CN210822786U - Unmanned aerial vehicle battery replacement device - Google Patents
Unmanned aerial vehicle battery replacement device Download PDFInfo
- Publication number
- CN210822786U CN210822786U CN201922003103.4U CN201922003103U CN210822786U CN 210822786 U CN210822786 U CN 210822786U CN 201922003103 U CN201922003103 U CN 201922003103U CN 210822786 U CN210822786 U CN 210822786U
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- China
- Prior art keywords
- aerial vehicle
- unmanned aerial
- rectangular
- rectangle
- local
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- Expired - Fee Related
Links
- 238000007789 sealing Methods 0.000 claims description 7
- 238000013016 damping Methods 0.000 claims description 6
- 125000003003 spiro group Chemical group 0.000 claims description 2
- 230000000694 effects Effects 0.000 abstract description 3
- 230000035939 shock Effects 0.000 abstract description 2
- 238000003780 insertion Methods 0.000 description 10
- 230000037431 insertion Effects 0.000 description 10
- 238000009434 installation Methods 0.000 description 4
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000000149 penetrating effect Effects 0.000 description 1
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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
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/70—Energy storage systems for electromobility, e.g. batteries
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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
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/7072—Electromobility specific charging systems or methods for batteries, ultracapacitors, supercapacitors or double-layer capacitors
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- Battery Mounting, Suspending (AREA)
Abstract
The utility model discloses an unmanned aerial vehicle battery replacement device, including the local casing of unmanned aerial vehicle, battery case and the sealed apron of L shape, be equipped with the rectangle concave groove in the local casing of unmanned aerial vehicle, there are four types of dogbone spliced eye of pegging graft with chucking device in the rectangle concave groove, chucking device dogbone spliced block, rectangle spout, rectangle slider, rectangle fixture block and spring, four rectangle fixture block on the chucking device corresponds respectively with the rectangle draw-in groove joint on the battery case, the fixed first fixture block that is equipped with two and two first draw-in groove one-to-one joints on the local casing of unmanned aerial vehicle of the sealed apron left end bottom of L shape, the fixed second fixture block that is equipped with two and two second draw-in groove one-to-ones joints on the local casing of unmanned aerial vehicle of the sealed apron right-hand member face of L. The utility model discloses make things convenient for battery case quick assembly disassembly to replace, the battery case is installed on unmanned aerial vehicle and is fixed effectual, and is stable good high and have good shock attenuation effect.
Description
Technical Field
The utility model belongs to the technical field of unmanned aerial vehicle, concretely relates to unmanned aerial vehicle battery replacement device.
Background
Unmanned aerial vehicle generalized definition is for not needing the driver to board the various remote control aircraft of driving, because unmanned aerial vehicle has no way directly to link to charge, its battery case all is that the dismantlement formula is changed and is used repeatedly supplementarily, the replacement of unmanned aerial vehicle battery case not only requires to change conveniently, fast, but the installation of battery case is fixed still to have good stability can and damping performance moreover, but the replacement of prior art's unmanned aerial vehicle battery case often does not reach above-mentioned requirement.
Therefore, we provide a make things convenient for battery case quick assembly disassembly replacement, and the battery case is installed on unmanned aerial vehicle and is fixed effectual, and stable good height just has the unmanned aerial vehicle battery replacement device of good shock attenuation effect to solve above-mentioned problem.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an unmanned aerial vehicle battery replacement device to solve the problem that proposes in the above-mentioned background art.
