CN109148761A - A kind of unmanned plane battery compartment - Google Patents
A kind of unmanned plane battery compartment Download PDFInfo
- Publication number
- CN109148761A CN109148761A CN201810865067.XA CN201810865067A CN109148761A CN 109148761 A CN109148761 A CN 109148761A CN 201810865067 A CN201810865067 A CN 201810865067A CN 109148761 A CN109148761 A CN 109148761A
- Authority
- CN
- China
- Prior art keywords
- battery
- frame
- unmanned plane
- battery compartment
- lock part
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
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Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M50/00—Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
- H01M50/20—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02E60/10—Energy storage using batteries
Abstract
The embodiment of the present invention discloses a kind of unmanned plane battery compartment, comprising: frame, the elastic parts being arranged on the frame inner opposite end, at least one locking assembly for being oppositely arranged on the guide member of two sides in the frame and being arranged at the frame exhaust openings；The locking assembly includes: to be fixed at least one tight lock part at both ends and the pushing member for pushing the tight lock part flexible on the inside of the frame end；The guide member is the guide rod being fixed on the inside of the frame.The technical solution of the embodiment of the present invention can greatly improve the replacement efficiency of battery and the fixed effect of battery, and structure is simple, convenient for promoting.
Description
Technical field
The present invention relates to unmanned plane fields, more particularly to a unmanned plane battery compartment.
Background technique
With the development of unmanned air vehicle technique, unmanned plane is such as taken photo by plane, measures, is supervised also continuous using in daily life
Control etc..Current most of unmanned plane during flyings provide energy by battery, but the energy that battery can once provide is limited,
After unmanned plane completes flight, when not enough power supply, user is just needed to replace manually to unmanned machine battery, operated numerous
It is trivial, influence user experience.
However, present unmanned machine battery and battery box structure for the unmanned machine battery of installation settings are excessively single,
It is unfavorable for the replacement of battery, reduces the replacement efficiency of unmanned machine battery, be not easy to be widely used.
Summary of the invention
The purpose of the present invention is to solve the problems of the above-mentioned prior art, a kind of unmanned plane battery compartment, electricity are provided
Pond and unmanned plane.
The purpose of the present invention is achieved through the following technical solutions:
According to an aspect of the present invention, a kind of battery compartment of unmanned plane is designed, comprising: frame is arranged in the frame
Elastic parts on inner opposite end is oppositely arranged on the guide member of two sides in the frame and is arranged in the frame exhaust openings
At least one locking assembly at place；The locking assembly includes: be fixed at both ends on the inside of the frame end at least one
A tight lock part and pushing member for pushing the tight lock part flexible；The guide member is to be fixed at the frame
The guide rod of inside.
Wherein, the guide rod may be, for example, aluminium alloy guide rod.
Wherein, the frame may be, for example, carbon fiber frame.
Preferably, the locking assembly further include: the screw rod that is arranged in the tight lock part and for driving the spiral shell
The motor of bar rotation.The screw rod is for fixing battery in the battery compartment, and the motor is for adjusting stretching for the screw rod
Contracting movement, when the screw rod elongation when, the screw rod is capable of fixing the battery, when the screw rod shorten when, the screw rod
The battery is loosened, convenient for the battery compartment is discharged in the battery, improves the replacement efficiency of battery.
Preferably, the tight lock part is the convex block of a square structure.For the motor and institute to be arranged in the convex block
Screw rod is stated, while the convex block is also used to lock the battery, the battery is avoided to be easy to fall off during installation.
Preferably, the tight lock part is the convex block of a cylindrical structure.
Preferably, the pushing member includes a cylinder and the gas bar being arranged on the cylinder, and the gas bar is another
End is fixedly connected with the tight lock part.The cylinder is used to adjust the stretching motion of the gas bar, and the gas bar and the lock
Tight portion is fixedly connected, when the effect that the gas bar can make the battery be fixedly clamped when extending to the battery, when
When the gas bar is shunk to the cylinder direction, the battery end loses resistance, in the elastic shape of the elastic parts
Under change, the battery can be made quickly to pop up a part of region, the region be convenient for being arranged in the grabbing device of base station by its
It takes out, improves the efficiency for taking battery.
Preferably, the elastic parts includes a spring and the push plate for being located at the spring at front end, the push plate and electricity
One end structure of pond is adapted.The spring is for pushing the battery to be discharged in the battery compartment, the push plate and the battery
One end structure is adapted, and can make battery uniform force in by pushing course, is released better effect, is taken battery speed
Fastly.
Preferably, the frame is the square frame for being provided with multiple support rods.The frame is for disposing and to institute
Battery limiting is stated, the battery is avoided to occur positional shift, while the rod-shaped frame of the multiple support can make battery in work
Heat dissipation effect is good when making, and reduces to the damage inside battery and unmanned plane, and the square frame material is few, reduces nobody
The weight of machine, improves flight efficiency.
