CN209126979U - Unmanned plane battery fixing structure and unmanned plane - Google Patents
Unmanned plane battery fixing structure and unmanned plane Download PDFInfo
- Publication number
- CN209126979U CN209126979U CN201821555034.7U CN201821555034U CN209126979U CN 209126979 U CN209126979 U CN 209126979U CN 201821555034 U CN201821555034 U CN 201821555034U CN 209126979 U CN209126979 U CN 209126979U
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- unmanned plane
- hole
- support base
- battery
- installation
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- 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
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
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- Charge And Discharge Circuits For Batteries Or The Like (AREA)
Abstract
A kind of unmanned plane battery fixing structure and unmanned plane, it is related to air vehicle technique field, the unmanned plane battery fixing structure includes unmanned plane main body, and the unmanned plane main body is a frame structure, and the frame structure is formed with one for limiting the installation space of fixed unmanned machine battery；The unmanned plane includes above-mentioned unmanned plane battery fixing structure and the unmanned machine battery, and the unmanned plane battery limiting is fixed in the installation space.By using this unmanned plane battery fixing structure, can making the installation of unmanned plane battery, operation is very easy, also very convenient when charging the battery or replacing battery, additionally it is possible to reduce the weight of unmanned plane, and occupy little space；This unmanned plane is simple and compact for structure, light-weight, facilitates the operation of unmanned plane itself.
Description
Technical field
The utility model relates to air vehicle technique fields, in particular to a kind of unmanned plane battery fixing structure and nothing
It is man-machine.
Background technique
Development recently as unmanned air vehicle technique is universal, and unmanned plane industry development is extremely swift and violent, compared to using the dynamic side of oil
The unmanned plane of formula, electronic unmanned plane have many advantages, such as that compact-sized, weight is more light, noise is small.
Electronic unmanned plane mainly uses battery to have as major impetus about the connection of unmanned machine battery and unmanned plane
Battery case is set on unmanned plane, then battery is installed in the battery case, this connection type is in battery to be replaced or to electricity
When pond is charged, operation is very inconvenient, and the weight that battery case also increases unmanned plane to a certain extent is arranged；Unmanned plane weight
Measure overweight, be unfavorable for its operation, if unmanned plane, which is accidentally fallen, bumps against some objects or personnel, will cause property and
The damage of personnel, the dense population areas especially in big and medium-sized cities, unmanned plane operation will be limited.
Utility model content
The purpose of this utility model is to provide a kind of unmanned plane battery fixing structure and unmanned planes, can make unmanned plane
Operation is very easy for the installation of battery.
The embodiments of the present invention are achieved in that
The one side of the utility model embodiment provides a kind of unmanned plane battery fixing structure comprising unmanned plane main body,
The unmanned plane main body is a frame structure, and it is empty for limiting the installation of fixed unmanned machine battery that the frame structure is formed with one
Between.
Optionally, in the utility model preferred embodiment, the unmanned plane main body includes bottom plate, from the bottom plate to
Multiple support rods of upper extension are respectively connected with multiple bars, the bottom plate, the multiple support between adjacent two support rod
Bar and the multiple bar are enclosed the frame structure jointly.
Optionally, in the utility model preferred embodiment, a barrier is connected between two bars being oppositely arranged
The frame structure is separated into cavity structure that one is used to install medicine-chest and described is used to limit fixed nothing by plate, the baffles
The installation space of man-machine battery.
It optionally, further include support base in the utility model preferred embodiment, the support base includes support base master
Body and pedestal for placing unmanned machine battery, the pedestal are connected to the bottom end of the support base main body, the support seat tool
There is a through-hole, it is in institute on two bars being oppositely arranged that the support base, which is socketed on by the through-hole close to the bottom plate,
It states pedestal and forms one for placing the platform of the unmanned machine battery.
Optionally, in the utility model preferred embodiment, the support base main body and the pedestal are integrally formed
Structure.
Optionally, in the utility model preferred embodiment, the quantity of the support base is the idol more than or equal to 4
Number is equally divided into two groups, and it is in be oppositely arranged that two groups of support bases pass through the through-hole to be socketed on close to the bottom plate respectively
On two bars.
