CN106976560B - Unmanned aerial vehicle motor seat, unmanned aerial vehicle drive arrangement and unmanned aerial vehicle - Google Patents
Unmanned aerial vehicle motor seat, unmanned aerial vehicle drive arrangement and unmanned aerial vehicle Download PDFInfo
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- CN106976560B CN106976560B CN201710317118.0A CN201710317118A CN106976560B CN 106976560 B CN106976560 B CN 106976560B CN 201710317118 A CN201710317118 A CN 201710317118A CN 106976560 B CN106976560 B CN 106976560B
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- aerial vehicle
- permanent magnet
- electromagnetic coil
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- 230000007246 mechanism Effects 0.000 claims abstract description 31
- 238000013016 damping Methods 0.000 claims abstract description 17
- 230000008859 change Effects 0.000 claims abstract description 16
- 239000000725 suspension Substances 0.000 claims abstract description 14
- 230000005389 magnetism Effects 0.000 claims abstract description 9
- 239000011159 matrix material Substances 0.000 claims description 3
- 230000000694 effects Effects 0.000 abstract description 13
- 238000006073 displacement reaction Methods 0.000 abstract description 9
- 238000000034 method Methods 0.000 description 5
- 230000008569 process Effects 0.000 description 5
- 230000000630 rising effect Effects 0.000 description 5
- 238000010586 diagram Methods 0.000 description 4
- 230000007717 exclusion Effects 0.000 description 4
- 238000004891 communication Methods 0.000 description 2
- 238000004880 explosion Methods 0.000 description 2
- 230000001174 ascending effect Effects 0.000 description 1
- 230000004888 barrier function Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000012937 correction Methods 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 239000013013 elastic material Substances 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 230000001788 irregular Effects 0.000 description 1
- 238000005339 levitation Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- 230000000087 stabilizing effect Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 230000035899 viability Effects 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/12—Rotor drives
- B64C27/14—Direct drive between power plant and rotor hub
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- B64D27/40—
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Apparatuses For Generation Of Mechanical Vibrations (AREA)
Abstract
The invention provides an unmanned aerial vehicle motor, an unmanned aerial vehicle driving device and an unmanned aerial vehicle, which comprise a motor base body and a magnetic suspension damping mechanism; the magnetic suspension damping mechanism comprises a permanent magnet, an electromagnetic coil and at least one Hall sensor; the permanent magnet is used for being connected with the motor; the electromagnetic coil and the Hall sensor are arranged on the motor base body; the hall sensor is provided corresponding to the permanent magnet and is used for generating an electric signal for adjusting the magnetism of the electromagnetic coil according to the magnetic field change of the permanent magnet. In the technical scheme, the electromagnetic coil can adjust the magnetism of the electromagnetic coil according to the electric signal, so that the magnetism changes along with the displacement change of the permanent magnet, the effect of repulsion or attraction with the magnetism of the permanent magnet is generated, and the vibration of the motor is relieved in a magnetic suspension mode and transmitted to the machine body.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle motor base, an unmanned aerial vehicle driving device and an unmanned aerial vehicle.
Background
The unmanned plane is called as unmanned plane for short, and is a unmanned plane operated by radio remote control equipment and a self-contained program control device.
The unmanned aerial vehicle has no cockpit on the fuselage, but is provided with an automatic pilot, a program control device and other devices. Personnel on the ground, ships or on a mother machine remote control station track, position, remote control, telemetere and digital transmission through radar and other equipment.
The unmanned aerial vehicle can take off like a common airplane under radio remote control or launch and lift off by using a booster rocket, and can also be brought into the air by a host machine to put in flight. When recovered, the aircraft can automatically land in the same way as the landing process of a common aircraft, and can also be recovered by a parachute or a barrier net for remote control.
