CN210592452U

CN210592452U - Unmanned aerial vehicle power supply mechanism capable of rapidly switching on and off power supply

Info

Publication number: CN210592452U
Application number: CN201921614187.9U
Authority: CN
Inventors: 王君浩; 张硕; 顾维春; 许必成
Original assignee: Wuxi Shenghuihong Technology Co Ltd
Current assignee: Wuxi Shenghuihong Technology Co Ltd
Priority date: 2019-09-26
Filing date: 2019-09-26
Publication date: 2020-05-22
Anticipated expiration: 2029-09-26

Abstract

The utility model relates to an unmanned aerial vehicle field, the unmanned aerial vehicle power supply mechanism of break-make power fast that specifically says so. It includes unmanned aerial vehicle's frame, has the power in this frame. The multifunctional electric bicycle is characterized in that a handle is arranged on the rack, a lifting ring is arranged on the inner side of the handle, and a sliding block is connected to the lower portion of the lifting ring. The top plate of the rack is provided with a sliding hole at the position corresponding to the lifting ring, the sliding block of the lifting ring extends into the sliding hole, and the sliding block and the sliding hole are in vertical sliding fit. The inside below of slide opening of frame is fixed with the electrically conductive connecting plate, the input of this electrically conductive connecting plate with the power links to each other, the output is used for linking to each other with unmanned aerial vehicle's power unit, and is open circuit between input and output, the bottom of slider has the electric conductor that is used for making the input of electrically conductive connecting plate and output switch on. This power supply mechanism can the fast break-make power, and the operation is very simple, can hardly increase unmanned aerial vehicle's volume, weight and cost moreover, the condition of burning loss can not appear yet, applicable unmanned aerial vehicle in whole models.

Description

Unmanned aerial vehicle power supply mechanism capable of rapidly switching on and off power supply

Technical Field

The utility model relates to an unmanned aerial vehicle field, the unmanned aerial vehicle power supply mechanism who is used for quick break-make power on the unmanned aerial vehicle organism that specifically says so.

Background

The unmanned aerial vehicle product of present comes to a lot, and hundreds of flowers are all round, but the kind of power supply mechanism is more single. The common traditional connector formula of jointing that has, organism shell need be demolishd to this kind of mode, uses two hands simultaneous operation, docks the connector of power supply lead-out wire and the connector of unmanned aerial vehicle power unit lead-out wire, just can realize the power supply of power to power unit. When needing the outage, also must demolish the shell, with two bayonet joint separations, just can realize cutting off of unmanned aerial vehicle power. For small and medium-sized unmanned aerial vehicles, the operable space of the inner cavity of the unmanned aerial vehicle is very small, and by adopting the structure for switching on and off electricity, the operation difficulty is very high, and the hands of people can be easily scratched. In addition, the mode of pressing or toggle switch is still adopted to realize the power on-off of unmanned aerial vehicle power. However, the driving circuit is required to be equipped in the mode of pressing the switch, which not only increases the cost of the unmanned aerial vehicle, but also increases the volume and weight of the unmanned aerial vehicle, so that the load of the unmanned aerial vehicle is increased and cannot be compensated. The over-current capability of the toggle switch is relatively weak, the switch is easy to burn under the condition that large current passes through, and other models are hardly suitable except for a miniature unmanned aerial vehicle.

SUMMERY OF THE UTILITY MODEL

The to-be-solved problem of the utility model is to provide an unmanned aerial vehicle power supply mechanism of break-make power fast, this power supply mechanism can the fast break-make power, and the operation is very simple, can hardly increase unmanned aerial vehicle's volume, weight and cost moreover, the condition of burning loss can not appear yet, applicable unmanned aerial vehicle in whole models.

In order to solve the problems, the following technical scheme is adopted:

the utility model discloses an unmanned aerial vehicle power supply mechanism that can break-make power fast includes unmanned aerial vehicle's frame, has the power in this frame. The unmanned aerial vehicle lifting device is characterized in that a handle used for lifting the unmanned aerial vehicle is arranged on the rack, a lifting ring is arranged on the inner side of the handle, and a sliding block is connected to the lower portion of the lifting ring. The top plate of the rack is provided with a sliding hole at the position corresponding to the lifting ring, the sliding block of the lifting ring extends into the sliding hole, and the sliding block and the sliding hole are in vertical sliding fit. The inside below of slide opening of frame is fixed with the electrically conductive connecting plate, the input of this electrically conductive connecting plate with the power links to each other, the output is used for linking to each other with unmanned aerial vehicle's power unit, and is open circuit between input and output, the bottom of slider has the electric conductor that is used for making the input of electrically conductive connecting plate and output switch on.

The conductive connecting plate is provided with a double-hole conductive socket, one jack of the conductive socket is electrically connected with the input end, and the other jack of the conductive socket is electrically connected with the output end. The electric conductor of slider bottom is the electrically conductive plug of twin columns, and when the slider moved down to electrically conductive plug insert electrically conductive socket in, the input and the output of electrically conductive connecting plate switched on, the power supplies power to unmanned aerial vehicle's power unit.