Preferably, opposite on the inside of the frame to be equipped with conducting block, the conducting block is corresponding with the power transmission section on battery, institute
Conducting block is stated to match with the power transmission section structure.It is described to be used to the electricity on the battery being transported to unmanned plane to conducting block
On, flight is controlled by the circuit inside unmanned plane.
According to an aspect of the present invention, a kind of unmanned machine battery is designed, setting battery, institute are adapted in the battery compartment
Battery is stated to include: battery main body, the shell being arranged in outside the battery main body and be arranged in the more of described battery main body one end
A power transmission section, the power transmission section match with the conducting block.The shell avoids the electricity for protecting the battery main body
Tank main body is excessive in unmanned replacement battery number and causes to wear, while structure is adapted in the shell and the battery compartment,
So that the battery compartment and the shell limit effect are more preferably, and the power transmission section matches to improve and contacts with the conducting block
Effect, so that the well conducting of battery, avoids unmanned plane from occurring powering off and the unmanned plane being caused to fall.
Preferably, the shell two sides be additionally provided with the guide rod be adapted guide groove and with the tight lock part
Adaptable groove, the groove is interior to be equipped with the threaded hole to match with the screw rod, and the guide groove and the groove are side
Shape structure.The guide groove is used to limit the installation path of the battery, avoids shifting when replacing battery and leading to institute
Battery Card is stated in the battery compartment, reduces the efficiency of replacement battery.
A kind of locking method of unmanned machine battery, comprising steps of
S1, battery guide slot and battery compartment guide rod are aligned；
S2, the battery is fully mounted in the battery compartment；
Pass through locking assembly telescopic locking in groove on S3, the battery.
Bring of the present invention is arranged in supporting and space the utility model has the advantages that by the frame providing support space in battery compartment
Elastic parts be convenient for improving battery ejection into the efficiency for taking out battery, and electricity can be made in the guide member of frame two sides
Pond will not shift in replacement, and locking assembly avoids it from taking off on unmanned plane for locking mounted battery
It falls, the tight lock part in locking assembly is locked by the way that the pushing member in face behind is arranged to control tight lock part, when tight lock part pine
When opening, battery is pushed into outside battery compartment under the elastic deformation of elastic parts, greatly improves the replacement efficiency of battery.This
Invention can greatly improve the replacement efficiency of battery, and structure is simple, and use scope is wide.
Detailed description of the invention
Fig. 1 is unmanned plane battery box structure schematic diagram of the present invention；
Fig. 2 is unmanned plane battery structure schematic diagram of the present invention；
Fig. 3 is pushing member structural schematic diagram of the present invention；
Fig. 4 is battery compartment locking method flow chart of the present invention.
Wherein: 1, frame；2, elastic parts；3, guide member；4, locking assembly；5, tight lock part；6, pushing member；7, it leads
To bar；8, screw rod；9, motor；10, convex block；11, cylinder；12, gas bar；13, spring；14, push plate；15, support rod；16, conductive
Block；17, square structure；18, battery main body；19, shell；20, power transmission section；21, guide groove；22, groove.
Specific embodiment
The preferred embodiment of the present invention is described below, those of ordinary skill in the art will be according to described below with this
The relevant technologies in field are realized, and can be more clearly understood that innovation and bring benefit of the invention.
As shown in Figure 1, providing a kind of battery compartment of unmanned plane, comprising: frame 1 is arranged in 1 inner opposite end of frame
On elastic parts 2, be oppositely arranged on the guide member 3 of two sides in the frame 1 and 1 exit of frame be set
At least one locking assembly 4；The locking assembly 4 includes: at least one for being fixed at 1 end of frame inside both ends
Tight lock part 5 and pushing member 6 for pushing the tight lock part 5 flexible；The guide member 3 is to be fixed at the frame
The guide rod 7 of 1 inside of frame.Supporting and space, the bullet being arranged in supporting and space are provided by the frame 1 in battery compartment
Property component 2 be convenient for improving battery ejection into the efficiency for taking out battery, and 3 energy of the guide member in 1 two sides of frame
So that battery will not shift in replacement, the locking assembly 4 for mounted battery to be locked, avoid its
It falls off on unmanned plane, the tight lock part 5 in the locking assembly 4 is controlled by the way that the pushing member 6 in face behind is arranged
Tight lock part 5 is locked, and when the tight lock part 5 unclamps, battery is pushed into battery compartment under the elastic deformation of the elastic parts 2
Outside, the replacement efficiency of battery is greatly improved.The guide rod 7 is used to be oriented to and support the effect of battery, when to electricity
When pond is replaced, the guide rod 7 can preferably be skidded off battery, simultaneously as the guide rod 7 is is oppositely arranged on
It states in frame 1, the guide rod 7 is smoothly slided on the battery, avoids the battery in the battery compartment
It shifts when mobile, more preferably, battery altering effect is higher for guide effect.
