Ultrahigh-voltage brushless aviation motor

Abstract

The invention relates to an ultra-high-voltage brushless aviation motor, which belongs to the field of ultra-high-voltage motors, and comprises a permanent magnet electrode plate, an electrode plate, an insulating rotor, a rotating shaft, an insulating stator and a base, the permanent magnet is a medium positive and negative charge rotor electrode plate with permanent property, and charges of the stator electrode plate are connected through a boosting module; by controlling the voltage of the variable electrodes, the electric field converted between the electrodes and the repulsion and attraction between different charges through multiple circuit triodes, electric energy is converted into kinetic energy through the rotor, the problems that in the prior art, a motor structure is light in weight, the energy consumption problem is solved, existing large-current overload heat loss is caused are solved, and the motor is used for power of the light unmanned aerial vehicle.

Description

Technical Field

[0001] The present invention relates to the field of aviation motors, and in particular to an ultra-high voltage brushless motor. Background Art

[0002] The brushless motors currently used in drones are all low-voltage motors with high-current power loads. From the perspective of power efficiency, the greater the current, the greater the heat generated by the load, and the greater the useless power loss.

[0003] Structurally, the permanent magnets of the brushless motor serve as the magnetic poles of the rotor or stator, and the copper coils are wound on the silicon steel material as the control magnetic poles of the rotor or stator. These are high-density materials, and the weight is proportional to the power. As the power increases, the weight also increases structurally. In the aviation field, the heavier the weight, the lower the aviation load efficiency, especially for micro UAVs. Reducing one gram of aircraft weight is equivalent to the cost-effectiveness of one gram of gold. In comparison, this motor cannot meet higher efficiency requirements. Summary of the invention

[0004] The present invention provides an ultra-high voltage brushless aviation motor, which is characterized by comprising a permanent electric body electrode sheet, an electrode sheet, an insulating rotor, a rotating shaft, an insulating stator, and a machine base. A plurality of permanent electric body electrode sheets are arranged on the inner wall of the insulating rotor and pasted with high-temperature insulating silicone, and are arranged in a circular pattern at intervals. A plurality of electrode sheets are arranged on the outer ring of the insulating stator and pasted with high-temperature insulating silicone, and are arranged in a circular pattern at intervals. The same-charge electric field electrode sheets repel the same-charge permanent electric bodies, and the opposite-charge electric field electrode sheets attract the opposite-charge permanent electric body electrode sheets. The electric field energy of the insulating stator is converted into the kinetic energy of the insulating rotor.

[0005] The electrode sheet is provided with a positive electrode sheet and a negative electrode sheet electrically connected to a circuit for converting positive and negative voltages of multiple power supply inputs, and a triode is provided to control the change of positive and negative voltages.

[0006] The permanent electricity electrode sheet is made of dielectric material, and is charged with positive and negative charges via a high voltage device to obtain a single-charge permanent electricity electrode.

[0007] It is further configured that the inner hole of the cover at one end of the insulating rotor is passed through a rotating shaft for fixed connection, and the rotating shaft passes through an inner hole of the insulating stator and is rotatably connected with a retaining spring of a bearing hole of a machine base.

[0008] It is further configured that the screws pass through the insulating stator to be provided with a plurality of mounting holes and are screwed to be connected with the screw holes of the machine base.

[0009] The beneficial progress made by the existing brushless low-voltage motor is different from the working principle. From the electric power formula, we know that W=UI. Under the same power, the voltage increases and the current decreases proportionally. The smaller the overload current of the motor, the smaller the power loss. At the same time, the existing motor material is the electromagnetic core of silicon steel sheet and copper wire electromagnetic coil, as well as permanent magnet. The thin sheets of different permanent magnets and electrodes are light in weight. BRIEF DESCRIPTION OF THE DRAWINGS

[0010] In order to more clearly illustrate the embodiments of the present invention or the existing technical solutions, a brief introduction to the drawings required for the description is given.

[0011] Figure 1 It is a perspective three-dimensional structural diagram of the present invention.

[0012] Figure 2 It is the exploded structural diagram of the assembly position of the present invention.

[0013] Figure 3 This is a diagram of the stator electrode control structure of the present invention.

