CN205396569U - Unmanned vehicles with battery formula counter weight device - Google Patents
Unmanned vehicles with battery formula counter weight device Download PDFInfo
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- CN205396569U CN205396569U CN201620176129.2U CN201620176129U CN205396569U CN 205396569 U CN205396569 U CN 205396569U CN 201620176129 U CN201620176129 U CN 201620176129U CN 205396569 U CN205396569 U CN 205396569U
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Abstract
The utility model provides an unmanned vehicles with battery formula counter weight device, unmanned vehicles (1) is including lift -launch equipment (2) and battery formula counter weight device (3), lift -launch equipment (2) arrange in one side of unmanned vehicles focus (O), is equipped with a plurality of holding the holding of battery equipment (4) battery formula counter weight device (3) intercommunication the battery to unmanned vehicles (1) power supply, battery formula counter weight device (3) is arranged the opposite side of unmanned vehicles focus (O), one or more hold equipment (4) and hold and have the battery battery formula counter weight device (3) arrives adjustable being of moment of unmanned vehicles focus (O) lift -launch equipment (2) are arrived the moment of unmanned vehicles focus (O).
Description
Technical field
This utility model belongs to unmanned vehicle field, particularly relates to a kind of unmanned vehicle with battery type counter weight device.
Background technology
It is that take photo by plane technology, the communication of a collection singlechip technology, sensor technology of taking photo by plane, GPS navigation is taken photo by plane many technology such as service technology, flight control technology, task control technology, programming technique rely on the high-tech product of hardware, the advantage that its filmed image has high-resolution, large scale, little area, high Up-to-date state that unmanned vehicle is taken photo by plane.And unmanned vehicle provides easy to operate for photography of taking photo by plane, it is easy to the remote sensing platform of transition；Taking off landing is limited less by place, on playground, highway or other openr ground all can landing, its stability, safety are good, and transition etc. is very easy；Small portable, low-noise energy-saving, efficiently motor-driven, image definition, lightness, miniaturization, the intelligent outstanding feature that unmanned vehicle is taken photo by plane especially.Apply many rotor wing unmanned aerial vehicles to carry out the monitoring of specific region and can there is no concern that personal security, also there is no concern that the muscle power restriction of pilot.Unmanned vehicle can perform various task the most dangerous, for instance bad environments, people cannot be close environment under adopt unmanned plane to carry out monitor in real time.Therefore, employing unmanned vehicle realizes taking photo by plane and is used widely now.
Unmanned vehicle is not when carrying other equipment, and its center of gravity is positioned at the axis of fuselage, thus balance when realizing unmanned vehicle.But, the weight of equipment carried due to unmanned vehicle has bigger difference.Such as, carrying digital camera, professional camera etc. at Handpiece Location, particularly once change the capture apparatus of different model, or to capture apparatus plus peripheral hardwares such as different camera lenses, will cause that original counterweight is destroyed.Capital has influence on the position of centre of gravity of unmanned vehicle, thus balance when having influence on unmanned vehicle flight so that middle shake of taking photo by plane, have a strong impact on shooting effect.The way generally adopted at present is " counterweight ", and namely when head carries certain equipment, by loading the object of constant weight at tail, the center of gravity to ensure electronic unmanned plane is positioned at location mid-shaft." counterweight " regulative mode can solve the gravity balance problem of unmanned vehicle, but has but increased the weight of the load of unmanned vehicle.Add the power consumption of unmanned vehicle, and have influence on cruising time and the flight safety of unmanned vehicle.Therefore, this balance adjusting method needs to improve.Carrying equipment it is typically necessary in actual applications, such as digital camera, video camera and various sensors etc., thus having influence on center of gravity and the balance of electronic unmanned plane due to unmanned vehicle." counterweight " method general at present, although can solve the problem that gravity balance problem, but increased the weight of the load of unmanned vehicle, add the energy consumption of unmanned vehicle, has influence on cruising time and the flight safety of unmanned vehicle, in the urgent need to improving.
Patent documentation CN201420367748 discloses a kind of balance weight assembly, uses balance weight mechanism and the The Cloud Terrace of this balance weight assembly, comprising:. a kind of balance weight assembly, including connecting seat and balancing weight, it is characterized in that: this balance weight assembly also includes the guide being arranged on this connection seat, this balancing weight is connected on this guide, and can move to adjust the center of gravity of this balance weight assembly along this guide.The patent discloses that the importance about counterweight, and how prior art uses the balancing weight of adjustable position to solve the technical scheme of counterweight problem.But in the program, although balancing weight increases the motility that counterweight regulates, but add unnecessary load-bearing to whole unmanned plane, and this counterweight adjustment structure is also relatively complicated.
