CN208835131U - A kind of unmanned plane structure of battery corer being readily disassembled - Google Patents
A kind of unmanned plane structure of battery corer being readily disassembled Download PDFInfo
- Publication number
- CN208835131U CN208835131U CN201821435835.XU CN201821435835U CN208835131U CN 208835131 U CN208835131 U CN 208835131U CN 201821435835 U CN201821435835 U CN 201821435835U CN 208835131 U CN208835131 U CN 208835131U
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- CN
- China
- Prior art keywords
- unmanned plane
- pair
- gliding mass
- shank
- readily disassembled
- 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.)
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Classifications
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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
- 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
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- Battery Mounting, Suspending (AREA)
Abstract
The utility model embodiment discloses a kind of unmanned plane structure of battery corer being readily disassembled, sliding is provided with gliding mass, a pair of of shank in the pedestal of the battery cover, skewed slot is provided on the pair of shank, the gliding mass two sides are respectively arranged with the traveller being slidably connected with the skewed slot of the pair of shank, and the pedestal two sides are slidably stretched out in the pair of shank end.Using the utility model, structure is simple, and installation is firm, convenient for being unmanned plane Fast Installation battery, has many advantages, such as convenient to use.
Description
Technical field
The utility model relates to unmanned plane fields more particularly to one kind to be readily disassembled, the simple unmanned plane battery cover of structure
Structure.
Background technique
The cruising ability of unmanned plane is one of its key technology, and therefore, power battery is most important for unmanned plane.
And by the limited mass that unmanned plane can carry, it can not be often equipped with the battery of enough capacity, it is in order to solve this problem, existing
In technology general way be by the way of replacing battery, and replace the structure of battery often exist be difficult to reach and nobody
Machine forms stable connection relationship, or structure is complicated, is easy to make drone center of unmanned aerial vehicle change, increase unmanned plane weight etc. to lack
It falls into.
Utility model content
The technical problem to be solved by the embodiment of the utility model is, providing a kind of unmanned plane battery cover being readily disassembled
Structure.The replacement operation of unmanned machine battery can be simplified, and stable connection structure can be formed with unmanned plane.
In order to solve the above-mentioned technical problem, the utility model embodiment provides a kind of unmanned plane battery cover being readily disassembled
Structure, the interior sliding of the pedestal of the battery cover is provided with gliding mass, a pair of of shank, is provided with skewed slot on the pair of shank, described
Gliding mass two sides are respectively arranged with the traveller being slidably connected with the skewed slot of the pair of shank, and the pair of shank end is slidably stretched
The pedestal two sides out.
Further, the spring for resetting the gliding mass is provided in the pedestal.
Further, support is provided in the pedestal, the spring one end is set in the support, and the other end is made
At the top of the gliding mass.,
Further, the pedestal corresponds to the gliding mass two sides and is provided with a pair of longitudinal card edge, and the gliding mass sliding is set
The pair of longitudinal card is placed between.
Further, the lateral card edge that there is the pedestal sliding the pair of shank is arranged.
Further, the glide direction of the pair of shank is vertical with the glide direction of the gliding mass.
Further, the glide direction of the skewed slot and the gliding mass is in 45 degree of angles.
Further, the gliding mass surface is provided with unlatching and dials body, and the box body corresponds to the unlatching group body setting and slides
Dynamic window.
Implement the utility model embodiment, have the following beneficial effects: that the utility model structure is simple, installation is firm, just
In for unmanned plane Fast Installation battery, have many advantages, such as convenient to use.
Detailed description of the invention
Fig. 1 is the structural schematic diagram that the utility model is applied on unmanned plane；
Fig. 2 is the decomposition texture schematic diagram of the utility model；
Fig. 3 is the schematic diagram of internal structure of the utility model；
Fig. 4 is the utility model internal breakup structural schematic diagram.
Specific embodiment
It is practical new to this below in conjunction with attached drawing to keep the purpose of this utility model, technical solution and advantage clearer
Type is described in further detail.
~ structural schematic diagram shown in Fig. 4 referring to Fig.1.
A kind of unmanned plane structure of battery corer being readily disassembled of the utility model embodiment is powered for unmanned plane, can
It is directly mounted in the battery cavities of uav bottom.
Sliding is provided with gliding mass 2, a pair of of shank 3a, 3b, shank in the pedestal 1 of the battery cover of the utility model embodiment
Skewed slot 31 is provided on 3a, 3b, 2 two sides of gliding mass are respectively arranged with the traveller 21 being slidably connected with the skewed slot 31 of shank 3a, 3b, pin
Body 3a, 3b slidably stretches out end 1 two sides of pedestal, for being connected in pedestal 1.