In order to achieve the above object, the utility model provides a following technical scheme: an unmanned aerial vehicle battery replacement device comprises an unmanned aerial vehicle local shell, a battery box and an L-shaped sealing cover plate, wherein a rectangular concave groove is arranged in the unmanned aerial vehicle local shell, four convex insertion holes which are fixedly inserted with four clamping devices respectively are fixedly arranged on the front side and the rear side of the rectangular concave groove on the unmanned aerial vehicle local shell, each clamping device comprises a convex insertion block which is inserted with the convex insertion hole and is fixed with the unmanned aerial vehicle local shell through a bolt, a rectangular sliding groove which is arranged on the convex insertion block, a rectangular sliding block which is arranged on the inner side of the rectangular sliding groove in a sliding manner, a rectangular clamping block which is fixedly arranged on the inner side of the rectangular sliding block and penetrates through a rectangular through hole on the convex insertion block, and a spring which is arranged on the inner side of the rectangular sliding groove and is fixedly connected with the rectangular sliding block and the convex insertion block, and the four rectangular clamping blocks on, the fixed first fixture block that is equipped with two and two first draw-in groove one-to-one joints on the local casing of unmanned aerial vehicle that is equipped with in L shape sealed apron left end bottom, the fixed second fixture block that is equipped with two and two second draw-in groove one-to-one joints on the local casing of unmanned aerial vehicle that is equipped with of L shape sealed apron right-hand member face.
Preferably, be equipped with four internal thread through-holes on the convex character form grafting piece, bolt and the local casing threaded connection of unmanned aerial vehicle that the spiro union is fixed on the internal thread through-hole.
Preferably, the rectangular concave groove is of a concave structure with an opening at the top and the left side.
Preferably, the local casing of unmanned aerial vehicle is last and be located the fixed rubber cushion that bonds of rectangle concave surface inslot side bottom.
Preferably, the L-shaped sealing cover plate is hermetically clamped at the top and the left side surface of the rectangular concave groove.
Preferably, the battery box is fixedly clamped on the inner side of the rectangular concave groove.
The utility model discloses a technological effect and advantage: this unmanned aerial vehicle battery replacement device, support the rectangle fixture block on two chucking devices of battery case leading flank on the front side, the spring is compressed, make rectangle fixture block and the rectangle draw-in groove joint on the battery case, then with the rectangle fixture block on two chucking devices on the local casing right side of unmanned aerial vehicle and the rectangle draw-in groove joint on the battery case, four rectangle fixture blocks two-wayly support the chucking and fix the battery case, it is convenient to the installation fixed position of battery case, and the dismantlement replacement of the battery case of being convenient for, correspond the joint through the fixture block on the L shape sealed cover board and the draw-in groove on the local casing of unmanned aerial vehicle, can effectual sealed rectangle concave surface groove, guarantee the stability and the security of battery case installation, protect the battery case, damping rubber pad well indian china hones.
Drawings
Fig. 1 is an exploded view of the present invention;
FIG. 2 is a schematic structural view of the clamping device of the present invention;
fig. 3 is a schematic structural view of the battery box fixed by the clamping device of the present invention.
In the figure: 1. an unmanned aerial vehicle local housing; 2. a battery case; 3. an L-shaped sealing cover plate; 4. a rectangular concave groove; 5. a shock-absorbing rubber pad; 6. a clamping device; 7. a convex-shaped plug hole; 8. a convex-shaped insertion block; 9. a rectangular chute; 10. a rectangular slider; 11. a rectangular through hole; 12. a rectangular fixture block; 13. a spring; 14. a rectangular clamping groove; 15. a first card slot; 16. a first clamping block; 17. a second card slot; 18. a second fixture block; 19. an internally threaded through bore.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