Patent documentation CN201420367748 discloses a kind of cell, unmanned plane and for being assembled into the external member of unmanned plane, and a kind of cell includes: the first battery core unit, first control circuit, the second battery core unit, second control circuit and battery container；Described first control circuit and described first battery core unit are electrical connected, for monitoring whether described first battery core unit breaks down, when described first battery core unit breaks down, disconnect the electrical connection between described first battery core unit and the power output end of first control circuit, so that described first battery core unit is stopped power supply or charges；Described second control circuit and described second battery core unit are electrical connected, for monitoring whether described second battery core unit breaks down, when described second battery core unit breaks down, disconnect the electrical connection between described second battery core unit and the power output end of second control circuit, so that described second battery core unit is stopped power supply or charges；Described battery container, is used for encapsulating described first battery core unit and described second battery core unit；Wherein, described first battery core unit is in parallel with described second battery core unit, and described first battery core unit and described second battery core unit include at least one battery core.Multiple battery that how to use of this patent major concern is powered to unmanned aerial vehicle, thus avoiding when cell, once cell malfunctions, the problem that then unmanned plane will run out of steam completely, so proposing the technical scheme adopting multiple cells to be used as backup, entirely without relating to counterweight problem.
Patent documentation CN203601574U discloses a kind of single electronic unmanned plane balance regulator of rotor, described electronic unmanned plane includes fuselage (7) and is arranged at the empennage (8) of back body, the front end of described fuselage connects carrying equipment (9), the electronic unmanned plane balance regulator of described single rotor farther includes base plate (1), front shoe (4) and rear fixed plate (5), in fuselage (7), the position of described carrying equipment (9) is provided with a draw-in groove being distributed along empennage (8) straight-bar length direction, binding has the base plate (1) of battery (3) to slide along described draw-in groove, one end of front shoe (4) and rear fixed plate (5) all with fuselage (7) clamping, the other end respectively with base plate (1) before, rear two ends are fixed.This patent is pinioned battery by fixing band and is achieved balance adjustment, but this patent carries out method without ground accurately adjust the balance of unmanned vehicle for different heavy burden weight, different weighted position, particularly when ensureing suitable electricity supply, this patent also cannot be conveniently carried out adjusting moment and changing battery, and its suitability obtains very big restriction.
Therefore, this area be badly in need of a kind of carrying equipment according to Different Weight and diverse location can rapidly, carry out the reequilibrate of unmanned vehicle accurately, easily, do not increase extra inert weight simultaneously.
Disclosed above-mentioned information is used only for strengthening the understanding to this utility model background in the background section, it is thus possible to comprise the information not being formed in this country prior art known to a person of ordinary skill in the art.
Utility model content
The purpose of this utility model is to be achieved by the following technical programs.
According to this utility model, a kind of unmanned vehicle with battery type counter weight device, described unmanned vehicle includes carrying equipment and battery type counter weight device, described carrying equipment is arranged in the side of unmanned vehicle center of gravity, the described battery type counter weight device described battery of connection holding equipment being provided with multiple accommodation battery is powered to described unmanned vehicle, described battery type counter weight device is arranged in the opposite side of described unmanned vehicle center of gravity, one or more accommodation equipment accommodate the described battery type counter weight device of battery and can be adjusted to the described carrying equipment moment to described unmanned vehicle center of gravity to the moment of described unmanned vehicle center of gravity.
Preferably, described unmanned vehicle is provided with the distance of the center of gravity of the support apparatus supporting described carrying equipment, described support apparatus adjustable and unmanned vehicle.
Preferably, described battery type counter weight device is positioned on the line of carrying equipment center of gravity and unmanned vehicle center of gravity.
Preferably, described line is the central axis of unmanned vehicle.
Preferably, described battery type counter weight device has the described accommodation equipment of multiple same size, described accommodation equipment is the battery draw-in groove of clamping battery, multiple described accommodation equipment equidistants are from linear arrangement, and described battery type counter weight device selects one or more described accommodation equipment accommodation battery to make described battery type counter weight device be equal to the described carrying equipment moment to described unmanned vehicle center of gravity to the moment of described unmanned vehicle center of gravity according to the moment of described carrying equipment to described unmanned vehicle center of gravity.