Optionally, in the utility model preferred embodiment, the first side of the support base main body is provided with for spiral shell
The first installation through-hole that fitting passes through is passed through first installation through-hole and is spirally connected and is fixed on the bar by spiro connecting piece.
Optionally, in the utility model preferred embodiment, the through-hole is opened in the second of the support base main body
On side, at least two is provided on the through-hole edge of the second side of the support base main body and is passed through for spiro connecting piece
The second installation through-hole, the baffles are provided with the third installation through-hole that at least four is passed through for spiro connecting piece, and the baffles are logical
Spiro connecting piece is crossed to be spirally connected across the third installation through-hole and second installation through-hole of the baffles with the support base
It is fixed.
Optionally, in the utility model preferred embodiment, the bottom plate includes support plate, the support plate with it is described
Support base is fixedly connected, and the bottom of the pedestal is provided with blind hole, and the support plate is provided with the 4th installation through-hole of at least four,
The support plate is bolted in the described blind of the support base by the 4th installation through-hole that spiro connecting piece passes through the support plate
In hole.
The another aspect of the utility model embodiment also provides a kind of unmanned plane comprising above-mentioned unmanned machine battery is solid
Determine structure and the unmanned machine battery, the unmanned plane battery limiting is fixed in the installation space.
The beneficial effect of the utility model embodiment includes:
This unmanned plane battery fixing structure includes unmanned plane main body, which is a frame structure, the frame knot
One is configured to for limiting the installation space of fixed unmanned machine battery；It, can be with by using this unmanned plane battery fixing structure
When to charge the battery or replace battery, operation is very easy, due to the sheet that this unmanned plane battery fixing structure is unmanned plane
Body structure does not cause the increase of unmanned plane additional weight, compares and battery case is arranged, reduce nobody to a certain extent
The weight of machine, and occupy little space.
This unmanned plane includes above-mentioned unmanned plane battery fixing structure and unmanned machine battery, and unmanned plane battery limiting is fixed on
In above-mentioned installation space；This unmanned plane is simple and compact for structure, light-weight, facilitates the operation of unmanned plane itself.
Detailed description of the invention
It, below will be to use required in embodiment in order to illustrate more clearly of the technical solution of the utility model embodiment
Attached drawing be briefly described, it should be understood that the following drawings illustrates only some embodiments of the utility model, therefore should not be by
Regard the restriction to range as, for those of ordinary skill in the art, without creative efforts, may be used also
To obtain other relevant attached drawings according to these attached drawings.
Fig. 1 is the unmanned plane battery fixing structure schematic diagram that an embodiment of the present invention provides；
Fig. 2 is the top view of unmanned plane battery fixing structure in Fig. 1；
Fig. 3 is the structural schematic diagram of support base in Fig. 1；
Fig. 4 is the bottom view of support base in Fig. 3；
Fig. 5 is the structural schematic diagram of baffles in Fig. 1；
Fig. 6 is the structural schematic diagram of support plate in Fig. 1；
Fig. 7 is the structural schematic diagram for the unmanned plane that an embodiment of the present invention provides.
Icon: 100- unmanned plane battery fixing structure；1- unmanned plane main body；2- support rod；3- bar；The first bar of 31-；
The second bar of 32-；4- baffles；41- third installation through-hole；5- support base；The first support base of 5a-；The second support base of 5b-；5c-
Third support base；5d- four-supporting；51- support base main body；52- pedestal；52a- first base；52b- second base；52c-
Third pedestal；The 4th pedestal of 52d-；53- through-hole；53a- first through hole；The second through-hole of 53b-；53c- third through-hole；53d- the 4th
Through-hole；The first installation through-hole of 54-；The second installation through-hole of 55-；56- blind hole；57- entire body groove；6- support plate；61- the 4th is installed
Through-hole；7- installation space；200- unmanned plane；The unmanned machine battery of 201-；The unmanned machine cap of 202-.
Specific embodiment
It is practical new below in conjunction with this to keep the objectives, technical solutions, and advantages of the embodiments of the present invention clearer
Attached drawing in type embodiment, the technical scheme in the utility model embodiment is clearly and completely described, it is clear that is retouched
The embodiment stated is the utility model a part of the embodiment, instead of all the embodiments.Usually here in attached drawing description and
The component of the utility model embodiment shown can be arranged and be designed with a variety of different configurations.
