CN109703765A - A kind of improvement structure of multi-rotor unmanned aerial vehicle battery system - Google Patents
A kind of improvement structure of multi-rotor unmanned aerial vehicle battery system Download PDFInfo
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- CN109703765A CN109703765A CN201811629461.XA CN201811629461A CN109703765A CN 109703765 A CN109703765 A CN 109703765A CN 201811629461 A CN201811629461 A CN 201811629461A CN 109703765 A CN109703765 A CN 109703765A
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- storage box
- card slot
- battery
- aerial vehicle
- unmanned aerial
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Abstract
The invention discloses a kind of improvement structures of multi-rotor unmanned aerial vehicle battery system, it include: body, the body lower end is equipped with bracket, groove is equipped in the middle part of the body lower end, the bottom portion of groove is equipped with sheet metal, the side wall of the groove is equipped with card slot, described card slot one end is equipped with through-hole, the through-hole is connected to card slot, the storage box is equipped in the groove, the storage box bottom sidewall is equipped with the buckle to match with card slot, is equipped with multiple partitions inside the storage box, the storage box is separated into multiple battery storage chambers by the partition.The present invention cooperates fixed battery by the storage box and lid, battery storage chamber can randomly place even number battery and be energized, the energy is saved, pass through the cooperation fixed storage box of card slot and buckle again, keep device fixed more firm on body, disassembly, installation are more convenient, and the battery of unmanned plane is more convenient for fix.
Description
Technical field
The present invention relates to changing for unmanned plane auxiliary device technical field more particularly to a kind of multi-rotor unmanned aerial vehicle battery system
Into structure.
Background technique
With the progress of automated control technology, common multi-rotor unmanned aerial vehicle has become very easy on the market at present
Upper hand, ordinary people only need to be after simply training, so that it may manipulate it and realize smooth flight in simple environment, this is certain
The use scope that multi-rotor unmanned aerial vehicle has been expanded in degree makes more and more people start to consider for multi-rotor unmanned aerial vehicle to be applied to
All kinds of fields.The miniaturization of sensor technology is even more to be pushed further into this development, by various sensor miniaturizations, so
Rear mount becomes a main trend of present Development of UAV in multi-rotor unmanned aerial vehicle.
The fuselage of existing unmanned plane is smooth, without three-dimension curved surface, and has reserved more screw hole and data transmission socket,
Different tasks is executed convenient for users to carrying the module oneself designed and produced.Unmanned plane be by battery mounted thereto come
There is provided what energy was operated, but the capacity of matched battery is smaller, cannot support unmanned plane long-play.It is existing
Quadrotor drone be powered using two pieces of batteries, one piece of battery and fly control connection, provide the electricity of the battery, voltage,
Life information, and be each control chip on fuselage and motor power supply；And another piece of battery be only motor power supply, quadrotor without
For man-machine flying platform after installing original-pack accessory, the actual flying time using two pieces of batteries is shorter, after plug-in other equipment,
Its flight time can further shorten；Furthermore if necessary to need to its power when installing larger plug-in device on the platform
It is replaced, this will cause its actual flying time and is difficult to meet the actual needs；And existing cell fixing device without
Method carries out the increase and decrease of battery according to unmanned plane weight, the self weight of unmanned plane is increased, so increasing the energy consumption of unmanned plane.
Summary of the invention
The purpose of the present invention is to provide a kind of improvement structure of multi-rotor unmanned aerial vehicle battery system, battery storage chamber can be with
Machine is placed even number battery and is energized, and has the advantages that have saved the energy, has saved the energy, solves unmanned plane own wt
The problem of, the quantity of unmanned self-contained battery can be voluntarily adjusted as needed.
A kind of improvement structure of multi-rotor unmanned aerial vehicle battery system, comprising: body, the body lower end are equipped with bracket, institute
It states and is equipped with groove in the middle part of body lower end, the bottom portion of groove is equipped with sheet metal, and the side wall of the groove is equipped with card slot, the card
Slot one end is equipped with through-hole, and the through-hole is connected to card slot, and the storage box is equipped in the groove, is set in the storage box bottom sidewall
There is the buckle to match with card slot, is equipped with multiple partitions inside the storage box, the storage box is separated into multiple electricity by the partition
Pond storage chamber；The storage box lower end is equipped with lid, and the lid is connected with the storage box by hinge, the inner wall of the lid
It is equipped with sheet metal, the outside of the sheet metal is equipped with sealing ring, and the lid lower end outer wall is equipped with key of uncapping, described to uncap
Key lower end is equipped with connecting column, and the connecting column side wall is equipped with spring, and the connecting column other end is equipped with movable button, described to uncap
Key, movable button two sidewalls on be equipped with block.