Compared with manned aircraft, it has the advantages of small size, low cost, convenient use, low requirement on battle environment, strong battlefield viability, etc., and is favored by army in various countries of the world. In several local wars, the unmanned plane plays a remarkable role in various combat capabilities such as accurate, efficient and convenient reconnaissance, interference, deception, searching, shooting correction, combat under the irregular condition and the like, and induces researches on related problems such as infinite military academia, equipment technology and the like. The unmanned plane can be repeatedly used for a plurality of times, has high flexibility, and is widely used for air reconnaissance, monitoring, communication, anti-diving, electronic interference and the like.
Many rotor unmanned aerial vehicle is one of them unmanned aerial vehicle promptly, and at present, current many rotor unmanned aerial vehicle can produce great vibrations when the operation, and the vibrations of motor just arouse one of them vibroseis of this kind of vibrations, and in the common unmanned aerial vehicle structure, the motor is the connected mode of hard hookup with the fuselage, and this kind of traditional hookup mode can be conducted the vibrations that the motor produced to the fuselage, makes unmanned aerial vehicle take place violently vibrations, influences flight stability.
Disclosure of Invention
The invention aims to provide an unmanned aerial vehicle motor, an unmanned aerial vehicle driving device and an unmanned aerial vehicle, so as to solve the technical problem that vibration generated by a motor can be transmitted to a machine body in a hard-connection mode in the prior art, and the unmanned aerial vehicle can generate severe vibration.
The invention provides an unmanned aerial vehicle motor, which comprises a motor seat body and a magnetic suspension damping mechanism, wherein the motor seat body is provided with a magnetic suspension damping mechanism;
the magnetic suspension damping mechanism comprises a permanent magnet, an electromagnetic coil and at least one Hall sensor; the permanent magnet is used for being connected with the motor;
the electromagnetic coil and the Hall sensor are connected with the motor base body; the Hall sensor is arranged corresponding to the permanent magnet and is used for generating an electric signal for adjusting the magnetism of the electromagnetic coil according to the magnetic field change of the permanent magnet.
In the above specific embodiment, after the motor starts to rotate, a lift force is obtained through rotation of the rotor, so that the permanent magnet is driven to rise together by rising of the motor, so that the permanent magnet generates displacement, and at the moment, the hall sensor senses a change of a surrounding magnetic field, that is, senses a change of displacement of the permanent magnet, so that the hall sensor transmits an electric signal formed by the change of displacement to the electromagnetic coil, and the electromagnetic coil adjusts magnetism of the electromagnetic coil according to the electric signal, so that the magnetism changes along with the change of displacement of the permanent magnet, and an effect that the magnetic force can repel or attract the permanent magnet is generated; therefore, the motor base can be driven to integrally lift up together with the unmanned aerial vehicle by utilizing the generated attractive magnetic force effect.
Meanwhile, in the ascending process, the unmanned aerial vehicle can also receive the change of gravity, so the Hall sensor can acquire the magnetic field change of the permanent magnet constantly and feed back to the electromagnetic coil, so that the magnetic repulsion or attraction is alternately generated between the electromagnetic coil and the permanent magnet in the flying process of the unmanned aerial vehicle, a magnetic suspension effect is formed, and vibration generated by the motor can be effectively relieved through the magnetic suspension mode.
Further, in an embodiment of the present invention, the connection between the hall sensor and the motor base body includes:
the Hall sensor is arranged on the side wall of the motor base body.
Further, in an embodiment of the present invention, the connection between the electromagnetic coil and the motor base body includes:
the motor cabinet body is provided with an annular groove, and the electromagnetic coil is arranged in the annular groove.
Further, in an embodiment of the present invention, a snap mechanism is further included; the clamping mechanism comprises a clamping buckle and a clamping part which are arranged on the motor base body;
one end of the buckle is hinged to one side of the annular groove, and the clamping part is arranged on the other side of the annular groove.
In the above specific embodiment, the locking engagement of the locking buckle and the locking portion may conveniently lock the electromagnetic coil in the annular groove, so that the electromagnetic coil may be more stably disposed in the annular groove and does not fall out; and simultaneously, the electromagnetic coil is conveniently taken out.