Therefore, requirement is not intended to limit to the detailed description of the embodiments of the present invention provided in the accompanying drawings below
The scope of the utility model of protection, but it is merely representative of the selected embodiment of the utility model.Based in the utility model
Embodiment, every other embodiment obtained by those of ordinary skill in the art without making creative efforts, all
Belong to the range of the utility model protection.
It should also be noted that similar label and letter indicate similar terms in following attached drawing, therefore, once a certain Xiang Yi
It is defined in a attached drawing, does not then need that it is further defined and explained in subsequent attached drawing.
It is in the description of the present invention, it should be noted that term " center ", "upper", "lower", "left", "right", " perpendicular
Directly ", the orientation or positional relationship of the instructions such as "horizontal", "inner", "outside" be based on the orientation or positional relationship shown in the drawings, or
The utility model product using when the orientation or positional relationship usually put, be merely for convenience of description the utility model and letter
Change description, rather than the device or element of indication or suggestion meaning must have a particular orientation, with specific orientation construct and
Operation, therefore should not be understood as limiting the present invention.In addition, term " first ", " second ", " third " etc. are only used for area
Divide description, is not understood to indicate or imply relative importance.
In addition, the terms such as term "horizontal", "vertical" are not offered as requiring component abswolute level or pendency, but can be slightly
Low dip.It is not to indicate that the structure has been had to if "horizontal" only refers to that its direction is more horizontal with respect to for "vertical"
It is complete horizontal, but can be slightly tilted.
In the description of the present invention, it should also be noted that, unless otherwise clearly defined and limited, term " is set
Set ", " installation ", " connected ", " connection " shall be understood in a broad sense, for example, it may be being fixedly connected, may be a detachable connection,
Or it is integrally connected；It can be mechanical connection, be also possible to be electrically connected；It can be directly connected, intermediary can also be passed through
It is indirectly connected, can be the connection inside two elements.For the ordinary skill in the art, it can be managed with concrete condition
Solve the concrete meaning of above-mentioned term in the present invention.
Embodiment
Fig. 1 is please referred to, the present embodiment provides a kind of unmanned plane battery fixing structures 100 comprising unmanned plane main body 1, nothing
Man-machine main body 1 is a frame structure, which is formed with an installation space 7 for being used to limit fixed unmanned machine battery 201,
It can be reduced weight of unmanned plane 200 itself using frame structure.
Wherein, unmanned plane main body 1 includes bottom plate, the multiple support rods 2 upwardly extended from the bottom plate, adjacent two above-mentioned support
Multiple bars 3 are respectively connected between bar 2, above-mentioned bottom plate, multiple support rods 2 and multiple bars 3 are enclosed above-mentioned frame jointly
Frame structure.
Optionally, in a baffles 4 are connected between two bars 3 being oppositely arranged, baffles 4 divide said frame structure
One is divided into for installing the cavity structure of medicine-chest and the installation space 7 for limiting fixed unmanned machine battery 201.
As shown in Figure 1, the first bar 31 and the second bar 32 are in be oppositely arranged, between the first bar 31 and the second bar 32
It is connected with baffles 4.
It further, further include support base 5 incorporated by reference to reference Fig. 2 and Fig. 3, support base 5 includes support base main body 51 and uses
In the pedestal 52 for placing unmanned machine battery 201, pedestal 52 is connected to the bottom end of support base main body 51, and support base 5 has a through-hole
53, it is on two bars 3 being oppositely arranged that support base 5, which is socketed on by through-hole 53 close to above-mentioned bottom plate, and pedestal 52 forms one and is used for
Place the platform of unmanned machine battery 201.
It should be noted that support base main body 51 and pedestal 52 are an integral molding structure.
Wherein, the quantity of support base 5 is the even number more than or equal to 4, is equally divided into two groups, which distinguishes
Being socketed on by through-hole 53 close to above-mentioned bottom plate is on two bars 3 being oppositely arranged.