Further, the side wall of the storage box is equipped with the fixing groove to match with movable button.
Further, the storage box bottom is equipped with electrode slice, and described electrode slice one end is connect with multiple battery storage chambers,
The connection of the sheet metal of the electrode slice other end and bottom portion of groove.
Further, the moving range of the key of uncapping is 0~3cm.
Further, one layer of underwater paint is coated on the storage outer box wall.
Further, the sheet metal is using made by metallic copper.
Compared with the prior art, the invention has the beneficial effects that: groove is equipped in the middle part of body lower end, in recess sidewall
Equipped with card slot, the buckle in the storage box enters in sliding slot from through-hole first, and then rotating clockwise can be completed the storage box
Fixed, lid can be uncapped key by pressing, and connecting column drives movable button to be detached from fixing groove, i.e., openable lid, inside the storage box
Be partitioned into multiple battery storage chambers, battery storage chamber for placing energy supply battery, can need to be flown according to unmanned plane away from
From the placement for carrying out battery, lid is closed, movable button is stuck in again under the action of the spring to be completed to fix in fixing groove, the storage box
The interior battery number placed is even number, and battery is that positive and negative intersection is placed, and the sheet metal on lid is connect with battery, is deposited
Storage box bottom electrode piece is also connect with battery, and electrode slice is connect with the sheet metal in groove, in the sheet metal and body in groove
Device electrical connection, that is, form complete closed circuit, energized to unmanned plane, the sealing ring on lid can prevent the rainy day from making
The entrance of moisture when industry, extends the service life of device；The present invention cooperates fixed battery by the storage box and lid, and battery is deposited
Storage chamber can randomly place even number battery and be energized, and save the energy, then pass through the cooperation fixed storage box of card slot and buckle,
Keep device fixed more firm on body, disassembly, installation are more convenient, and the battery of unmanned plane is more convenient for fix.
Detailed description of the invention
Attached drawing is used to provide further understanding of the present invention, and constitutes part of specification, with reality of the invention
It applies example to be used to explain the present invention together, not be construed as limiting the invention.In the accompanying drawings:
Fig. 1 is a kind of positive structure schematic of the improvement structure of multi-rotor unmanned aerial vehicle battery system proposed by the present invention.
Fig. 2 is a kind of top view of the improvement structure of multi-rotor unmanned aerial vehicle battery system proposed by the present invention.
Fig. 3 is the structural representation of the storage box in a kind of improvement structure of multi-rotor unmanned aerial vehicle battery system proposed by the present invention
Figure.
Fig. 4 is the structural representation of movable button in a kind of improvement structure of multi-rotor unmanned aerial vehicle battery system proposed by the present invention
Figure.
In figure: 1- body, 2- bracket, 3- the storage box, 4- lid, 5- hinge, 6- sheet metal, 7- card slot, 8- through-hole, 9- card
Button, 10- partition, 11- sealing ring, 12- are uncapped key, 13- connecting column, 14- spring, 15- movable button, 16- block.
Specific embodiment
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation description, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other
Embodiment shall fall within the protection scope of the present invention.
Referring to Fig.1-4, a kind of improvement structure of multi-rotor unmanned aerial vehicle battery system, comprising: body 1,1 lower end of body are equipped with
Bracket 2,1 lower end of body middle part are equipped with groove, and bottom portion of groove is equipped with sheet metal 6, and the side wall of groove is equipped with card slot 7, card slot 7 one
End is equipped with through-hole 8, and through-hole 8 is connected to card slot 7, and the storage box 3 is equipped in groove, and 3 bottom sidewall of the storage box is equipped with and 7 phase of card slot
It is matched to buckle 9, multiple partitions 10 are equipped with inside the storage box 3, the storage box 3 is separated into multiple battery storage chambers by partition 10；It deposits
3 lower end of storage box is equipped with lid 4, and lid 4 is connected with the storage box 3 by hinge 5, and the inner wall of lid 4 is equipped with sheet metal 6, gold
The outside for belonging to piece 6 is equipped with sealing ring 11, and the sheet metal 6 and 6 shape of bottom portion of groove sheet metal, specification on the inner wall of lid 4 are complete
Just as 4 lower end outer wall of lid is equipped with key 12 of uncapping, and equipped with connecting column 13,13 side wall of connecting column is equipped with for 12 lower end of key of uncapping
Spring 14,13 other end of connecting column be equipped with movable button 15, key 12 of uncapping, movable button 15 two sidewalls on be equipped with block 16；It deposits
The side wall of storage box 3 is equipped with the fixing groove to match with movable button 15；3 bottom of the storage box be equipped with electrode slice, electrode slice one end with
The sheet metal 6 of multiple battery storage chamber connections, the electrode slice other end and bottom portion of groove connects；Uncap key 12 moving range be 0
~3cm；One layer of underwater paint is coated on 3 outer wall of the storage box；Sheet metal 6 is using made by metallic copper.