Further, in the embodiment of the invention, the motor damping mechanism is further included; the motor damping mechanism comprises a motor fixing sleeve, a motor fixing shell and at least two elastic pieces;
the motor is fixed in the motor fixing sleeve, the motor fixing sleeve is arranged in the motor fixing shell, and the motor fixing shell is elastically connected with the motor fixing sleeve through the elastic piece.
In the above-mentioned a specific embodiment, when unmanned aerial vehicle flies, the vibrations of motor can further alleviate through damper, further improvement stable effect on magnetic suspension damper's basis.
Further, in an embodiment of the present invention, connecting pieces are provided at both ends of the elastic member, and the elastic member is connected to the motor fixing sleeve and the motor fixing case through the connecting pieces provided at both ends.
Further, in an embodiment of the present invention, the motor base body includes any one of a cylindrical structure, a truncated cone structure, a square structure, and a prismatic table structure.
Further, in an embodiment of the present invention, three hall sensors are provided, and the three hall sensors are disposed on a side wall of the motor base body in an annular matrix.
The application also provides an unmanned aerial vehicle driving device, which comprises a motor and the unmanned aerial vehicle motor seat;
the permanent magnet of the unmanned aerial vehicle motor seat is fixedly arranged with the output end of the motor.
The application also provides an unmanned aerial vehicle, which comprises an unmanned aerial vehicle body, a horn, a rotor wing and the unmanned aerial vehicle driving device;
the unmanned aerial vehicle body passes through the horn with unmanned aerial vehicle drive arrangement is connected, the rotor passes through unmanned aerial vehicle drive arrangement drive rotation.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings that are needed in the description of the embodiments or the prior art will be briefly described, and it is obvious that the drawings in the description below are some embodiments of the present invention, and other drawings can be obtained according to the drawings without inventive effort for a person skilled in the art.
Fig. 1 is an exploded view of a base of a unmanned aerial vehicle according to an embodiment of the present invention;
FIG. 2 is a schematic plan view of a portion of a motor of a unmanned aerial vehicle according to an embodiment of the present invention;
fig. 3 is a schematic plan view of a motor base of the unmanned aerial vehicle according to an embodiment of the present invention;
fig. 4 is an exploded schematic view of a driving device of an unmanned aerial vehicle according to an embodiment of the present invention;
fig. 5 is a second schematic explosion diagram of the unmanned aerial vehicle driving device according to an embodiment of the present invention;
FIG. 6 is a schematic perspective view of a motor damper mechanism according to an embodiment of the present invention;
FIG. 7 is a schematic plan view of a motor damper mechanism according to an embodiment of the present invention;
fig. 8 is a schematic structural diagram of a fastening mechanism according to an embodiment of the present invention.
Reference numerals:
0-motor; 1-a motor base body; 2-a magnetic suspension damping mechanism;
3-a snap-fit mechanism; 4-a motor damping mechanism;
11-an annular groove;
21-permanent magnets; 22-electromagnetic coils; a 23-hall sensor;
31-a buckle; 32-an engagement portion;
41-a motor fixing sleeve; 42-a motor fixing case; 43-elastic member; 44-connecting piece.
Detailed Description
The following description of the embodiments of the present invention will be made apparent and fully in view of the accompanying drawings, in which some, but not all embodiments of the invention are shown. All other embodiments, which can be made by those skilled in the art based on the embodiments of the invention without making any inventive effort, are intended to be within the scope of the invention.
In the description of the present invention, it should be noted that the directions or positional relationships indicated by the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", etc. are based on the directions or positional relationships shown in the drawings, are merely for convenience of describing the present invention and simplifying the description, and do not indicate or imply that the devices or elements referred to must have a specific orientation, be configured and operated in a specific orientation, and thus should not be construed as limiting the present invention.