[0014] Figure 4 This is a structural diagram of the stator electrode of the present invention.

[0015] Figure 5 This is a diagram of the rotor electrode structure of the present invention.

[0016] In the figure, it includes a permanent electric body electrode sheet (1), a negative charge permanent electric body (101), a positive charge permanent electric body (102) electrode sheet (2), a positive electrode sheet (201), a negative electrode sheet (202), an insulating rotor (3), an insulating rotor cover shaft hole (301), a rotating shaft (4), a rotating shaft retaining ring groove (401), an insulating stator (5), a stator mounting hole (501), a stator shaft hole (502), a stator screw (503), a machine base (6), a screw hole (601), a mounting hole (602), and a bearing hole (603). DETAILED DESCRIPTION

[0017] The technical solutions in the embodiments of the present invention will be described clearly and completely below in conjunction with the drawings in the embodiments of the present invention. Obviously, the described embodiments are only a part of the embodiments of the present invention, rather than all of the embodiments. In the description of the present invention, it should be understood that the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "up", "down", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inside", "outside", "clockwise", "counterclockwise" and the like indicate positions or positional relationships based on the positions or positional relationships shown in the drawings, and are only for the convenience of describing the present invention and simplifying the description, rather than indicating or implying that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore cannot be understood as limiting the present invention.

[0018] See also Figure 1 The overall structure of the ultra-high voltage brushless aviation motor assembly, Figure 2 The ultra-high voltage brushless aviation motor shown in the figure comprises a permanent electrode sheet (1), an electrode sheet (2), an insulating rotor (3), a rotating shaft (4), an insulating stator (5), and a machine base (6). The insulating rotor (3) is tightly connected to the rotating shaft (4). The rotating shaft (4) is sleeved in a stator shaft hole (502) of the insulating stator (5) so that the bearing can move and the retaining spring can limit the position.

[0019] Figure 5 As shown, a plurality of permanent electric body electrode sheets (1) are provided, which are respectively negative charge permanent electric bodies (101) and positive charge permanent electric bodies (102), and are placed on the inner wall of the insulating rotor (3) and pasted with high-temperature insulating silicone rubber, and are arranged in a circular pattern at intervals. The insulating rotor (3) is an insulating, high-strength, lightweight composite material. An end cover of the insulating rotor (3) is provided with an insulating rotor cover shaft hole (301), and the rotating shaft (4) is sleeved in the insulating rotor cover shaft hole (301) and is tightly connected.

[0020] Figure 4 The multiple electrode sheets (2) shown in the figure are respectively a positive electrode sheet (201) and a negative electrode sheet (202) which are placed on the outer ring of the insulating stator (5) and pasted with high-temperature insulating silicone and arranged in a circular pattern at intervals. The insulating stator (5) is an insulating, high-strength, lightweight composite material. The insulating stator (5) is provided with a sub-mounting hole (501) and a stator shaft hole (502). The electric field electrode sheets (2) with the same charge and the permanent electric body (1) with the same charge repel each other, and the electric field electrode sheets (2) with different charges and the permanent electric body electrode sheets (1) with different charges attract each other. The electric field energy of the insulating stator (5) is converted into kinetic energy of the insulating rotor (3).

[0021] Figure 3 As shown, the electrode sheet (2) is provided with a positive electrode sheet (201) and a negative electrode sheet (202) electrically connected to a circuit for converting positive and negative voltages of multiple power inputs, and a triode is provided to control the change of positive and negative voltages. The triode can be an ordinary triode, a triode MOS tube, or a triode IGBT tube. Figure 3 The control part S1 and S2 are configured as control electrodes electrically connected to a frequency-adjustable control module, and the high and low level switching frequencies control the collector and emitter conduction frequencies, thereby achieving frequency changes of the positive electrode sheet (201) and the negative electrode sheet (202).

[0022] The existing power supply voltage standard is divided into 1000 volts, which is the range of low-voltage brushless motors. 300 kV to 1000 kV is ultra-high voltage, and more than 1000 kV is ultra-high voltage. This voltage standard is applied to power grid transmission and has been widely used. The boost module can reach the range of ultra-high voltage and ultra-high voltage, and both ultra-high voltage and ultra-high voltage can supply power to the electrode.