Further, the locking assembly 4 is the first locking assembly 4 and second being oppositely arranged in the frame 1
Locking assembly 4, the effect that first locking assembly 4, second locking assembly 4 can lock battery and fix,
When first locking assembly 4 is mobile to the battery direction simultaneously with second locking assembly 4, the first locking group
Part 4, second locking assembly 4 can also play the effect of clamping to the battery, increase the stationarity of the battery.
In embodiments of the present invention, the locking assembly 4 further include: the screw rod 8 in the tight lock part 5 is set and is used
In the motor 9 for driving the screw rod 8 to rotate.For fixing battery in the battery compartment, the motor 9 is used for the screw rod 8
The stretching motion for adjusting the screw rod 8, when the screw rod 8 is in elongation, the screw rod 8 is capable of fixing the battery, when the spiral shell
For bar 8 when shortening, the screw rod 8 loosens the battery, convenient for the battery compartment is discharged in the battery, improves battery more
Change efficiency.
In embodiments of the present invention, the tight lock part 5 is the convex block 10 of a square structure 17.For setting in the convex block 10
The motor 9 and the screw rod 8 are set, while the convex block 10 is also used to lock the battery, the battery is avoided to install
When be easy to fall off.
Further, the tight lock part 5 further includes cylindrical bump 10, convenient for described in setting in the cylindrical bump 10
Motor 9 and the screw rod 8, so that the fixed effect in the Telescopic Fixed battery of the screw rod 8 is good.
In embodiments of the present invention, as shown in figure 3, the pushing member 6 includes a cylinder 11 and is arranged in the gas
Gas bar 12 on cylinder 11,12 other end of gas bar are fixedly connected with the tight lock part 5.The cylinder 11 is for adjusting the gas
The stretching motion of bar 12, and the gas bar 12 is fixedly connected with the tight lock part 5, when the gas bar 12 is extended to the battery
When the battery can be made to be fixedly clamped effect, when the gas bar 12 is shunk to 11 direction of cylinder, the electricity
Pond end loses resistance, under the elastic deformation of the elastic parts 2, the battery can be made quickly to pop up a part
Region, the region are convenient for the grabbing device that base station is arranged in be drawn off, improve the efficiency for taking battery.
In embodiments of the present invention, the elastic parts 2 including a spring 13 and is located at pushing away for 13 front end of spring
Plate 14, the push plate 14 are adapted with one end structure of battery.The spring 13 is for pushing the battery that the battery compartment is discharged
Interior, the push plate 14 is adapted with one end structure of battery, can be made battery uniform force in by pushing course, be pushed away
Better effect out takes battery speed fast；The spring 13 is arranged on the middle position of the battery compartment side, so that the spring
13 are uniformly distributed when endurance acts on, and increase the service life of the spring 13.
Further, the push plate 14 is square structure 17, and the push plate 14 is equipped with leads to what conducting block 16 was adapted
Hole, the through-hole are used to provide a clearance position for the conducting block 16, avoid the battery from blocking when taking out, reduce battery
Replacement efficiency.
In embodiments of the present invention, the frame 1 is the square frame 1 for being provided with multiple support rods 15.The frame 1 is used
In placement and to the battery limiting, avoid the battery that positional shift, while the frame of 15 shape of the multiple support rod occurs
Frame 1 can make battery, and heat dissipation effect is good at work, reduces to the damage inside battery and unmanned plane, the square frame
1 material is few, reduces the weight of unmanned plane, improves flight efficiency.
In embodiments of the present invention, 1 inside of the frame is opposite is equipped with conducting block 16, the conducting block 16 on battery
Power transmission section 20 is corresponding, and the conducting block 16 matches with 20 structure of power transmission section.It is described to conducting block 16 for will be described
Electricity on battery is transported on unmanned plane, and flight is controlled by the circuit inside unmanned plane.
According to an aspect of the present invention, a kind of unmanned machine battery is designed, as shown in Figure 2.It is adapted in the battery compartment
Battery is set, and the battery includes: battery main body 18, the shell 19 being arranged in outside the battery main body 18 and is arranged described
Multiple power transmission sections 20 of 18 one end of battery main body, the power transmission section 20 match with the conducting block 16.The shell 19 is used for
The battery main body 18 is protected, avoids the battery main body 18 excessive in unmanned replacement battery number and causes to wear, while institute
Structure in shell 19 and the battery compartment is stated to be adapted, so that the battery compartment and 19 limit effect of shell are more preferably, and institute
It states power transmission section 20 and the conducting block 16 matches and improves contact effect, so that the well conducting of battery, avoids unmanned plane from going out
It now powers off and the unmanned plane is caused to fall.