As depicted in figs. 1 and 2, the quantity of support base 5 is 4, is the first support base 5a, the second support base 5b, the respectively
There is first through hole 53a, the second support base 5b to have the second through-hole by three support base 5c, four-supporting 5d, the first support base 5a
There is third through-hole 53c, four-supporting 5d to have fourth hole 53d, the first support base 5a and the by 53b, third support base 5c
Two support base 5b pass through first through hole 53a respectively and the second through-hole 53b is socketed on the first bar 31, third support base 5c and
Four-supporting 5d passes through third through-hole 53c and fourth hole 53d respectively and is socketed on the second bar 32.
First support base 5a includes first base 52a, and the second support base 5b includes second base 52b, third support base 5c
It include the 4th pedestal 52d, first base 52a, second base 52b, third pedestal including third pedestal 52c, four-supporting 5d
52c, the 4th pedestal 52d form one for placing the platform of unmanned machine battery 201.
Optionally, as shown in figure 3,5 bottom of support base is recessed with an entire body groove 57, entire body groove 57 helps to increase peace
Convenience during dress.
Optionally, the first side of support base main body 51 is provided with the first installation through-hole 54 passed through for spiro connecting piece, passes through
Spiro connecting piece passes through the first installation through-hole 54 and is spirally connected and is fixed on bar 3.
Optionally, through-hole 53 is opened in the second side of support base main body 51, the second side of support base main body 51
The second installation through-hole 55 that at least two is passed through for spiro connecting piece is provided on 53 edge of through-hole, baffles 4 are provided at least four confession
The third installation through-hole 41 that spiro connecting piece passes through, baffles 4 pass through the third installation through-hole 41 and second of baffles 4 by spiro connecting piece
Installation through-hole 55 and be spirally connected fixation with support base 5.
It should be noted that baffles 4 are fixedly connected with the second support base 5b and four-supporting 5d.
Optionally, as shown in figure 5, baffles 4 are hollow design, unmanned plane 200 can both be reduced using hollow design
Weight, and facilitate the heat dissipation of unmanned machine battery 201.
Optionally, above-mentioned bottom plate includes support plate 6, and support plate 6 is fixedly connected with support base 5, the bottom setting of pedestal 52
There is blind hole 56, as shown in figure 4, support plate 6 is provided with the 4th installation through-hole 61 of at least four, as shown in fig. 6, support plate 6 passes through spiral shell
The 4th installation through-hole 61 that fitting passes through support plate 6 is bolted in the blind hole 56 of support base 5.
It should be noted that carbon fiber board can be used in support plate 6, carbon fiber board has tensile strength height, shock resistance, anti-impact
The good performance such as hitting property.
Fig. 7 is please referred to, the present embodiment also provides a kind of unmanned plane 200 comprising above-mentioned unmanned plane battery fixing structure
100 and unmanned machine battery 201, the unmanned limit of machine battery 201 is fixed in installation space 7.
Optionally, unmanned plane 200 further includes unmanned machine cap 202, when unmanned machine cap 202 is buckling state, unmanned plane
The upper contact of the bottom of top cover 202 and unmanned machine battery 201 can play fixed function to unmanned machine battery 201.
It should be noted that when to charge the battery or replace battery unmanned machine cap 202 only need to be opened, by nobody
Machine battery 201 takes out.
In conclusion this unmanned plane battery fixing structure 100 includes unmanned plane main body 1, which is a frame
Structure, the frame structure are formed with one for limiting the installation space 7 of fixed unmanned machine battery 201, can make unmanned plane battery
201 limits are fixed in installation space 7, by using this unmanned plane battery fixing structure 100, make the peace of unmanned machine battery 201
Operation is very easy for dress, also very convenient when charging the battery or replacing battery, due to this unmanned plane battery fixing structure 100
For this body structure of unmanned plane 200, the increase of 200 additional weight of unmanned plane is not caused, compares and battery case is set, one
Determine the weight for reducing unmanned plane 200 in degree, and occupies little space.
This unmanned plane 200 includes above-mentioned unmanned plane battery fixing structure 100 and unmanned machine battery 201；This unmanned plane 200
With beneficial effect identical with the unmanned plane battery fixing structure 100 in previous embodiment；Due to unmanned machine battery fixed knot
The structure and beneficial effect of structure 100 are described in detail in the above-described embodiments, and details are not described herein, in addition, this nothing
Man-machine 200 also have the characteristics that operation that is simple and compact for structure, light-weight, and then facilitating itself.