Corresponding 2 two sides of gliding mass of pedestal 1 are provided with a pair of longitudinal card along 11a, 11b, and gliding mass 2 is slideably positioned in longitudinal card edge
Between 11a, 11b.
Corresponding, pedestal 1 is provided with shank transverse direction card and is slideably positioned in opposite direction along 12a, 12b, 12c, 12d, shank 3a
For the card of setting between 12a, 12b, shank 3b is slideably positioned in the card being arranged oppositely between 12c, 12d.
The lateral card edge of a pair of of shank is set with sliding.
The glide direction of shank 3a, 3b are vertical with the glide direction of gliding mass 2.
Preferably, the glide direction of skewed slot 31 and gliding mass is in 45 degree of angles.
It is provided with support 13 in pedestal 1, the spring 14 for acting on 2 top of gliding mass is provided in support 13.
2 surface of gliding mass is provided with unlatching and dials body 22, and sliding window 15 is arranged in the corresponding group body 22 of opening of box body 1.
When the utility model is used, dialling body 22 by pushing to open, make its shank 3a, 3b slid inward that links, shank
In the end retraction box body 1 of 3a, 3b, the incidental battery of the battery cover of the utility model can be dismounted, in answering for spring
Under the effect of position, it can quickly carry out being locked on unmanned plane, structure is simple, and use is efficient and convenient.
Certainly the above embodiments are only for explaining the technical ideas and features of the present invention, and its object is to allow be familiar with this
The people of technology can understand the content of the utility model and implement accordingly, and the protection model of the utility model can not be limited with this
It encloses.Any modifications made in accordance with the spirit of the main technical solutions of the utility model should all cover the guarantor in the utility model
Within the scope of shield.
Claims (8)
1. a kind of unmanned plane structure of battery corer being readily disassembled, which is characterized in that sliding is provided in the pedestal of the battery cover
Gliding mass, a pair of of shank are provided with skewed slot on the pair of shank, and the gliding mass two sides are respectively arranged with and the pair of shank
The pedestal two sides are slidably stretched out in the traveller that skewed slot is slidably connected, the pair of shank end.
2. the unmanned plane structure of battery corer according to claim 1 being readily disassembled, which is characterized in that setting in the pedestal
There is the spring for resetting the gliding mass.
3. the unmanned plane structure of battery corer according to claim 2 being readily disassembled, which is characterized in that setting in the pedestal
There is support, the spring one end is set in the support, and the other end acts at the top of the gliding mass.
4. the unmanned plane structure of battery corer according to claim 1 being readily disassembled, which is characterized in that the pedestal corresponds to institute
It states gliding mass two sides and is provided with a pair of longitudinal card edge, the gliding mass is slideably positioned in the pair of longitudinal card between.
5. the unmanned plane structure of battery corer according to claim 1 being readily disassembled, which is characterized in that the pedestal, which has, to be slided
The lateral card edge of the dynamic the pair of shank of setting.
6. the unmanned plane structure of battery corer according to claim 1 being readily disassembled, which is characterized in that the pair of shank
Glide direction is vertical with the glide direction of the gliding mass.
7. the unmanned plane structure of battery corer according to claim 6 being readily disassembled, which is characterized in that the skewed slot with it is described
The glide direction of gliding mass is in 45 degree of angles.
8. one 7 described in any item unmanned plane structure of battery corer being readily disassembled according to claim 1, which is characterized in that described
Gliding mass surface is provided with unlatching and dials body, and the box body corresponds to described open and dials body setting sliding window.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821435835.XU CN208835131U (en) | 2018-08-31 | 2018-08-31 | A kind of unmanned plane structure of battery corer being readily disassembled |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821435835.XU CN208835131U (en) | 2018-08-31 | 2018-08-31 | A kind of unmanned plane structure of battery corer being readily disassembled |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208835131U true CN208835131U (en) | 2019-05-07 |
Family
ID=66311857
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821435835.XU Active CN208835131U (en) | 2018-08-31 | 2018-08-31 | A kind of unmanned plane structure of battery corer being readily disassembled |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208835131U (en) |
-
2018
- 2018-08-31 CN CN201821435835.XU patent/CN208835131U/en active Active
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| GR01 | Patent grant | ||
| GR01 | Patent grant |