In the description of the present invention, it should be noted that, unless explicitly specified and limited otherwise, the terms "mounted," "connected," and "connected" are to be construed broadly, and may be either fixedly connected, detachably connected, or integrally connected, for example; can be mechanically or electrically connected; can be directly connected or indirectly connected through an intermediate medium, and can be communication between two elements. The specific meaning of the above terms in the present invention will be understood in specific cases by those of ordinary skill in the art.
Fig. 1 is an exploded view of a motor 0 seat of an unmanned aerial vehicle according to an embodiment of the present invention; fig. 2 is a schematic plan view of a motor 0 seat of an unmanned aerial vehicle according to an embodiment of the present invention; fig. 3 is a schematic plan view of a motor 0 seat of an unmanned aerial vehicle according to an embodiment of the present invention; fig. 4 is an exploded schematic view of a driving device for an unmanned aerial vehicle according to an embodiment of the present invention.
As shown in fig. 1 to 4, the unmanned aerial vehicle motor 0 seat provided in this embodiment includes a motor seat body 1 and also includes a magnetic suspension damping mechanism 2.
As shown in fig. 1 or 2 or 3 or 4, the magnetic suspension damping mechanism 2 includes a permanent magnet 21, an electromagnetic coil 22, and at least one hall sensor 23; the permanent magnet 21 is used for being connected with the motor 0; when the motor 0 rotates, a lifting force is obtained through the rotation of the rotor, so that the permanent magnet 21 is driven to rise along with the motor 0 by the rising of the motor 0, and the surrounding magnetic field is changed due to the displacement change of the permanent magnet 21 caused by the rising.
The permanent magnet 21 is preferably fixedly connected with the motor 0, so that the flying stability of the unmanned aerial vehicle can be ensured.
In addition, the connection between the permanent magnet 21 and the motor 0 is not limited to the above-described fixed connection, and may be a detachable connection such as a hinge connection, a snap connection, or a screw connection. This application provides only limited examples, and any technical solution based on this application should be included in the protection scope of this application without obtaining inventive work.
With continued reference to fig. 1-4, the electromagnetic coil 22 and the hall sensor 23 are disposed on the motor base body 1; the hall sensor 23 is provided corresponding to the permanent magnet 21, so that the hall sensor 23 can sense a change in magnetic field generated by displacement of the permanent magnet 21 due to the driving of the motor 0.
At this time, the hall sensor 23 generates an electric signal for adjusting the magnetism of the electromagnetic coil 22 according to the magnetic field change of the permanent magnet 21, and when the electromagnetic coil 22 senses such an electric signal, the magnetic field change around the electromagnetic coil 22 is adjusted according to the electric signal, thereby generating a magnetic field corresponding to the magnetic field generated by the permanent magnet 21 in real time.
The magnetic field changes generated by the permanent magnet 21 and the electromagnetic coil 22 correspond to each other, so that the electromagnetic coil 22 and the permanent magnet 21 are mutually exclusive or attracted to each other.
The mutual exclusion or mutual attraction effect not only can enable the permanent magnet 21 to be magnetically connected with the electromagnetic coil 22 so that the whole body of the unmanned aerial vehicle is driven to rise by the lifting force of the motor 0 and the rotor wing, but also can slow down the vibration generated by the motor 0 through the alternating mutual exclusion or mutual attraction effect.
The principle is illustrated by way of example in the course of the ascent of an unmanned aerial vehicle:
when the motor 0 rotates, a lifting force is obtained through the rotation of the rotor, so that the permanent magnet 21 is driven to rise along with the motor 0 by the rising of the motor 0, and the surrounding magnetic field is changed due to the displacement change of the permanent magnet 21 caused by the rising.
Through mutual exclusion effect or mutual suction effect of this kind of real-time variation, after motor 0 obtains the power that rises of rotor, can drive permanent magnet 21 and rise, and the magnetic force effect that the corresponding solenoid 22 can produce with permanent magnet 21 looks attraction through the feedback of hall sensor 23 this moment, so, motor 0 rises and will drive motor cabinet body 1 and whole unmanned aerial vehicle through this kind of magnetic force effect and rise, only through magnetic force connection between this process motor cabinet body 1 and the motor 0, do not produce other hard couplings, so motor 0's vibrations can be slowed down.