The above descriptions are merely preferred embodiments of the present invention, is not intended to limit the utility model, for this
For the technical staff in field, various modifications and changes may be made to the present invention.It is all in the spirit and principles of the utility model
Within, any modification, equivalent replacement, improvement and so on should be included within the scope of protection of this utility model.
Claims (8)
1. a kind of unmanned plane battery fixing structure, which is characterized in that including unmanned plane main body, the unmanned plane main body is a frame
Structure, the frame structure are formed with one for limiting the installation space of fixed unmanned machine battery；The unmanned plane main body includes
Bottom plate, the multiple support rods upwardly extended from the bottom plate are respectively connected with multiple bars between adjacent two support rod, described
Bottom plate, the multiple support rod and the multiple bar are enclosed the frame structure jointly；It further include support base, it is described
Support base includes support base main body and the pedestal for placing unmanned machine battery, and the pedestal is connected to the support base main body
Bottom end, the support base have a through-hole, and it is in be oppositely arranged that the support base, which is socketed on by the through-hole close to the bottom plate,
Two bars on, the pedestal forms one for placing the platform of the unmanned machine battery.
2. unmanned plane battery fixing structure according to claim 1, which is characterized in that between two bars being oppositely arranged
A baffles are connected with, the frame structure is separated into the cavity structure and the use that one is used to install medicine-chest by the baffles
In the installation space of the fixed unmanned machine battery of limit.
3. unmanned plane battery fixing structure according to claim 2, which is characterized in that the support base main body and the bottom
Seat is an integral molding structure.
4. unmanned plane battery fixing structure according to claim 3, which is characterized in that the quantity of the support base be greater than
Or the even number equal to 4, it is equally divided into two groups, two groups of support bases pass through the through-hole respectively and are socketed on is in close to the bottom plate
On two be oppositely arranged the bar.
5. unmanned plane battery fixing structure according to claim 4, which is characterized in that the first side of the support base main body
Face is provided with the first installation through-hole passed through for spiro connecting piece, passes through first installation through-hole by spiro connecting piece and is spirally connected and is fixed on
On the bar.
6. unmanned plane battery fixing structure according to claim 4, which is characterized in that the through-hole is opened in the support
In the second side of seat main body, at least two is provided on the through-hole edge of the second side of the support base main body
For the second installation through-hole that spiro connecting piece passes through, the baffles are provided with the third installation through-hole that at least four is passed through for spiro connecting piece,
The baffles pass through the third installation through-hole and second installation through-hole and the institute of the baffles by spiro connecting piece
Support base is stated to be spirally connected fixation.
7. unmanned plane battery fixing structure according to claim 4, which is characterized in that the bottom plate includes support plate, institute
It states support plate to be fixedly connected with the support base, the bottom of the pedestal is provided with blind hole, and the support plate is provided at least four
4th installation through-hole, the support plate are bolted in the branch by the 4th installation through-hole that spiro connecting piece passes through the support plate
In the blind hole for supportting seat.
8. a kind of unmanned plane, which is characterized in that including unmanned plane battery fixing structure described in any one of claim 1-7
With the unmanned machine battery, the unmanned plane battery limiting is fixed in the installation space.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821555034.7U CN209126979U (en) | 2018-09-21 | 2018-09-21 | Unmanned plane battery fixing structure and unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821555034.7U CN209126979U (en) | 2018-09-21 | 2018-09-21 | Unmanned plane battery fixing structure and unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209126979U true CN209126979U (en) | 2019-07-19 |
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ID=67228547
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821555034.7U Active CN209126979U (en) | 2018-09-21 | 2018-09-21 | Unmanned plane battery fixing structure and unmanned plane |
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| Country | Link |
|---|---|
| CN (1) | CN209126979U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2022067939A1 (en) * | 2020-09-30 | 2022-04-07 | 拓攻（南京）机器人有限公司 | Agricultural unmanned aerial vehicle |
-
2018
- 2018-09-21 CN CN201821555034.7U patent/CN209126979U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2022067939A1 (en) * | 2020-09-30 | 2022-04-07 | 拓攻（南京）机器人有限公司 | Agricultural unmanned aerial vehicle |
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