The utility model discloses a further improvement scheme is there is the draw runner at the both ends of power, and there is the spout corresponding position department in the frame for the power can insert in the spout of frame through its draw runner. And one surface of the power supply, which is opposite to the rack, is provided with a conductive slot, and a conductive inserting column is arranged at a corresponding position of the rack and is connected with the input end of the conductive connecting plate. When the power supply is arranged in the rack, the conductive inserting column of the rack is inserted into the conductive inserting groove of the power supply, so that the power supply is communicated with the conductive connecting plate. This structure can realize the fast loading and unloading of power and unmanned aerial vehicle frame, and the operation is more convenient.

The utility model discloses a further improvement scheme is there is the lock ear at the both ends of power surface, and the corresponding position of frame has the screw, and when the frame was packed into to the power, the accessible bolt was fixed the lock ear of power in corresponding screw department. This structure can be with power locking in the unmanned aerial vehicle frame, increases the joint strength of power and frame for power supply mechanism is more stable.

By adopting the scheme, the method has the following advantages:

the utility model discloses an unmanned aerial vehicle power supply mechanism that can break-make power fast is provided with the handle that is used for carrying putting unmanned aerial vehicle in the frame, and there is the bail the inboard of handle, and the sub-unit connection of bail has the slider. The top plate of the rack is provided with a sliding hole at the position corresponding to the lifting ring, the sliding block of the lifting ring extends into the sliding hole, and the sliding block and the sliding hole are in vertical sliding fit. The inside below of slide opening of frame is fixed with the electrically conductive connecting plate, the input of this electrically conductive connecting plate with the power links to each other, the output is used for linking to each other with unmanned aerial vehicle's power unit, and is open circuit between input and output, the bottom of slider has the electric conductor that is used for making the input of electrically conductive connecting plate and output switch on. The power supply mechanism is arranged on the body of the unmanned aerial vehicle, when the unmanned aerial vehicle needs to be started, a user only needs to hold the handle by one hand and push the lifting ring downwards by virtue of force, so that the electric conductor on the sliding block at the lower part of the lifting ring is inserted into the conductive connecting plate, the input end and the output end of the lifting ring are conducted, and the power supply can supply power to the power mechanism; when the machine needs to be shut down, the handle is held by one hand, then the lifting ring is lifted upwards by virtue of force, the conductor on the sliding block at the lower part of the lifting ring is separated from the conductive connecting plate, the input end is disconnected with the output end, and the connection between the power supply and the power mechanism can be cut off. When the power supply mechanism is adopted to switch on or off the power supply, the power supply mechanism does not need to be disassembled, and does not need to act in a machine body, so that the operation is very simple and convenient. Simultaneously, this structure need not to be equipped with drive circuit, can not increase unmanned aerial vehicle's volume, weight and cost hardly, also can not burn any part when the heavy current passes through, applicable unmanned aerial vehicle in all models.

Drawings

Fig. 1 is a schematic structural diagram of the power supply mechanism of the unmanned aerial vehicle capable of rapidly switching on and off the power supply;

fig. 2 is the utility model discloses a but unmanned aerial vehicle power supply mechanism's of quick break-make power three-dimensional explosion schematic diagram.

Detailed Description

The present invention will be described in further detail with reference to the accompanying drawings.

As shown in fig. 1 and fig. 2, the utility model discloses an unmanned aerial vehicle power supply mechanism that can break-make power supply fast includes unmanned aerial vehicle's frame 1, has power 2 in this frame 1. There is the handle 3 that is used for carrying putting unmanned aerial vehicle in the frame 1, and there is a bail 5 in the inboard of handle 3, and the sub-unit connection of bail 5 has slider 6. A sliding hole is formed in the top plate of the machine frame 1 at the position corresponding to the lifting ring 5, the sliding block 6 of the lifting ring 5 extends into the sliding hole, and the sliding block and the sliding hole are in vertical sliding fit. The utility model discloses a power supply, including frame 1, power supply 2, slider 6, frame 1, the below of inside slide opening is fixed with conductive connection board 4, the input of this conductive connection board 4 with power 2 links to each other, the output is used for linking to each other with unmanned aerial vehicle's power unit, and is open circuit between input and output, the bottom of slider 6 has the electric conductor that is used for making conductive connection board 4's input and output switch on.

The conductive connecting plate 4 is provided with a double-hole conductive socket 8, one jack of the conductive socket 8 is electrically connected with the input end, and the other jack is electrically connected with the output end. The electric conductor of 6 bottoms of slider is the electrically conductive plug 7 of twin columns, and when slider 6 moves down to electrically conductive plug 7 and inserts electrically conductive socket 8 in, the input and the output of electrically conductive connecting plate 4 switch on, power 2 supplies power to unmanned aerial vehicle's power unit.

