619, is energized by a switching power supply (NOT SHOWN) controlled by a frequency controller (NOT SHOWN) such that when, for example, stator piezoelectric actuator 619 is energized, it expands along axis of expansion 619a, causing the corresponding stator magnet element to get closer to one or more rotor magnet elements. This produces a change in the orientation of the magnetic fields of the stator and rotor magnetic elements, causing the corresponding stator magnetic element to exert a force on the rotor magnetic element which in turn causes the rotor magnet element to exert a force on the housing 612, causing it, along with the entire rotor assembly 614 to rotate around central point 611 on bearing 652 relative to stator assembly 618. This rotational force is transmitted to an external load via hollow shaft 632 (NOT SHOWN, see
It is not required that each rotor magnet element be exactly geometrically opposed to a stator magnet element at any particular time during operation or non-operation and in fact it is likely that the equilibrium during non-operation will result in some degree of offset. It is strongly preferred that there be a rotor magnet element for each stator magnet element, and vice versa. It is required that there be a gap between the rotor magnet elements and the stator magnet elements sufficient to allow the rotor magnet elements to move freely without contacting the stator magnet elements under any reasonable amount of bearing load, rotary speed, or transient vibratory load.
Although the configuration of magnets shown will be inherently stable due to magnetic attraction between the individual magnets, it is preferred that the magnets in each rotor magnet element and stator magnet element be epoxied or otherwise physically affixed to each other to maintain the desired alignment and prevent shifting under load or due to vibration or other transient phenomena.
It is strongly preferred, but not required, to use an overlapping configuration of magnets as shown in the rotor magnet elements and the stator magnet elements as this will minimize asymmetries in the overall magnetic field structure in the brushless magnetic motor.
For purposes of this description, it is assumed that base element 682 is secured to something which is designated as static and therefore base element 682 forms part of a stator assembly. For example, if motor 60 were to be used to drive the wheel of an electric vehicle, base element 682 would ultimately be statically affixed to the chassis of the vehicle, whereas housing 612 would ultimately be statically affixed to the wheel of the vehicle.
Capacitor array 680, which does not rotate relative to the stator assembly, includes capacitor plates such as capacitor plate 658, each capacitor plate separated by a gap such as capacitor gaps 657a and 657b. Capacitor array energizes rotor piezoelectric array 621, which includes one or more rotor piezoelectric actuators such as rotor piezoelectric actuator 621. The rotor piezoelectric actuators are mechanically affixed to one or more (optional) rotor magnet brackets 678, each rotor magnet bracket having a rotor circumferential surface 662, and (optional) rotor vertical guides 661a and 661b, with all of the rotor magnet brackets forming rotor magnet bracket assembly 660. Mechanically affixed to the rotor piezoelectric actuators, either directly or via the (optional) rotor magnet brackets, are one or more rotor magnet elements such as rotor magnet element 642, each rotor magnet element comprising one or more rotor magnets such as rotor magnet 616, with all of the rotor magnet elements forming rotor magnet assembly 672.
When energized, the rotor piezoelectric actuators expand toward the center of motor 60 (since they cannot expand against the fixed position of the rest of the rotor assembly including ultimately housing 612) pushing the rotor magnet elements toward the stator magnet elements (see below) and imparting a magnetic force as explained in previous descriptions (see
Rotor magnet assembly 672 radially surrounds stator magnet assembly 670, the rotor magnet assembly separated from the stator magnet assembly by a gap (NOT SHOWN, see
When energized, the stator piezoelectric actuators expand toward the outer circumference of motor 60 (since they cannot expand toward the fixed position of the rest of the stator assembly) pushing the stator magnet elements toward the rotor magnet elements and imparting a magnetic force as explained in previous descriptions (see
Electric motor with positional sensing 80 comprises rotor assembly 82, stator magnet assemblies 84 and 87, and piezoelectric actuator 810 which is operably affixed to PCB 92 (NOT SHOWN: See
If necessary, fluid can be forcibly circulated around the assemblies or even through the gap to cool the motor, but as many piezoelectric devices actually work better when they reach a relatively high operating temperature, the need for cooling will be minimal in many applications. This is another advantage of the invention. It is required that for all embodiments and configurations of the invention, that operating temperatures be kept low enough to avoid demagnetization of any permanent magnets which are used. This will vary as various kinds of magnetic material have different demagnetization thresholds. (For example, some ferrite magnets can tolerate temperatures up to 250° C., whereas some rare-earth magnets can only tolerate temperatures up to 100° C.)