When the unmanned aerial vehicle flies, the motor 0 is connected with the motor seat body 1 by pure magnetic force, so that the permanent magnet 21 and the electromagnetic coil 22 are subjected to continuous relative displacement change, and further the mutual exclusion or mutual attraction effect is generated between the permanent magnet 21 and the electromagnetic coil 22 alternately through the feedback electric signal of the Hall sensor 23, and the vibration of the motor 0 can be relieved.
As a preferred embodiment, three hall sensors 23 are provided, and as shown in any of fig. 1 to 4, the three hall sensors 23 are disposed on the side wall of the motor base body 1 in a ring matrix.
With continued reference to fig. 1-3, the connection of the hall sensor 23 to the motor base body 1 includes:
the Hall sensor 23 is arranged on the side wall of the motor base body 1.
Fig. 5 is a second schematic explosion diagram of the unmanned aerial vehicle driving device according to an embodiment of the present invention.
As shown in fig. 5, and in contrast to fig. 4, the connection of the electromagnetic coil 22 with the motor base body 1 includes:
the motor cabinet body 1 is provided with an annular groove 11, and the electromagnetic coil 22 is arranged in the annular groove 11.
Fig. 8 is a schematic structural diagram of a fastening mechanism according to an embodiment of the present invention.
Further, as shown in fig. 8, the device further comprises a buckling mechanism 3; the fastening mechanism 3 comprises a fastening 31 and a fastening part 32 which are arranged on the motor base body 1; in fig. 8, a specific embodiment is shown that one end of the buckle 31 is hinged to one side of the annular groove 11, and the engaging portion 32 is disposed on the other side of the annular groove 11.
Because one end of the buckle 31 is hinged to one side of the annular groove 11, the buckle 31 can rotate along the hinge point, in the use process, the buckle 31 can be rotated to one side opposite to the clamping portion 32, so that the annular groove 11 is exposed for placing the electromagnetic coil 22, and after the electromagnetic coil 22 is fixed, the buckle 31 rotates to the clamping portion 32 along the hinge point and is clamped and fixed with the clamping portion 32, shielding of the annular groove 11 is completed, and the electromagnetic coil 22 is placed to drop out.
FIG. 6 is a schematic perspective view of a motor damper mechanism according to an embodiment of the present invention; fig. 7 is a schematic plan view of a motor damper mechanism according to an embodiment of the present invention.
Further, as shown in fig. 6 and 7, the motor damping mechanism 4 is further included; the motor damping mechanism 4 comprises a motor 0 fixing sleeve, a motor fixing shell 42 and at least two elastic pieces 43; as can be seen in fig. 7, the motor 0 is fixed in the motor 0 fixing sleeve and is connected with the motor 0 fixing sleeve, so that the motor 0 cannot be separated from the motor 0 fixing sleeve; while such connection is not limited to a fixed connection, it may also include elastic or other open connections.
Further, the motor 0 fixing sleeve is provided in the motor fixing case 42, and the motor fixing case 42 and the motor 0 fixing sleeve are elastically connected to each other by the elastic member 43.
When the unmanned aerial vehicle flies, if the motor 0 vibrates, the vibration cannot be directly transmitted to the motor fixing shell 42 due to the elastic piece 43, and then the vibration is transmitted, but the primary slow release is carried out through the elastic piece 43; in this way, the stabilizing effect can be further improved by the magnetic levitation shock absorbing mechanism 2.
The elastic piece 43 includes a connecting member having elasticity such as a spring, an elastic material, or the like.
Further, with continued reference to fig. 7, the elastic member 43 is provided at both ends with connection pieces 44 for more convenient connection of the elastic member 43, as shown in fig. 7, wherein the elastic member 43 is connected to the motor 0 fixing case and the motor fixing case 42 through the connection pieces 44 provided at both ends.
