CN207578412U - Battery replacement device - Google Patents
Battery replacement device Download PDFInfo
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- CN207578412U CN207578412U CN201721709475.3U CN201721709475U CN207578412U CN 207578412 U CN207578412 U CN 207578412U CN 201721709475 U CN201721709475 U CN 201721709475U CN 207578412 U CN207578412 U CN 207578412U
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- Prior art keywords
- battery
- mechanical arm
- replacement device
- battery replacement
- aircraft
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Abstract
The utility model provides a kind of battery replacement device, the battery replacement device is used to replace the battery in aircraft, the battery replacement device includes control platform, first mechanical arm, second mechanical arm and conveying mechanism, the control platform has a hollow cavity, the fixing end fixing device of first mechanical arm is on the bottom surface of the hollow cavity, the control platform also has an accommodating chamber for accommodating the conveying mechanism, the accommodating chamber is interconnected with the hollow cavity, the fixing end of the conveying mechanism is fixed on the bottom surface of the accommodating chamber, the fixing end fixing device of second mechanical arm is on the end face of the accommodating chamber, multiple batteries can be placed in the first end face of the conveying mechanism.Battery replacement device provided by the utility model can automatically take out used battery in aircraft, and will be filled in battery compartment of the new cell apparatus of electricity in aircraft, and replacement speed is fast, efficient, without manual operation.
Description
Technical field
The utility model is related to vehicle technology field more particularly to a kind of battery replacement devices.
Background technology
The replacement of battery in existing aircraft, mainly by the power switch of operating personnel elder generation long-press battery, to close
After the power supply for powering off pond, then battery used in aircraft is taken out manually.Then it will be filled with the new battery of electricity manually again
Device is in the battery compartment of aircraft, and the power switch of manual long-press battery, so that aircraft electrifying startup, manually more
It is low to change battery efficiency, and inconvenient.
Utility model content
In view of this, the utility model aim is to provide a kind of battery replacement device, can automatically take out in aircraft
Used battery, and will be filled in battery compartment of the new cell apparatus of electricity in aircraft, replacement speed is fast, efficient,
Without manual operation.
The utility model provides a kind of battery replacement device, and the battery replacement device is used to replace the electricity in aircraft
Pond, the battery replacement device include control platform, the first mechanical arm, the second mechanical arm and conveying mechanism, the control
Platform has a hollow cavity, and the fixing end fixing device of first mechanical arm is on the bottom surface of the hollow cavity, the control
Platform processed also has an accommodating chamber for accommodating the conveying mechanism, and the accommodating chamber is interconnected with the hollow cavity, described defeated
The fixing end of mechanism is sent to be fixed on the bottom surface of the accommodating chamber, the fixing end fixing device of second mechanical arm is described
Multiple batteries can be placed on the end face of accommodating chamber, in the first end face of the conveying mechanism.
Specifically, the battery replacement device further includes control module, and the control module is mechanical with described first respectively
Arm and the electrical connection of the second mechanical arm.
Specifically, the housing of the control platform is equipped with key zone and viewing area, and the key zone is arranged on prime number and shows
Show the both sides in area.
Specifically, the key zone is equipped with multiple buttons, and multiple buttons are electrically connected with the control module.
Specifically, the first transmission mechanism, first transmission mechanism and the control are equipped in first mechanical arm
Module is electrically connected, first mechanical arm to be driven to capture the claw portion of the aircraft.
Specifically, the second transmission mechanism, second transmission mechanism and the control are equipped in second mechanical arm
Module is electrically connected, second mechanical arm to be driven to capture the battery in the aircraft or the electricity on the conveying mechanism
Pond.
Specifically, it after the control module receives battery altering signal, controls described in the first transmission mechanism driving
First mechanical arm captures the claw portion of the aircraft, and the aircraft is placed in opposite with second mechanical arm
On position.