Preferably, described battery type counter weight device has multiple various sizes of described accommodation equipment, described accommodation equipment is the battery draw-in groove of the clamping battery with closing lid, multiple described liftoff multiple rows of arrangements of accommodation equipment interval Unequal distance, described battery type counter weight device selects one or more described accommodation equipment accommodation battery to make described battery type counter weight device be equal to the described carrying equipment moment to described unmanned vehicle center of gravity to the moment of described unmanned vehicle center of gravity according to the moment of described carrying equipment to described unmanned vehicle center of gravity.
Preferably, described accommodation equipment is provided with the battery compartment slidably holding battery, and described battery type counter weight device slides into precalculated position according to the moment one or more battery compartments containing battery of selection of described carrying equipment to described unmanned vehicle center of gravity and makes described battery type counter weight device be equal to the described carrying equipment moment to described unmanned vehicle center of gravity to the moment of described unmanned vehicle center of gravity.
Preferably, described support apparatus is the The Cloud Terrace being arranged on described unmanned vehicle, and described carrying equipment is capture apparatus, the described capture apparatus that described The Cloud Terrace adjustable is mounted thereto.
Preferably, battery type counter weight device includes the initial accommodation equipment being located in unmanned vehicle center of gravity, and when unmanned vehicle does not carry carrying equipment, battery is contained in described initial accommodation equipment.
The scheme that the utility model proposes can simply by position installing an appropriate number of battery to realize counterweight balance, it is not necessary to complicated position adjustment；Battery type counter weight device has power supply deliverability simultaneously, significant increase flight efficiency, during battery type counter weight device counterweight, it designs through optimizing compared to position and the counterweight amount of center of gravity, especially as the application scheme proposes, the words of multiple counterweight battery are designed, it is possible to suitably make use of the relation between weight and moment so that the adjustment of counterweight can coordinate accurately within the counterweight scope pre-set according to the mode that then its weight is more light further away from center of gravity.
Accompanying drawing explanation
Fig. 1 is the structural representation of the unmanned vehicle with battery type counter weight device according to one embodiment of this utility model.
Fig. 2 is the structural representation of the unmanned vehicle with battery type counter weight device according to another embodiment of this utility model.
Fig. 3 is the structural representation of the unmanned vehicle with battery type counter weight device according to another embodiment of this utility model.
Below in conjunction with drawings and Examples, the utility model is further explained.
Detailed description of the invention
Described in detail below being actually merely illustrative of and be not intended to limit application and use.Additionally, be not intended to be subject to above technical field, background, brief overview or described in detail below in present any clearly or the theoretical constraint of hint.
Embodiment of the present utility model describes a kind of unmanned vehicle with battery type counter weight device.The schematic diagram of the unmanned vehicle with battery type counter weight device according to an embodiment of the present utility model as shown in Figure 1, unmanned vehicle 1 includes carrying equipment 2 and battery type counter weight device 3, described carrying equipment 2 is arranged in the side of unmanned vehicle center of gravity O, it is provided with the described battery type counter weight device 3 of the accommodation equipment 4 of multiple accommodation battery to connect described battery and power to described unmanned vehicle 1, described battery type counter weight device 3 is arranged in the opposite side of described unmanned vehicle center of gravity O, one or more accommodation equipment 4 accommodate the described battery type counter weight device 3 of battery and can be adjusted to the described carrying equipment 2 moment to described unmanned vehicle center of gravity O to the moment of described unmanned vehicle center of gravity O.Wherein, unmanned vehicle center of gravity O refers to the position of centre of gravity when not carrying carrying equipment 2 and battery of the unmanned vehicle 1 with battery type counter weight device.
In one embodiment, unmanned vehicle 1 is many rotor unmanned aircrafts.Accommodation equipment 4 there is no special feature with the electrical connection flying the power consumption unit such as control, electricity tune, motor on unmanned vehicle 1.Multiple accommodation equipment 4 can be used in parallel, or multiple accommodation equipment 4 can also be series connection use, this series connection use hold equipment 4 can similar multiple batteries cascade arrange, its concrete connected mode should be there is no doubt by those skilled in the art.