Further, in the embodiment of the present invention, the motor base body 1 includes any one of a cylindrical structure, a truncated cone structure, a square structure and a prismatic table structure.
The application also provides an unmanned aerial vehicle driving device, which comprises a motor 0 and the unmanned aerial vehicle motor 0 seat;
the permanent magnet 21 of the unmanned aerial vehicle motor 0 seat is fixedly arranged with the output end of the motor 0.
Since the specific structure, functional principle and technical effect of the unmanned aerial vehicle motor 0 seat are described in detail above, the description thereof will be omitted.
The application also provides an unmanned aerial vehicle, which comprises an unmanned aerial vehicle body, a horn, a rotor wing and the unmanned aerial vehicle driving device;
the unmanned aerial vehicle body passes through the horn with unmanned aerial vehicle drive arrangement is connected, the rotor passes through unmanned aerial vehicle drive arrangement drive rotation.
Finally, it should be noted that: the above embodiments are only for illustrating the technical solution of the present invention, and not for limiting the same; although the invention has been described in detail with reference to the foregoing embodiments, it will be understood by those of ordinary skill in the art that: the technical scheme described in the foregoing embodiments can be modified or some or all of the technical features thereof can be replaced by equivalents; such modifications and substitutions do not depart from the spirit of the invention.
Claims (8)
1. The unmanned aerial vehicle motor seat comprises a motor seat body (1), and is characterized by further comprising a magnetic suspension damping mechanism (2);
the magnetic suspension damping mechanism (2) comprises a permanent magnet (21), an electromagnetic coil (22) and at least one Hall sensor (23); the permanent magnet (21) is used for being connected with the motor (0);
the electromagnetic coil (22) and the Hall sensor (23) are connected with the motor base body (1); the Hall sensor (23) is arranged corresponding to the permanent magnet (21) and is used for generating an electric signal for adjusting the magnetism of the electromagnetic coil (22) according to the magnetic field change of the permanent magnet (21);
the Hall sensor (23) is connected with the motor base body (1) and comprises: the Hall sensor (23) is arranged on the side wall of the motor base body (1);
the electromagnetic coil (22) is connected with the motor base body (1) and comprises: the motor cabinet body (1) is provided with an annular groove (11), and the electromagnetic coil (22) is arranged in the annular groove (11).
2. The unmanned aerial vehicle motor according to claim 1, further comprising a snap mechanism (3); the clamping mechanism (3) comprises a clamping buckle (31) and a clamping part (32) which are arranged on the motor base body (1);
one end of the buckle (31) is hinged to one side of the annular groove (11), and the clamping part (32) is arranged on the other side of the annular groove (11).
3. The unmanned aerial vehicle motor according to claim 1, further comprising a motor damping mechanism (4); the motor damping mechanism (4) comprises a motor fixing sleeve (41), a motor fixing shell (42) and at least two elastic pieces (43);
the motor (0) is fixed in the motor fixing sleeve (41), the motor fixing sleeve (41) is arranged in the motor fixing shell (42), and the motor fixing shell (42) is elastically connected with the motor fixing sleeve (41) through the elastic piece (43).
4. A unmanned aerial vehicle motor according to claim 3, wherein the elastic member (43) is provided with connection pieces (44) at both ends, and the elastic member (43) is connected to the motor fixing case (41) and the motor fixing case (42) through the connection pieces (44) provided at both ends.
5. The unmanned aerial vehicle motor stand according to any one of claims 1 to 4, wherein the motor stand body (1) comprises any one of a cylindrical structure, a truncated cone structure, a square structure, and a prismatic table structure.
6. The unmanned aerial vehicle motor according to any of claims 1 to 4, wherein three hall sensors (23) are provided, and three hall sensors (23) are provided in an annular matrix on the side wall of the motor housing body (1).