Specifically, the control module is after the first feedback signal that first mechanical arm is sent is received, control
Second transmission mechanism drives the battery to be replaced of battery compartment of the second mechanical arm grabbing device in the aircraft,
And the battery to be replaced is placed on the conveying mechanism.
Specifically, the control module is after the second feedback signal of the conveying mechanism is received, control described second
Transmission mechanism driving the second mechanical arm crawl is placed on the conveying mechanism and the first battery of electricity abundance, and will
First cell apparatus is in the battery compartment of the aircraft, and second mechanical arm depresses the power supply of the aircraft
It switchs and keeps preset time.
Specifically, the battery replacement device further includes charging module, and the charging module is arranged on the conveying mechanism
On, to charge to the battery on the conveying mechanism.
It can be seen that battery replacement device provided in this embodiment, the first mechanical arm and the are controlled by control platform
Two mechanical arms are operated accordingly, can automatically take out used battery in aircraft, and will be filled with the new of electricity
In battery compartment of the cell apparatus in aircraft, replacement speed is fast, efficient, without manual operation.
Above and other objects, features and advantages to allow the utility model can be clearer and more comprehensible, preferable reality cited below particularly
Example is applied, and coordinates institute's accompanying drawings, is described in detail below.
Description of the drawings
Fig. 1 and Fig. 2 is the dimensional structure diagram of battery replacement device that the utility model embodiment provides.
Fig. 3 is the main structure diagram of battery replacement device that the utility model embodiment provides.
Fig. 4 is the overlooking the structure diagram of battery replacement device that the utility model embodiment provides.
Specific embodiment
Further to illustrate that the utility model is the technological means and effect that realization expected purpose is taken, below in conjunction with
Attached drawing and preferred embodiment, to according to the utility model proposes the specific embodiment of battery replacement device, method, step,
Structure, feature and effect are described in detail as after.
Aforementioned and other technology contents, feature and effect in relation to the utility model, following cooperation with reference to schema compared with
It can clearly be presented in the detailed description of good embodiment.By the explanation of specific embodiment, when can be to the utility model
Reach technological means that expected purpose taken and effect be able to more deeply and it is specific understand, however institute's accompanying drawings only carry
For reference with purposes of discussion, not it is used for limiting the utility model.
It please refers to Fig.1 and Fig. 2, Fig. 1 and Fig. 2 is the solid of battery replacement device 100 that the utility model embodiment provides
Structure diagram.Battery replacement device 100 provided in this embodiment can be, but not limited to the battery for replacing in aircraft 200
50.As shown in Figures 1 and 2, specifically, in the present embodiment, battery replacement device 100 includes the 10, first machinery of control platform
Arm 20, the second mechanical arm 30 and conveying mechanism 40.Control platform 10 has a hollow cavity 102.First mechanical arm 20
Fixing end fixing device is on the bottom surface of hollow cavity 102 103.Control platform 10 also has an accommodating chamber for accommodating conveying mechanism 40
(figure does not indicate), accommodating chamber is interconnected with hollow cavity 102, and the fixing end of conveying mechanism 40 is fixed on the end face of accommodating chamber (figure
It is not shown) on, for the fixing end fixing device of the second mechanical arm 30 on the end face of accommodating chamber, the first of conveying mechanism 40 is flat
Multiple batteries 50 can be placed on face.
Specifically, in the present embodiment, it can be, but not limited to downward by the middle part of the first end face 101 of control platform 10
Recess forms the hollow cavity 102 of control platform 10, and hollow cavity 102 is cylindric, and the diameter of section of hollow cavity 102 is more than flight
The outer diameter of device 200.Specifically, one is additionally provided on the inner wall of hollow cavity 102 can accommodate 40 and second mechanical arm of conveying mechanism
30 accommodating chamber, accommodating chamber are interconnected with hollow cavity 102.Specifically, the bottom on the front end face of the shell of control platform 10
Portion extends outward to form a boss (figure does not indicate), and key zone 104 and viewing area 105, and button are equipped on the end face of boss
Area 104 can be, but not limited to be arranged on the both sides of viewing area 105.Specifically, in the present embodiment, in key zone 104 can with but
It is not limited to be equipped with multiple buttons 106 comprising battery altering button.