The utility model provides an unmanned aerial vehicle battery replacement device as shown in figures 1-3, which comprises an unmanned aerial vehicle partial shell 1, a battery box 2 and an L-shaped sealing cover plate 3, a rectangular concave groove 4 is arranged in the local shell 1 of the unmanned aerial vehicle, the rectangular concave groove 4 is of a concave structure with the top and the left side both being open, the battery box 2 is fixedly clamped at the inner side of the rectangular concave groove 4, the L-shaped sealing cover plate 3 is hermetically clamped at the top and the left side surface of the rectangular concave groove 4, the damping rubber pad 5 which supports and supports the battery box in a propping manner is fixedly bonded on the local shell 1 of the unmanned aerial vehicle and at the bottom of the inner side of the rectangular concave groove 4, the battery box 2 is fixedly clamped in the rectangular concave groove 4, and an opening on the rectangular concave groove 4 is sealed by the L-shaped sealing cover plate 3 after the battery box is mounted at the top of the damping rubber pad 5, so that the mounting stability and the damping performance of the battery box 2 can be effectively ensured;
four convex inserting holes 7 which are fixedly inserted with four clamping devices 6 respectively are fixedly arranged on the local shell 1 of the unmanned aerial vehicle and positioned at the front side and the rear side of the rectangular concave groove 4, the clamping devices 6 are inserted and fixed with the convex inserting holes 7, the clamping devices 6 can be hidden in the local shell 1 of the unmanned aerial vehicle, the space in the rectangular concave groove 4 is not occupied, and the rectangular concave groove 4 can conveniently limit and fix the battery box 2;
the clamping devices 6 comprise a convex splicing block 8 which is spliced with a convex splicing hole 7 and is fixed with the local shell 1 of the unmanned aerial vehicle through a bolt in a threaded manner, a rectangular sliding groove 9 arranged on the convex splicing block 8, a rectangular sliding block 10 arranged on the inner side of the rectangular sliding groove 9 in a sliding manner, a rectangular clamping block 12 fixedly arranged on the inner side of the rectangular sliding block 10 and penetrating through a rectangular through hole 11 on the convex splicing block 8, and a spring 13 arranged on the inner side of the rectangular sliding groove 9 and fixedly connecting the rectangular sliding block 10 with the convex splicing block 8, the battery box 2 is installed, the front side of the battery box 2 is pressed against the rectangular clamping blocks 12 on the two clamping devices 6 on the front side, the spring 13 is compressed, the rectangular clamping block 12 is clamped with the battery box 2, then the rectangular clamping blocks 12 on the two clamping devices 6 on the right side of the local shell 1 of the unmanned aerial vehicle are, the battery box is convenient to mount, fix and position, and the battery box 2 is convenient to detach and replace;
the convex insertion block 8 is provided with four internal thread through holes 19, bolts fixedly screwed on the internal thread through holes 19 are in threaded connection with the local unmanned aerial vehicle shell 1, and the convex insertion block 8 is provided with the internal thread through holes 19, so that the clamping device 6 is conveniently and fixedly screwed in the convex insertion holes 7 in the local unmanned aerial vehicle shell 1;
four last rectangle fixture block 12 of chucking device 6 corresponds respectively with the 14 joints of rectangle draw-in groove on the battery case 2, 3 left end bottoms of L shape sealed apron are fixed and are equipped with two first fixture blocks 16 with two first draw-in grooves 15 one-to-one joints on the local casing of unmanned aerial vehicle 1, 3 right-hand member faces of L shape sealed apron are fixed and are equipped with two second fixture blocks 18 with two second draw-in grooves 17 one-to-one joints on the local casing of unmanned aerial vehicle 1, four rectangle fixture blocks 12 two-way support the rectangle draw-in groove on the chucking fixed battery case 2, correspond the joint through the fixture block on the L shape sealed apron 3 and the draw-in groove on the local casing of unmanned aerial vehicle 1, can effectual sealed rectangle concave surface groove 4, guarantee the stability and the security of battery case installation.
Finally, it should be noted that: although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications and variations can be made in the embodiments or in part of the technical features of the embodiments without departing from the spirit and the scope of the invention.