In embodiments of the present invention, 19 two sides of shell be additionally provided with the guide rod 7 be adapted guide groove 21, with
And the groove 22 being adapted with the tight lock part 5, the groove 22 is interior equipped with the threaded hole to match with the screw rod 8, described
Guide groove 21 and the groove 22 are square structure 17.The guide groove 21 is used to limit the installation path of the battery, avoids
It shifts when replacing battery and causes the Battery Card in the battery compartment, reduce the efficiency of replacement battery.
The embodiment of the present invention also provides a kind of unmanned plane, which may include unmanned plane described in previous embodiment
The specific structure and function of battery compartment and battery, the unmanned plane battery compartment and battery can refer to the part or complete of previous embodiment
Portion's content, which is not described herein again.
As shown in figure 4, the embodiment of the present invention also designs a kind of locking method of unmanned machine battery, comprising steps of
S1, battery guide slot 21 and battery compartment guide rod 7 are aligned；
S2, the battery is fully mounted in the battery compartment；The guide groove 21 of the battery and 7 knot of guide rod
Structure is adapted, and the battery is quickly mounted in the battery compartment, improves the efficiency of battery installation, the battery
It replaces efficiency in the battery compartment to improve, use scope is wide.
Pass through 4 telescopic locking of locking assembly in groove 22 on S3, the battery.The groove 22 and the locking assembly
4 match, so that the battery is able to achieve quick-replaceable and the battery is locked on battery compartment, the battery are avoided to move
It is fallen off when dynamic.
The above content is a further detailed description of the present invention in conjunction with specific preferred embodiments, and it cannot be said that
A specific embodiment of the invention is only limited to these instructions.General technical staff of the technical field of the invention is come
It says, without departing from the inventive concept of the premise, a number of simple deductions or replacements can also be made, all shall be regarded as belonging to this hair
Bright protection scope.
Claims (10)
1. a kind of unmanned plane battery compartment characterized by comprising frame, elastic group be arranged on the frame inner opposite end
Part, at least one the locking group for being oppositely arranged on the guide member of two sides in the frame and being arranged at the frame exhaust openings
Part；
The locking assembly includes: to be fixed at least one tight lock part at frame end inside both ends and for pushing away
Move the flexible pushing member of the tight lock part；
The guide member is the guide rod being fixed on the inside of the frame.
2. a kind of unmanned plane battery compartment according to claim 1, which is characterized in that the guide rod is aluminium alloy guiding
Bar.
3. a kind of unmanned plane battery compartment according to claim 1 to 2, which is characterized in that the frame is carbon fiber frame
Frame.
4. a kind of unmanned plane battery compartment according to claim 1 to 3, which is characterized in that the locking assembly is also wrapped
It includes: the screw rod being arranged in the tight lock part and the motor for driving the screw rod rotation.
5. a kind of unmanned plane battery compartment according to claim 1 to 4, which is characterized in that the tight lock part is one rectangular
The convex block of structure.
6. -5 any a kind of unmanned plane battery compartment according to claim 1, which is characterized in that the tight lock part is a cylinder
The convex block of shape structure.
7. -6 any a kind of unmanned plane battery compartment according to claim 1, which is characterized in that the pushing member includes one
Cylinder and the gas bar being arranged on the cylinder, the gas bar other end are fixedly connected with the tight lock part.
8. -7 any a kind of unmanned plane battery compartment according to claim 1, which is characterized in that the elastic parts includes one
Spring and the push plate for being located at the spring at front end, the push plate and one end structure of battery are adapted.
9. -8 any a kind of unmanned plane battery compartment according to claim 1, which is characterized in that the frame is more to be provided with
The square frame of a support rod.
10. -9 any a kind of unmanned plane battery compartment according to claim 1, which is characterized in that opposite on the inside of the frame
Equipped with conducting block, the conducting block is corresponding with the power transmission section on battery, and the conducting block matches with the power transmission section structure.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810865067.XA CN109148761A (en) | 2018-08-01 | 2018-08-01 | A kind of unmanned plane battery compartment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810865067.XA CN109148761A (en) | 2018-08-01 | 2018-08-01 | A kind of unmanned plane battery compartment |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109148761A true CN109148761A (en) | 2019-01-04 |
Family
ID=64798694
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810865067.XA Pending CN109148761A (en) | 2018-08-01 | 2018-08-01 | A kind of unmanned plane battery compartment |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109148761A (en) |
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| PB01 | Publication | ||
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Application publication date: 20190104 |