In one embodiment, carrying equipment 2 can be the arbitrary equipment that unmanned vehicle 1 carries, for instance can be capture apparatus or monitoring device.Wherein, capture apparatus is visible ray high-definition camera, high-resolution camera, infrared thermoviewer or ultraviolet imagery equipment.
In one embodiment, battery type counter weight device 3 is integrally formed with unmanned vehicle 1.In another embodiment, battery type counter weight device 3 is detachably connected on unmanned vehicle 1.
In one embodiment, described battery type counter weight device 3 is positioned on the line AOB of carrying equipment center of gravity and unmanned vehicle center of gravity O.Described line AOB is the central axis of unmanned vehicle 1.This is conducive to the balance of unmanned vehicle 1.
nullIn one embodiment，Unmanned vehicle 1 includes carrying equipment 2 and battery type counter weight device 3，Described carrying equipment 2 is arranged in the side of unmanned vehicle center of gravity O，It is provided with the described battery type counter weight device 3 of the accommodation equipment 4 of multiple accommodation battery to connect described battery and power to described unmanned vehicle 1，Described battery type counter weight device 3 is arranged in the opposite side of described unmanned vehicle center of gravity O，Described battery type counter weight device 3 has the described accommodation equipment 4 of multiple same size，Described accommodation equipment is the battery draw-in groove of clamping battery，Multiple described equidistant linear arrangements of accommodation equipment 4，Described battery type counter weight device 3 holds battery according to the moment one or more described accommodation equipment 4 of selection of described carrying equipment 2 to described unmanned vehicle center of gravity O and makes described battery type counter weight device 3 arrive the moment of described unmanned vehicle center of gravity O equal to described carrying equipment 2 to the moment of described unmanned vehicle center of gravity O.In an embodiment, battery needs to form, with carrying equipment 2, the function that weight mutually compensates for and can realize centre of gravity adjustment, and battery unit is distributed with carrying equipment 2 one-tenth wire.Battery corresponding to battery draw-in groove can be have same specification and size, so, according to the distance of battery draw-in groove unmanned vehicle 1 center of gravity O apart, and fills the quantity of battery, it is possible to for the concrete weights of carrying equipment 2, it is achieved effective counterweight.And owing to the size of these batteries, specification are identical, the cost of battery and battery type counter weight device 3 is greatly controlled, and the installation of battery is also very convenient.
In one embodiment, being actually needed weight, these batteries corresponding to battery draw-in groove can also be have different specifications and size, and battery draw-in groove then has specifications different accordingly and size too.nullUnmanned vehicle 1 includes carrying equipment 2 and battery type counter weight device 3，Described carrying equipment 2 is arranged in the side of unmanned vehicle center of gravity O，It is provided with the described battery type counter weight device 3 of the accommodation equipment 4 of multiple accommodation battery to connect described battery and power to described unmanned vehicle 1，Described battery type counter weight device 3 is arranged in the opposite side of described unmanned vehicle center of gravity O，Described battery type counter weight device 3 has multiple various sizes of described accommodation equipment 4，Described accommodation equipment 4 is the battery draw-in groove of the clamping battery with closing lid，Multiple described accommodation equipment 4 interval liftoff multiple rows of arrangements of Unequal distance，Described battery type counter weight device 3 holds battery according to the moment one or more described accommodation equipment 4 of selection of described carrying equipment 2 to described unmanned vehicle center of gravity O and makes described battery type counter weight device 3 arrive the moment of described unmanned vehicle center of gravity O equal to described carrying equipment 2 to the moment of described unmanned vehicle center of gravity O.For example, battery type counter weight device 3 is disposed with 3 battery draw-in grooves, these three battery draw-in grooves are followed successively by draw-in groove first, draw-in groove second, draw-in groove third, wherein battery specifications corresponding to draw-in groove the first and second the third and size diminish successively, assume the battery of the battery of draw-in groove first correspondence 1000mAh specification, the battery of draw-in groove second correspondence 750mAh specification, the corresponding 500mAh specification of draw-in groove third, and owing to the specification of battery is different, its counterweight is also different, different plus the draw-in groove moment length compared to unmanned vehicle center of gravity O, then the counterbalancing effect produced is also different.Under the design of this scheme, this counter weight construction is advantageously in the intense adjustment for counterweight.This concrete scheme is only illustrative thinking and principle that the application counterbalance design is described, can design targetedly according to the position of actual carrying equipment 2 and weight about concrete battery pocket numbers, draw-in groove position, draw-in groove specifications design etc., thus reaching more preferably effect.