Specifically, in the present embodiment, battery replacement device 100 further includes a control module (not shown).Control mould
Block assembly is in control platform 10, and one end of control module is electrically connected respectively with the first mechanical arm 20 and the second mechanical arm 30
It connects, the other end of control module is electrically connected respectively with multiple buttons 106.
Specifically, in the present embodiment, the first transmission mechanism (not shown) is equipped in the first mechanical arm 20, first passes
Motivation structure is electrically connected with control module, to drive the claw portion 202 of the first mechanical arm 20 crawl aircraft 200.First machinery
Arm 20 further includes multiple arms (figure does not indicate), the first jaw components 22 and pedestal (figure does not indicate), the first transmission mechanism packet
Include multiple motors (not shown).Specifically, multiple arms are mutually flexibly connected from beginning to end to form the first mechanical arm 20, multiple
Motor is respectively used to the claw portion 202 for driving corresponding arm rotation or the first jaw components 22 crawl aircraft 200.First machine
The fixing end of tool arm 20 is fixedly connected with pedestal, and pedestal can be, but not limited to the bottom surface 103 by fastener and hollow cavity 102
It is fixedly connected.The free end of first mechanical arm 20 is flexibly connected with the first jaw components 22.Multiple motors are and control module
Electrical connection, to receive corresponding control signal, so as to drive corresponding arm rotation or the first jaw components 22 crawl aircraft
200 claw portion 202.Specifically, in the present embodiment, the first jaw components 22 crawl aircraft of the first mechanical arm 20
During 200 claw portion 202, the free end holding horizontal direction of the first mechanical arm 20, and the claw portion 202 of aircraft 200
Center is located on the center line of hollow cavity 102.
Please also refer to Fig. 3 and Fig. 4, Fig. 3 is the main view knot of battery replacement device 100 that the utility model embodiment provides
Structure schematic diagram, Fig. 4 are the overlooking the structure diagram of battery replacement device 100 that the utility model embodiment provides.Such as Fig. 3 and figure
Shown in 4, specifically, in the present embodiment, the second transmission mechanism (not shown), the second transmission are equipped in the second mechanical arm 30
Mechanism is electrically connected with control module, to drive the battery 50 or conveying mechanism 40 in the second mechanical arm 30 crawl aircraft 200
On battery 50.It is (not shown that second mechanical arm 30 further includes multiple arms (figure does not indicate), the second jaw components 32 and pedestal
Go out), the first transmission mechanism includes multiple motors (not shown).Specifically, multiple arms are mutually flexibly connected to form from beginning to end
Second mechanical arm 30, multiple motors are respectively used to that corresponding arm motion or the second jaw components 32 of driving is driven to capture
First battery of the electricity abundance on the battery or conveying mechanism 40 to be replaced of aircraft 200.The fixation of first mechanical arm 20
End is fixedly connected with pedestal, and pedestal can be, but not limited to be fixedly connected with the end face of accommodating chamber by fastener.Second manipulator
The free end of arm 30 is flexibly connected with the second jaw components 32.Multiple motors are electrically connected with control module, corresponding to receive
Signal is controlled, so as to which corresponding arm motion or the second jaw components 32 be driven to capture battery to be replaced or the first battery.Specifically
Ground, in the present embodiment, when the second jaw components 32 of the second mechanical arm 30 capture battery or the first battery to be replaced, second
The free end of mechanical arm 30 keeps horizontal direction.
Specifically, in the present embodiment, the fixing end of conveying mechanism 40 is fixed on by fastener on the end face of accommodating chamber.
Output mechanism includes first end face 42, and first end face 42 is positioned in annular shape, multiple first batteries in first end face 42.
Further, in one embodiment, battery replacement device 100 further includes a charging module (not shown), fills
Electric module is arranged on to charge to battery to be replaced in first end face 42, specifically, charging module respectively with control platform
10 power end and control module electrical connection.