Groove is equipped in the middle part of 1 lower end of body, recess sidewall is equipped with card slot 7, and the buckle 9 in the storage box 3 is first from through-hole 8
It enters in sliding slot 7, then rotates clockwise the fixation that the storage box 3 can be completed, lid 4 can be by pressing key 12 of uncapping, even
Connecing column 13 drives movable button 15 to be detached from fixing groove, i.e., openable lid 4 is divided into multiple batteries by partition 10 inside the storage box 3
Storage chamber, battery storage chamber can carry out the placement of battery according to the distance that unmanned plane need to fly, close for placing energy supply battery
Lid 4, movable button 15 is stuck in fixing groove again under the effect of spring 14 to be completed to fix, the battery that can be placed in the storage box 3
Number is even number, and battery is that positive and negative intersection is placed, and the sheet metal 6 on lid 4 is connect with battery, 3 bottom of the storage box electricity
Pole piece is also connect with battery, and electrode slice is connect with the sheet metal 6 in groove, the sheet metal 6 in groove and the electricity of the device in body 1
Connection, that is, form complete closed circuit, energized to unmanned plane, when the sealing ring 11 on lid 4 can prevent raining working
The entrance of moisture extends the service life of device；The present invention cooperates fixed battery, battery storage by the storage box 3 and lid 4
Chamber can randomly place even number battery and be energized, and save the energy, then the cooperation fixed storage box by card slot 7 and buckle 9
3, keep device fixed more firm on body 1, disassembly, installation are more convenient, and the battery of unmanned plane is more convenient for fix.
In use, removing the storage box 3 of 1 lower end of body, lid 4 is opened, successively positive and negative alternate places even number battery, closes
Upper cover body 4, then card slot 7 is passed through into through-hole 8, it is fixed in rotation to card slot 7；When taking-up, only need rotary buckle 9 counterclockwise to
It is extracted at through-hole 8, presses key 12 of uncapping, movable button 15 is separated with fixing groove, opens lid 4, takes out battery, which makes
With simple, it can be put into suitable battery number according to demand, alleviate the weight of unmanned plane, saved the energy.
Place is not described in detail by the present invention, is the well-known technique of those skilled in the art.
It although an embodiment of the present invention has been shown and described, for the ordinary skill in the art, can be with
A variety of variations, modification, replacement can be carried out to these embodiments without departing from the principles and spirit of the present invention by understanding
And modification, the scope of the present invention is defined by the appended.
Claims (6)
1. a kind of improvement structure of multi-rotor unmanned aerial vehicle battery system characterized by comprising body (1), the body (1)
Lower end is equipped with bracket (2), groove is equipped in the middle part of body (1) lower end, the bottom portion of groove is equipped with sheet metal (6), described recessed
The side wall of slot is equipped with card slot (7), and described card slot (7) one end is equipped with through-hole (8), and the through-hole (8) is connected to card slot (7), institute
It states in groove and is equipped with the storage box (3), the storage box (3) bottom sidewall is equipped with the buckle (9) to match with card slot (7), institute
It states and is equipped with multiple partitions (10) inside the storage box (3), the storage box (3) is separated into multiple battery storage chambers by the partition (10)；
The storage box (3) lower end is equipped with lid (4), and the lid (4) is connected with the storage box (3) by hinge (5), the lid
(4) inner wall is equipped with sheet metal (6), and the outside of the sheet metal (6) is equipped with sealing ring (11), outside lid (4) lower end
Wall is equipped with and uncaps key (12), and key of uncapping (12) lower end is equipped with connecting column (13), and connecting column (13) side wall is equipped with
Spring (14), connecting column (14) other end be equipped with movable button (15), the key of uncapping (12), movable button (15) two sidewalls
On be equipped with block (16).