nullIn order to adjust counterweight further subtly，In one embodiment，Unmanned vehicle 1 includes carrying equipment 2 and battery type counter weight device 3，Described carrying equipment 2 is arranged in the side of unmanned vehicle center of gravity O，It is provided with the described battery type counter weight device 3 of the accommodation equipment 4 of multiple accommodation battery to connect described battery and power to described unmanned vehicle 1，Described battery type counter weight device 3 is arranged in the opposite side of described unmanned vehicle center of gravity O，Described accommodation equipment 4 is provided with the battery compartment slidably holding battery，Described battery type counter weight device 3 slides into precalculated position according to the moment one or more battery compartments containing battery of selection of described carrying equipment 2 to described unmanned vehicle center of gravity O and makes described battery type counter weight device 3 arrive the moment of described unmanned vehicle center of gravity O equal to described carrying equipment 2 to the moment of described unmanned vehicle center of gravity O.Adjust moment continuously by the slip of battery compartment and balance moment further subtly.
nullIn one embodiment，The schematic diagram of the unmanned vehicle with battery type counter weight device according to an embodiment of the present utility model as shown in Figure 2，Unmanned vehicle 1 includes carrying equipment 2 and battery type counter weight device 3，Described carrying equipment 2 is arranged in the side of unmanned vehicle center of gravity O，It is provided with the described battery type counter weight device 3 of the accommodation equipment 4 of multiple accommodation battery to connect described battery and power to described unmanned vehicle 1，Described battery type counter weight device 3 is arranged in the opposite side of described unmanned vehicle center of gravity O，Accommodate the described battery type counter weight device 3 of battery and can be adjusted to the described carrying equipment 2 moment to described unmanned vehicle center of gravity O to the moment of described unmanned vehicle center of gravity O，Wherein，Unmanned vehicle center of gravity O refers to the position of centre of gravity when not carrying carrying equipment 2 and battery of the unmanned vehicle 1 with battery type counter weight device.Described unmanned vehicle 1 is provided with the distance of the center of gravity of the support apparatus 5 supporting described carrying equipment 2, described support apparatus 5 adjustable and unmanned vehicle.Further, described support apparatus 5 is the The Cloud Terrace being arranged on described unmanned vehicle, and described carrying equipment 2 is capture apparatus, the described capture apparatus that described The Cloud Terrace adjustable is mounted thereto.The Cloud Terrace is responsible for establishing shot equipment, and is provided that device location adjusts function and stabilization function, and capture apparatus is generally moving camera, it is possible under circumstances, efficiently accomplish shooting task.The Cloud Terrace is can the all-directional tripod head that can rotate up and down again of left rotation and right rotation.The Cloud Terrace can apply to the electric platform shot on a large scale, and this electric platform high speed attitude can be realized by two operating motors.In one embodiment, the described capture apparatus that the described The Cloud Terrace adjustable that is arranged on described unmanned vehicle 1 is mounted thereto, described The Cloud Terrace includes the adjusting mechanism for zoom operational, elevating movement and azimuth motion.
The schematic diagram of the unmanned vehicle with battery type counter weight device according to an embodiment of the present utility model as shown in Figure 3, unmanned vehicle 1 includes carrying equipment 2 and battery type counter weight device 3, battery type counter weight device 3 includes the initial accommodation equipment 6 being located on unmanned vehicle center of gravity O, when unmanned vehicle 1 does not carry carrying equipment, battery is contained in described initial accommodation equipment 6.In the present embodiment, when the unloaded flight of unmanned vehicle 1, battery type counter weight device 3 nor affects on the balance of unmanned vehicle 1.
Although embodiment of the present utility model being described above in association with accompanying drawing, but this utility model is not limited to above-mentioned specific embodiments and applications field, and above-mentioned specific embodiments is merely schematic, guiding, rather than restrictive.Those of ordinary skill in the art is under the enlightenment of this specification and without departing from this utility model scope of the claimed protection, it is also possible to making a variety of forms, these belong to the row of this utility model protection.