Specifically, in the present embodiment, after control module receives battery altering signal, control the first transmission mechanism driving
First mechanical arm 20 captures the claw portion 202 of aircraft 200, and aircraft 200 is placed in the second mechanical arm 30 relatively
Position on.Further, control module is after the first feedback signal for receiving the transmission of the first mechanical arm 20, control second
Transmission mechanism drives 30 grabbing device of the second mechanical arm in the battery to be replaced of the battery compartment of aircraft 200, and will be to be replaced
Battery is placed on conveying mechanism 40.Further, control module is after the second feedback signal of conveying mechanism 40 is received,
Control the second transmission mechanism that the crawl of the second mechanical arm 30 is driven to be placed on conveying mechanism 40 and the first battery of electricity abundance,
And by the first cell apparatus in the battery compartment of aircraft 200, and the power switch of the second mechanical arm 30 pressure aircraft 200
And keep preset time.
Specifically, in the present embodiment, the battery altering in operating personnel press the key zone 104 of control platform 10 by
During key, control module will receive the battery altering signal of battery altering button transmission, and be obtained according to the battery altering signal processing
Multiple motors in the first mechanical arm 20 are sent to first control signal, and by first control signal, to drive the first machine
The jaw components of tool arm 20 capture the claw portion 202 of aerial aircraft 200, and the aircraft 200 is moved to and second
30 corresponding position of mechanical arm, and the second jaw components 32 of the second mechanical arm of battery compartment face 30 of aircraft 200.
When aircraft 200 is moved to the second 30 corresponding position of mechanical arm by the first mechanical arm 20, the first mechanical arm
20 will send the first feedback signal to control module.Control module handles to obtain second control signal according to the first feedback signal,
And be sent to second control signal in multiple motors of the second mechanical arm 30, to drive the second mechanical arm 30 so as to fly
Battery to be replaced is captured in battery compartment in device 200, and the battery to be replaced of taking-up is placed on conveying mechanism 40 and charging
On the corresponding position of module, to charge to battery to be replaced.Charging module will after charging to battery to be replaced
The second feedback signal is sent to control module.Control module handles to obtain third control letter according to the second feedback signal received
Number, and third control signal is sent in multiple motors in the second mechanical arm 30, to drive the second mechanical arm 30
Second jaw components 32 are captured from conveying mechanism 40 with the first battery at full charge, so as to which the first battery is inserted into flight
In battery compartment in device 200, the first battery is inserted into the battery of aircraft 200 in the second jaw components 32 by the second mechanical arm 30
It depresses the power switch of aircraft 200 simultaneously behind storehouse and keeps preset time, to start aircraft 200.Second mechanical arm 30
Third feedback signal is sent to control module after the power switch preset time of pressure aircraft 200, control module is according to connecing
The third feedback signal received handles to obtain the 4th control signal, and the 4th control signal is sent to the first mechanical arm 20
In multiple motors, to drive the first mechanical arm 20 that aircraft 200 is moved to outside hollow cavity 102, so as to fulfill aircraft 200
Electrification extract battery 50, and the first battery that will be filled with electricity is inserted into the battery compartment in aircraft 200, with can be automatically fast
Speed replaces battery 50.
It can be seen that battery replacement device 100 provided in this embodiment, the first mechanical arm is controlled by control platform 10
20 with the second mechanical arm 30 carry out it is corresponding operate, can automatically take out used battery 50 in aircraft 200, and will
In the battery compartment of 50 device of new battery at full charge in aircraft 200, replacement speed is fast, efficient, without manual operation.
More than, be only the utility model preferred embodiment, limit in any form not is made to the utility model
System although the utility model has been disclosed with preferred embodiment as above, is not limited to utility model, and any to be familiar with sheet special
The technical staff of industry is not departing from the range of utility model technical solution, is being made when using the technology contents of the disclosure above
Perhaps the equivalent embodiment of equivalent variations is changed or is modified to, as long as being without departing from utility model technical solution content, according to practical
It is new to still fall within this practicality for any simple modification, equivalent change and modification that novel technical spirit makees above example
In the range of type technical solution.