2. a kind of improvement structure of multi-rotor unmanned aerial vehicle battery system according to claim 1, it is characterised in that: described to deposit
The side wall of storage box (3) is equipped with the fixing groove to match with movable button (15).
3. a kind of improvement structure of multi-rotor unmanned aerial vehicle battery system according to claim 1, it is characterised in that: described to deposit
Storage box (3) bottom is equipped with electrode slice, and described electrode slice one end connect with multiple battery storage chambers, the electrode slice other end with it is recessed
The sheet metal (6) of trench bottom connects.
4. a kind of improvement structure of multi-rotor unmanned aerial vehicle battery system according to claim 1, it is characterised in that: described to open
The moving range of Gai Jian (12) is 0~3cm.
5. a kind of improvement structure of multi-rotor unmanned aerial vehicle battery system according to claim 1, it is characterised in that: described to deposit
One layer of underwater paint is coated on storage box (3) outer wall.
6. a kind of improvement structure of multi-rotor unmanned aerial vehicle battery system according to claim 1, it is characterised in that: the gold
Belong to piece (6) using made by metallic copper.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811629461.XA CN109703765A (en) | 2018-12-28 | 2018-12-28 | A kind of improvement structure of multi-rotor unmanned aerial vehicle battery system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811629461.XA CN109703765A (en) | 2018-12-28 | 2018-12-28 | A kind of improvement structure of multi-rotor unmanned aerial vehicle battery system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109703765A true CN109703765A (en) | 2019-05-03 |
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ID=66259143
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811629461.XA Pending CN109703765A (en) | 2018-12-28 | 2018-12-28 | A kind of improvement structure of multi-rotor unmanned aerial vehicle battery system |
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Citations (7)
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| US20110281149A1 (en) * | 2010-05-14 | 2011-11-17 | Itt Manufacturing Enterprises, Inc. | Battery pack |
| CN204474341U (en) * | 2015-01-16 | 2015-07-15 | 陕西浩泽环保科技发展有限公司 | A kind of water-purifying machine lateral plate structure |
| CN204635859U (en) * | 2015-05-20 | 2015-09-16 | 浙江林炎集团有限公司 | Washable self-locking button Drinking cup lid |
| CN105939933A (en) * | 2015-11-30 | 2016-09-14 | 深圳市大疆创新科技有限公司 | Battery accommodating device, unmanned aerial vehicle and electronic device |
| CN206432302U (en) * | 2017-01-11 | 2017-08-22 | 无锡觅睿恪科技有限公司 | Unmanned plane power pack component |
| CN107600439A (en) * | 2017-09-26 | 2018-01-19 | 上海重塑能源科技有限公司 | A kind of long endurance unmanned aircraft electrical source of power device and unmanned plane |
| CN108807762A (en) * | 2018-06-12 | 2018-11-13 | 福建云众动力科技有限公司 | A kind of battery modules recombinating transformation |
-
2018
- 2018-12-28 CN CN201811629461.XA patent/CN109703765A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20110281149A1 (en) * | 2010-05-14 | 2011-11-17 | Itt Manufacturing Enterprises, Inc. | Battery pack |
| CN204474341U (en) * | 2015-01-16 | 2015-07-15 | 陕西浩泽环保科技发展有限公司 | A kind of water-purifying machine lateral plate structure |
| CN204635859U (en) * | 2015-05-20 | 2015-09-16 | 浙江林炎集团有限公司 | Washable self-locking button Drinking cup lid |
| CN105939933A (en) * | 2015-11-30 | 2016-09-14 | 深圳市大疆创新科技有限公司 | Battery accommodating device, unmanned aerial vehicle and electronic device |
| CN206432302U (en) * | 2017-01-11 | 2017-08-22 | 无锡觅睿恪科技有限公司 | Unmanned plane power pack component |
| CN107600439A (en) * | 2017-09-26 | 2018-01-19 | 上海重塑能源科技有限公司 | A kind of long endurance unmanned aircraft electrical source of power device and unmanned plane |
| CN108807762A (en) * | 2018-06-12 | 2018-11-13 | 福建云众动力科技有限公司 | A kind of battery modules recombinating transformation |
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Application publication date: 20190503 |
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