Claims (10)
1. the unmanned vehicle with battery type counter weight device, described unmanned vehicle (1) includes carrying equipment (2) and battery type counter weight device (3), described carrying equipment (2) is arranged in the side of unmanned vehicle center of gravity (O), it is provided with the described battery type counter weight device (3) of the accommodation equipment (4) of multiple accommodation battery to connect described battery and power to described unmanned vehicle (1), described battery type counter weight device (3) is arranged in the opposite side of described unmanned vehicle center of gravity (O), it is characterized in that: one or more accommodation equipment (4) accommodate the described battery type counter weight device (3) of battery and can be adjusted to, to the moment of described unmanned vehicle center of gravity (O), the moment mating described carrying equipment (2) to described unmanned vehicle center of gravity (O).
2. the unmanned vehicle with battery type counter weight device according to claim 1, it is characterised in that: described unmanned vehicle (1) is provided with the support apparatus (5) supporting described carrying equipment (2).
3. the unmanned vehicle with battery type counter weight device according to claim 1, it is characterised in that: described unmanned vehicle (1) is many rotor unmanned aircrafts.
4. the unmanned vehicle with battery type counter weight device according to claim 2, it is characterized in that: described support apparatus (5) is the The Cloud Terrace being arranged on described unmanned vehicle, described carrying equipment (2) is capture apparatus, the described capture apparatus that described The Cloud Terrace adjustable is mounted thereto.
5. the unmanned vehicle with battery type counter weight device according to claim 1, it is characterized in that: described battery type counter weight device (3) has the described accommodation equipment (4) of multiple same size, described accommodation equipment is the battery draw-in groove of clamping battery, the equidistant linear arrangement of multiple described accommodation equipment (4).
6. the unmanned vehicle with battery type counter weight device according to claim 1, it is characterized in that: described battery type counter weight device (3) has multiple various sizes of described accommodation equipment (4), described accommodation equipment (4) is the battery draw-in groove of the clamping battery with closing lid, multiple described accommodation equipment (4) interval liftoff multiple rows of arrangements of Unequal distance.
7. the unmanned vehicle with battery type counter weight device according to claim 1, it is characterised in that: described accommodation equipment (4) is provided with the battery compartment slidably holding battery.
8. the unmanned vehicle with battery type counter weight device according to claim 4, it is characterised in that:. described The Cloud Terrace includes the adjusting mechanism for zoom operational, elevating movement and azimuth motion.
9. the unmanned vehicle with battery type counter weight device according to claim 1, it is characterised in that: battery type counter weight device (3) includes being located at and initially holds equipment (6) in unmanned vehicle center of gravity (O).
10. the unmanned vehicle with battery type counter weight device according to claim 1, it is characterised in that: battery type counter weight device (3) is detachably connected on unmanned vehicle (1).
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| Application Number | Priority Date | Filing Date | Title |
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| CN201620176129.2U CN205396569U (en) | 2016-03-08 | 2016-03-08 | Unmanned vehicles with battery formula counter weight device |
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| CN201620176129.2U CN205396569U (en) | 2016-03-08 | 2016-03-08 | Unmanned vehicles with battery formula counter weight device |
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| CN205396569U true CN205396569U (en) | 2016-07-27 |
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105775152A (en) * | 2016-03-08 | 2016-07-20 | 谭圆圆 | Unmanned aerial vehicle with battery type counterweight device and counterweight method thereof |
| CN106314636A (en) * | 2016-08-29 | 2017-01-11 | 倪学才 | Balance car |
| CN106364686A (en) * | 2016-09-30 | 2017-02-01 | 安徽翼讯飞行安全技术有限公司 | Power supply structure for unmanned aerial vehicle |
| CN106364623A (en) * | 2016-08-29 | 2017-02-01 | 倪学才 | Balance vehicle |
-
2016
- 2016-03-08 CN CN201620176129.2U patent/CN205396569U/en active Active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105775152A (en) * | 2016-03-08 | 2016-07-20 | 谭圆圆 | Unmanned aerial vehicle with battery type counterweight device and counterweight method thereof |
| CN106314636A (en) * | 2016-08-29 | 2017-01-11 | 倪学才 | Balance car |
| CN106364623A (en) * | 2016-08-29 | 2017-02-01 | 倪学才 | Balance vehicle |
| CN106364686A (en) * | 2016-09-30 | 2017-02-01 | 安徽翼讯飞行安全技术有限公司 | Power supply structure for unmanned aerial vehicle |
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