To practice this embodiment of the invention, an electrical potential is put across piezoelectric actuator 810, which is electrically connected to PCB 92. This causes piezoelectric actuator 810 to expand along its long axis, changing the relative position of the stator magnet assemblies and the rotor assembly. This in turn causes electromagnetic force to be exerted on the rotor assembly, which will rotate to a position which will minimize the magnetic potential energy between the rotor assembly and the stator assemblies. The electrical potential across piezoelectric actuator 810, is then removed and/or reversed, causing it to contract along its long axis, again changing the relative position of the various magnet assemblies, and imparting more rotational energy to the rotor assembly. A switching power supply (NOT SHOWN) continuously cycles the electrical potential across the piezoelectric actuator to produce the desired rotational energy as in earlier described embodiments.
It is optional, but neither preferred nor required, for either the rotor assembly or the stator assembly, or both, to comprise multiple magnets as in earlier described configurations. (See
Alternate configurations of the invention, which can be applied to any of the described embodiments, will now be disclosed.
In a first alternate configuration of the invention (NOT SHOWN) some or all of the rotor magnets, or some or all of the stator magnets, of either the preferred embodiment or the first alternate embodiment are replaced with electromagnets.
In a second alternate configuration of the invention (NOT SHOWN) one or more elastic members is fitted into the motor assembly such that the piezoelectric actuators are working against the elastic members when they are energized, compressing them and creating elastic potential energy, so that when the piezoelectric actuator(s) is/are de-energized, the magnet(s) affixed to the piezoelectric actuator(s) return to their prior position more quickly and without the need to impose a reverse polarity potential across the piezoelectric actuator when the elastic potential energy provides impetus to the piezoelectric actuators.
In a third alternate configuration of the invention (NOT SHOWN) the features of the first and second configurations are combined.
It will be apparent to those of ordinary skill in the art that while the invention and its preferred embodiments are described in terms of rotary motors, the principles taught by the invention can be used to create linear motors, such as reciprocating motors, by using the basic principle of piezoelectric motivation of opposing magnetic elements to create a linear force instead of a centripetal force. Thus, the claims below include both rotary configurations and linear configurations where and as appropriate.
While various embodiments and configurations of the present invention have been described above, it should be understood that they have been presented by way of example only, and not limitation. Thus, the breadth and scope of the present invention should not be limited by any of the above exemplary embodiments.
This application—taken as a whole with the abstract, specification, and drawings being combined—provides sufficient information for a person having ordinary skill in the art to practice the invention as disclosed herein. Any measures necessary to practice this invention are well within the skill of a person having ordinary skill in this art after that person has made a careful study of this disclosure.
Because of this disclosure and solely because of this disclosure, modification of this device and method can become clear to a person having ordinary skill in this particular art. Such modifications are clearly covered by this disclosure.
This application claims priority to U.S. patent application Ser. No. 16/941,477, “BRUSHLESS ELECTRIC MOTOR,” filed Jul. 28, 2020, in the United States Patent and Trademark Office, said application by the same inventive entity, with the entirety of said application being incorporated herein by reference to provide continuity of disclosure. This invention relates to a new type of electronic motor with a position sensor which uses piezoelectric elements to detect the interaction of permanent magnets or electromagnets. The sensor is integrated into a brushless electric motor design. Novel configurations of permanent magnets allow the motor assembly to deliver large amounts of torque while remaining stable at load and over long operating times but still delivering extremely precise and reliable sensor position information.
| Number | Date | Country | |
|---|---|---|---|
| Parent | 16941477 | Jul 2020 | US |
| Child | 17501424 | US |