Claims (6)
1. The utility model provides an unmanned aerial vehicle battery replacement device, includes local casing of unmanned aerial vehicle (1), battery case (2) and L shape sealed apron (3), its characterized in that: a rectangular concave groove (4) is arranged in the local shell (1) of the unmanned aerial vehicle, four convex splicing holes (7) which are fixedly spliced with four clamping devices (6) respectively are fixedly arranged on the local shell (1) of the unmanned aerial vehicle and positioned at the front side and the rear side of the rectangular concave groove (4), each clamping device (6) comprises a convex splicing block (8) which is spliced with the convex splicing hole (7) and is in threaded fixation with the local shell (1) of the unmanned aerial vehicle through a bolt, a rectangular sliding chute (9) arranged on the convex splicing block (8), a rectangular sliding block (10) which is arranged on the inner side of the rectangular sliding chute (9) in a sliding manner, a rectangular clamping block (12) which is fixedly arranged on the inner side of the rectangular sliding block (10) and penetrates through a rectangular through hole (11) on the convex splicing block (8), and a spring (13) which is arranged on the inner side of the rectangular sliding chute (9) and is fixedly connected with the rectangular sliding block (10, four rectangle fixture block (12) on chucking device (6) correspond respectively with rectangle draw-in groove (14) joint on battery case (2), L shape sealed apron (3) left end bottom is fixed be equipped with two with first fixture block (16) of two first draw-in grooves (15) one-to-one joint on the local casing of unmanned aerial vehicle (1), L shape sealed apron (3) right-hand member face is fixed be equipped with two with second fixture block (18) of two second draw-in grooves (17) one-to-one joints on the local casing of unmanned aerial vehicle (1).
2. The unmanned aerial vehicle battery replacement device of claim 1, wherein: be equipped with four internal thread through-holes (19) on the convex character form grafting piece (8), bolt and the local casing of unmanned aerial vehicle (1) threaded connection that the spiro union is fixed on internal thread through-hole (19).
3. The unmanned aerial vehicle battery replacement device of claim 1, wherein: the rectangular concave groove (4) is of a concave structure with an opening at the top and the left side.
4. The unmanned aerial vehicle battery replacement device of claim 1, wherein: the damping rubber pad (5) is fixedly bonded to the bottom of the inner side of the rectangular concave groove (4) on the local shell (1) of the unmanned aerial vehicle.
5. The unmanned aerial vehicle battery replacement device of claim 1, wherein: the L-shaped sealing cover plate (3) is hermetically clamped at the top and the left side of the rectangular concave groove (4).
6. The unmanned aerial vehicle battery replacement device of claim 1, wherein: the battery box (2) is fixedly clamped on the inner side of the rectangular concave groove (4).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922003103.4U CN210822786U (en) | 2019-11-19 | 2019-11-19 | Unmanned aerial vehicle battery replacement device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922003103.4U CN210822786U (en) | 2019-11-19 | 2019-11-19 | Unmanned aerial vehicle battery replacement device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210822786U true CN210822786U (en) | 2020-06-23 |
Family
ID=71273681
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201922003103.4U Expired - Fee Related CN210822786U (en) | 2019-11-19 | 2019-11-19 | Unmanned aerial vehicle battery replacement device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN210822786U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112072160A (en) * | 2020-09-21 | 2020-12-11 | 上海空间电源研究所 | Nesting and involution assembly fixture for rectangular flexible battery |
| CN113715678A (en) * | 2021-08-20 | 2021-11-30 | 航天时代飞鹏有限公司 | Rapid battery replacement method for freight unmanned aerial vehicle |
-
2019
- 2019-11-19 CN CN201922003103.4U patent/CN210822786U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112072160A (en) * | 2020-09-21 | 2020-12-11 | 上海空间电源研究所 | Nesting and involution assembly fixture for rectangular flexible battery |
| CN112072160B (en) * | 2020-09-21 | 2021-09-10 | 上海空间电源研究所 | Nesting and involution assembly fixture for rectangular flexible battery |
| CN113715678A (en) * | 2021-08-20 | 2021-11-30 | 航天时代飞鹏有限公司 | Rapid battery replacement method for freight unmanned aerial vehicle |
| CN113715678B (en) * | 2021-08-20 | 2023-10-17 | 航天时代飞鹏有限公司 | Quick replacement method for freight unmanned aerial vehicle battery |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20200623 Termination date: 20211119 |