[0023] Figure 5 As shown, the permanent body electrode sheet (1) is a dielectric material, and a single-charge permanent body electrode is obtained. Our common permanent magnets are made of composite neodymium iron boron dielectric materials. After passing through a charging magnetic field, a stable magnet is formed. Similarly, the common dielectric of permanent bodies is rosin, palm wax, and beeswax as raw materials. After passing through a high-voltage positive and negative charge device and a charging field, a stable single permanent body is formed, a negatively charged permanent body (101) or a positively charged permanent body (102).

[0024] Figure 4 As shown, one end of the insulating rotor (3) is covered with an insulating rotor cover shaft hole (301), which is passed through the rotating shaft (4) for fixed connection, and the rotating shaft (4) is passed through the inner hole of the insulating stator shaft hole (502) and is connected to the base bearing hole (603) by a retaining spring for limited rotation. The stator screw (503) passes through the insulating stator mounting hole (501) and is provided with a plurality of mounting holes, which are screwed and connected to the base screw hole (601), and the mounting hole (602) is a hole reserved for the fuselage of the drone.

[0025] Working process and principle control; Common power sources for low-voltage brushless motors are two-phase, three-phase, and four-phase, which are determined by the different winding methods of the stator coils inside. Similarly, the charge electrode spacing of high-voltage brushless motors is different, and the power supply can be two-phase, three-phase, or four-phase control connected in series, or in series. The power supply control method is to convert the electrodes of the transistor. Low-voltage brushless motors use the repulsion and adsorption force of the permanent magnetic field to complete the conversion of electrical energy into kinetic energy, while high-voltage brushless motors use the repulsion and adsorption force of the permanent electric field to complete the conversion of electrical energy into kinetic energy. Under the premise that the power of the two is the same, the current of the high-voltage brushless motor is low, the loss of overload current is very small, and the temperature is low, thereby achieving energy saving.

[0026] Although the present invention has been described in detail with reference to the aforementioned embodiments, it is still possible for those skilled in the art to modify the technical solutions described in the aforementioned embodiments, or to make equivalent substitutions for some of the technical features therein. Any modifications, equivalent substitutions, improvements, etc. made within the spirit and principles of the present invention should be included in the protection scope of the present invention.

Claims

1. Ultra-high voltage brushless aviation motor, characterized by It comprises a permanent electric body electrode sheet (1), an electrode sheet (2), an insulating rotor (3), a rotating shaft (4), an insulating stator (5), and a machine base (6), wherein a plurality of permanent electric body electrode sheets (1) are arranged on the inner wall of the insulating rotor (3) and pasted with high-temperature insulating silicone rubber, and are arranged in a circular pattern at intervals; a plurality of electrode sheets (2) are arranged on the outer ring of the insulating stator (5) and pasted with high-temperature insulating silicone rubber, and are arranged in a circular pattern at intervals; the same-charge electric field electrode sheets (2) and the same-charge permanent electric body (1) repel each other, and the opposite-charge electric field electrode sheets (2) and the opposite-charge permanent electric body electrode sheets (1) attract each other, and the electric field energy of the insulating stator (5) is converted into kinetic energy of the insulating rotor (3); The electrode sheet (2) is provided with a positive electrode sheet (201) and a negative electrode sheet (202) electrically connected to a circuit for converting positive and negative voltages of multiple power supply inputs, and is provided with a triode to control the change of positive and negative voltages; The permanent electric body electrode sheet (1) is a dielectric material, and is subjected to a high-voltage positive and negative charge charging device to obtain a single-charge permanent electric body electrode.

2. According to claim 1, the ultra-high voltage brushless aviation motor is characterized in that: The inner hole of the cover at one end of the insulating rotor (3) passes through the rotating shaft (4) for fixed connection, and the rotating shaft (4) passes through the inner hole of the insulating stator (5) and is rotatably connected to the bearing hole of the base (6) by a retaining spring.

3. According to claim 1, the ultra-high voltage brushless aviation motor is characterized in that: The screws (203) pass through a plurality of mounting holes provided on the insulating stator (5) and are screwed to the screw holes of the machine base (6) for connection.

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