In this embodiment, there are the draw runner 9 at the both ends of power 2, there is the spout corresponding position department on the frame 1 for power 2 can insert in the spout of frame 1 through its draw runner 9. One side of the power supply 2, which is opposite to the rack 1, is provided with a conductive slot 10, a conductive inserting column 11 is arranged at a corresponding position of the rack 1, and the conductive inserting column 11 is connected with the input end of the conductive connecting plate 4. When the power supply 2 is installed in the rack 1, the conductive insertion posts 11 of the rack 1 are inserted into the conductive insertion slots 10 of the power supply 2, so that the power supply 2 is communicated with the conductive connecting plate 4. This structure can realize the fast loading and unloading of power 2 and unmanned aerial vehicle frame 1, and the operation is more convenient.

Two ends of the outer surface of the power supply 2 are provided with locking lugs 13, corresponding positions of the rack 1 are provided with screw holes 12, and when the power supply 2 is installed in the rack 1, the locking lugs 13 of the power supply 2 can be fixed at the corresponding screw holes 12 through bolts. This structure can be with power 2 locking in unmanned aerial vehicle frame 1, increases the joint strength of power 2 and frame 1 for power supply mechanism is more stable.

During the use, install this power supply mechanism on unmanned aerial vehicle's the fuselage. When the power mechanism needs to be started, the power supply 2 can supply power to the power mechanism only by holding the handle 3 with one hand and pushing the lifting ring 5 downwards by virtue of force to enable the conductive plug 7 on the sliding block 6 at the lower part of the lifting ring to be inserted into the conductive socket 8 of the conductive connecting plate 4 in the machine frame 1; when the machine needs to be shut down, the handle 3 is held by a single hand, the lifting ring 5 is lifted upwards by virtue of force, the conductive plug 7 on the lower sliding block 6 is separated from the conductive socket 8 of the conductive connecting plate 4 in the machine frame 1, and then the connection between the power supply 2 and the power mechanism can be cut off. When the power supply mechanism is adopted to switch on or off the power supply 2, disassembly is not needed, and the power supply mechanism does not need to act in a machine body, so that the operation is very simple and convenient. Simultaneously, this structure need not to be equipped with drive circuit, can not increase unmanned aerial vehicle's volume, weight and cost hardly, also can not burn any part when the heavy current passes through, applicable unmanned aerial vehicle in all models.

Claims

1. An unmanned aerial vehicle power supply mechanism capable of rapidly switching on and off a power supply comprises a frame (1) of an unmanned aerial vehicle, wherein a power supply (2) is arranged in the frame (1); the unmanned aerial vehicle lifting device is characterized in that a handle (3) used for lifting and placing the unmanned aerial vehicle is arranged on the rack (1), a lifting ring (5) is arranged on the inner side of the handle (3), and a sliding block (6) is connected to the lower part of the lifting ring (5); a sliding hole is formed in the top plate of the rack (1) at the position corresponding to the lifting ring (5), a sliding block (6) of the lifting ring (5) extends into the sliding hole, and the sliding block and the sliding hole are in vertical sliding fit; the utility model discloses a unmanned aerial vehicle, including frame (1), the below of inherent slide opening of frame (1) is fixed with electrically conductive connecting plate (4), the input of this electrically conductive connecting plate (4) with power (2) link to each other, the output is used for linking to each other with unmanned aerial vehicle's power unit, and is between input and output and opens circuit, the bottom of slider (6) has the electric conductor that is used for making the input of electrically conductive connecting plate (4) and output switch on.

2. The unmanned aerial vehicle power supply mechanism capable of rapidly switching on and off the power supply according to claim 1, wherein the conductive connecting plate (4) is provided with a double-hole conductive socket (8), one jack of the conductive socket (8) is electrically connected with the input end, and the other jack is electrically connected with the output end; the electric conductor of slider (6) bottom is two electrically conductive plugs (7) of post, when slider (6) move down to electrically conductive plug (7) insert in electrically conductive socket (8), the input and the output of electrically conductive connecting plate (4) switch on, power (2) are to unmanned aerial vehicle's power unit power supply.

3. The unmanned aerial vehicle power supply mechanism capable of rapidly switching on and off the power supply according to claim 1 or 2, characterized in that two ends of the power supply (2) are provided with sliding strips (9), and a sliding groove is formed in a corresponding position on the rack (1), so that the power supply (2) can be inserted into the sliding groove of the rack (1) through the sliding strips (9); one surface of the power supply (2) opposite to the rack (1) is provided with a conductive slot (10), a conductive inserting column (11) is arranged at the corresponding position of the rack (1), and the conductive inserting column (11) is connected with the input end of the conductive connecting plate (4); when the power supply (2) is arranged in the rack (1), the conductive inserting column (11) of the rack (1) is inserted into the conductive inserting groove (10) of the power supply (2), so that the power supply (2) is communicated with the conductive connecting plate (4).

4. The unmanned aerial vehicle power supply mechanism of power of can switching on and shutting down fast of claim 3, characterized in that there is lock ear (13) at the both ends of power (2) surface, and the corresponding position of frame (1) has screw (12), when frame (1) was packed into to power (2), can fix the lock ear (13) of power (2) in corresponding screw (12) department through the bolt.