7. A drone drive comprising a motor and a drone motor as claimed in any one of claims 1 to 6;
the permanent magnet of the unmanned aerial vehicle motor seat is fixedly arranged with the output end of the motor (0).
8. A drone comprising a drone body, a horn, a rotor, and the drone drive of claim 7;
the unmanned aerial vehicle body passes through the horn with unmanned aerial vehicle drive arrangement is connected, the rotor passes through unmanned aerial vehicle drive arrangement drive rotation.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710317118.0A CN106976560B (en) | 2017-05-08 | 2017-05-08 | Unmanned aerial vehicle motor seat, unmanned aerial vehicle drive arrangement and unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710317118.0A CN106976560B (en) | 2017-05-08 | 2017-05-08 | Unmanned aerial vehicle motor seat, unmanned aerial vehicle drive arrangement and unmanned aerial vehicle |
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| Publication Number | Publication Date |
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| CN106976560A CN106976560A (en) | 2017-07-25 |
| CN106976560B true CN106976560B (en) | 2023-07-21 |
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| CN201710317118.0A Active CN106976560B (en) | 2017-05-08 | 2017-05-08 | Unmanned aerial vehicle motor seat, unmanned aerial vehicle drive arrangement and unmanned aerial vehicle |
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Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN207045655U (en) * | 2017-07-28 | 2018-02-27 | 深圳市大疆创新科技有限公司 | Horn component, frame and unmanned vehicle |
| CN107839871B (en) * | 2017-11-30 | 2023-11-17 | 歌尔股份有限公司 | Propeller connection structure and unmanned vehicles |
| CN107769459A (en) * | 2017-11-30 | 2018-03-06 | 无锡典聚科技有限公司 | There is the error-proof structure of set lead-out wire in a kind of electronic strut of tail-gate |
| CN108482649B (en) * | 2018-03-01 | 2021-05-25 | 常熟京常智能科技有限公司 | Many rotor formula unmanned aerial vehicle magnetic suspension damping device |
| CN113194693A (en) * | 2021-05-13 | 2021-07-30 | 山东立尔智能科技有限公司 | Be used for outside heat sink of electric power automation equipment |
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| CN103419931A (en) * | 2012-05-18 | 2013-12-04 | 李晓桓 | Autonomous lift-off aircraft |
| CN104670487A (en) * | 2013-10-03 | 2015-06-03 | 奥格斯塔韦斯兰股份公司 | Hover aircraft rotor and hover aircraft |
| CN105323445A (en) * | 2015-09-21 | 2016-02-10 | 杭州卓壮科技有限公司 | Magnetic suspension video camera |
| CN205524941U (en) * | 2016-04-26 | 2016-08-31 | 徐启航 | Magnetic suspension variable -pitch propeller oar and aircraft |
| CN206885350U (en) * | 2017-05-08 | 2018-01-16 | 昊翔电能运动科技(昆山)有限公司 | A kind of unmanned plane motor cabinet, unmanned machine actuating device and unmanned plane |
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- 2017-05-08 CN CN201710317118.0A patent/CN106976560B/en active Active
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|---|---|---|---|---|
| CN103419931A (en) * | 2012-05-18 | 2013-12-04 | 李晓桓 | Autonomous lift-off aircraft |
| CN104670487A (en) * | 2013-10-03 | 2015-06-03 | 奥格斯塔韦斯兰股份公司 | Hover aircraft rotor and hover aircraft |
| CN105323445A (en) * | 2015-09-21 | 2016-02-10 | 杭州卓壮科技有限公司 | Magnetic suspension video camera |
| CN205524941U (en) * | 2016-04-26 | 2016-08-31 | 徐启航 | Magnetic suspension variable -pitch propeller oar and aircraft |
| CN206885350U (en) * | 2017-05-08 | 2018-01-16 | 昊翔电能运动科技(昆山)有限公司 | A kind of unmanned plane motor cabinet, unmanned machine actuating device and unmanned plane |
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| CN106976560A (en) | 2017-07-25 |
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