Claims (10)
1. a kind of battery replacement device, which is characterized in that the battery replacement device is used to replace the battery in aircraft, described
Battery replacement device includes control platform, the first mechanical arm, the second mechanical arm and conveying mechanism, and the control platform has
One hollow cavity, the fixing end fixing device of first mechanical arm is on the bottom surface of the hollow cavity, and the control platform is also
The accommodating chamber for accommodating the conveying mechanism with one, the accommodating chamber are interconnected with the hollow cavity, the conveying mechanism
Fixing end is fixed on the bottom surface of the accommodating chamber, and the fixing end fixing device of second mechanical arm is in the accommodating chamber
Multiple batteries can be placed on end face, in the first end face of the conveying mechanism.
2. battery replacement device according to claim 1, which is characterized in that the battery replacement device further includes control mould
Block, the control module are electrically connected respectively with first mechanical arm and the second mechanical arm.
3. battery replacement device according to claim 2, which is characterized in that the housing of the control platform is equipped with button
Area and viewing area, the key zone are arranged on the both sides of the viewing area.
4. battery replacement device according to claim 3, which is characterized in that the key zone is equipped with multiple buttons, more
A button is electrically connected with the control module.
5. battery replacement device according to claim 2, which is characterized in that first is equipped in first mechanical arm and is passed
Motivation structure, first transmission mechanism are electrically connected with the control module, to drive the first mechanical arm crawl is described to fly
The claw portion of row device.
6. battery replacement device according to claim 5, which is characterized in that second is equipped in second mechanical arm and is passed
Motivation structure, second transmission mechanism are electrically connected with the control module, to drive the second mechanical arm crawl is described to fly
The battery on battery or the conveying mechanism in row device.
7. battery replacement device according to claim 6, which is characterized in that the control module receives battery altering letter
After number, first transmission mechanism is controlled to drive the claw portion of the first mechanical arm crawl aircraft, and by described in
Aircraft is placed on the position opposite with second mechanical arm.
8. battery replacement device according to claim 7, which is characterized in that the control module is receiving described first
After the first feedback signal that mechanical arm is sent, second transmission mechanism is controlled to drive the second mechanical arm grabbing device
It is placed on the conveying mechanism in the battery to be replaced of the battery compartment of the aircraft, and by the battery to be replaced.
9. battery replacement device according to claim 8, which is characterized in that the control module is receiving the conveying
After second feedback signal of mechanism, control second transmission mechanism that the second mechanical arm crawl is driven to be placed on described defeated
It send in mechanism and the first battery of electricity abundance, and by first cell apparatus in the battery compartment of the aircraft, and institute
The second mechanical arm is stated to depress the power switch of the aircraft and keep preset time.
10. battery replacement device according to claim 1, which is characterized in that the battery replacement device further includes charging
Module, the charging module are arranged on the conveying mechanism, to charge to the battery on the conveying mechanism.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721709475.3U CN207578412U (en) | 2017-12-06 | 2017-12-06 | Battery replacement device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721709475.3U CN207578412U (en) | 2017-12-06 | 2017-12-06 | Battery replacement device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207578412U true CN207578412U (en) | 2018-07-06 |
Family
ID=62736489
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721709475.3U Active CN207578412U (en) | 2017-12-06 | 2017-12-06 | Battery replacement device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207578412U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108945489A (en) * | 2018-08-01 | 2018-12-07 | 深圳市旭发智能科技有限公司 | A kind of installation method of unmanned machine battery |
-
2017
- 2017-12-06 CN CN201721709475.3U patent/CN207578412U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108945489A (en) * | 2018-08-01 | 2018-12-07 | 深圳市旭发智能科技有限公司 | A kind of installation method of unmanned machine battery |
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