CN216750151U - Quick detach many compatible formula unmanned aerial vehicle battery rack and unmanned aerial vehicle - Google Patents
Quick detach many compatible formula unmanned aerial vehicle battery rack and unmanned aerial vehicle Download PDFInfo
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- CN216750151U CN216750151U CN202123022446.9U CN202123022446U CN216750151U CN 216750151 U CN216750151 U CN 216750151U CN 202123022446 U CN202123022446 U CN 202123022446U CN 216750151 U CN216750151 U CN 216750151U
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Abstract
The utility model discloses a many compatible formula unmanned aerial vehicle battery rack of quick detach and unmanned aerial vehicle belongs to the unmanned aerial vehicle field. The quick-release multi-compatible unmanned aerial vehicle battery rack comprises a battery rack and a battery support plate; the battery frame is fixedly provided with a connecting piece used for being connected with the body of the unmanned aerial vehicle, the battery frame is also fixedly provided with two parallel sliding rails which are arranged oppositely, and two side edges of the battery support plate are connected to the two sliding rails in a sliding manner; the battery carrier plate is provided with a fastening structure for fixing the position of a battery, two ends of the fastening structure are fixed through hollow holes arranged on the battery carrier plate, and the battery carrier plate is provided with a plurality of hollow holes so that the fastening structure is suitable for fixing batteries of various specifications; and the battery carrier plate is also fixed with a quick-release locking mechanism used for fixing the battery carrier plate relative to the battery frame. The utility model has the advantages of simple structure and reasonable design, can carry out unmanned aerial vehicle's battery fast and change, improve unmanned aerial vehicle executive task's efficiency to still be applicable to the battery of different specifications.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle field, in particular to many compatible formula unmanned aerial vehicle battery rack of quick detach and unmanned aerial vehicle.
Background
An unmanned aircraft, abbreviated as "drone", and abbreviated in english as "UAV", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer. Unmanned aerial vehicles can be classified into military use and civil use according to different application fields. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In the civil aspect, the unmanned aerial vehicle is widely applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, the use of the unmanned aerial vehicle is greatly expanded, and the unmanned aerial vehicle technology is actively applied and developed in the industry in various countries.
Among the prior art, unmanned aerial vehicle carries out the change in-process of battery after the outfield flight battery exhausts, often because the fixed mode of battery is complicated, is difficult to realize quick change to lead to the execution efficiency greatly reduced of flight task. Therefore, how to solve the problem of quick replacement of the battery is increasingly important.
SUMMERY OF THE UTILITY MODEL
The problem that the speed is slow is changed to the unmanned aerial vehicle battery that prior art exists, the utility model aims to provide a quick detach many compatible formula unmanned aerial vehicle battery rack and unmanned aerial vehicle.
In order to achieve the above purpose, the technical scheme of the utility model is that:
on one hand, the utility model provides a quick-release multi-compatible unmanned aerial vehicle battery rack, which comprises a battery rack and a battery support plate; the battery support is characterized in that a connecting piece used for being connected with a body of the unmanned aerial vehicle is fixedly arranged on the battery support, two parallel and oppositely arranged slide rails are also fixedly arranged on the battery support, and two side edges of the battery support plate are connected to the two slide rails in a sliding manner; the battery carrier plate is provided with a fastening structure for fixing the position of a battery, two ends of the fastening structure are fixed through hollow holes arranged on the battery carrier plate, and the battery carrier plate is provided with a plurality of hollow holes so that the fastening structure is suitable for fixing batteries with various specifications; and the battery support plate is also fixedly provided with a quick-release locking mechanism used for fixing the battery support plate relative to the battery rack.
Preferably, the quick-release locking mechanism is a spring bolt, and a pin hole matched with the spring bolt is formed in the battery rack.
Preferably, the battery rack comprises a bottom plate parallel to the battery carrier plate, and the connecting piece and the slide rail are both fixedly mounted on the bottom plate.
Preferably, the bottom plate comprises two symmetrically arranged and mutually independent sub-plates, and the connecting piece and the sliding rail are fixedly installed on each sub-plate.
Preferably, each daughter board is provided with the pin hole, and two sides of the battery carrier plate are respectively and correspondingly provided with the quick release locking mechanism.
Preferably, the connecting piece is fixedly mounted at two ends of each sub-board.
Preferably, the hollow hole is in a long strip shape.
Preferably, the fastening structure is a strap or a magic tape.
On the other hand, the utility model provides an unmanned aerial vehicle still, including the fuselage, still include fixed mounting be in as above on the fuselage the many compatible formula unmanned aerial vehicle battery racks of quick detach.
Adopt above-mentioned technical scheme, the utility model provides a many compatible formula unmanned aerial vehicle battery racks of quick detach's beneficial effect lies in: due to the arrangement of the slide rail on the battery frame, the battery support plate which is connected with the battery frame in a sliding way through the slide rail and used for loading the battery and the quick-release locking mechanism, when the battery is replaced, the battery support plate can be detached from the battery frame only by releasing the fixed connection relation between the battery support plate and the battery frame through the quick-release locking mechanism, the battery support plate loaded with a new battery is installed on the battery frame, and finally the battery support plate is locked and fixed through the quick-release locking mechanism; so, the dismouting process of battery is quick and the operation of being convenient for, can improve unmanned aerial vehicle greatly and carry out the efficiency of flight task.
Drawings
Fig. 1 is a schematic structural view of the battery rack of the fast-release multi-compatible unmanned aerial vehicle of the present invention;
fig. 2 is a schematic structural view of the battery rack of the quick-release multi-compatible unmanned aerial vehicle of the present invention in another direction;
fig. 3 is the utility model discloses the many compatible formula unmanned aerial vehicle battery racks's of quick detach plan view.
In the figure, 1-battery rack, 2-sliding rail, 3-battery carrier plate, 4-quick-release locking mechanism, 5-connecting piece and 6-battery.
Detailed Description
The following describes the present invention with reference to the accompanying drawings. It should be noted that the description of the embodiments is provided to help understanding of the present invention, but the present invention is not limited thereto. In addition, the technical features related to the embodiments of the present invention described below may be combined with each other as long as they do not conflict with each other.
It should be noted that, in the description of the present invention, the terms "upper", "lower", "left", "right", "front", "back", etc. indicate the orientation or position relationship of the structure of the present invention based on the drawings, and are only for the convenience of describing the present invention, but do not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and thus, should not be construed as limiting the present invention.
In the technical scheme, the terms "first" and "second" are only used for referring to the same or similar structures or corresponding structures with similar functions, and are not used for ranking the importance of the structures, or comparing the sizes or other meanings.
In addition, unless expressly stated or limited otherwise, the terms "mounted" and "connected" are to be construed broadly, e.g., the connection may be a fixed connection, a removable connection, or an integral connection; can be mechanically or electrically connected; the two structures can be directly connected or indirectly connected through an intermediate medium, and the two structures can be communicated with each other. To those skilled in the art, the specific meanings of the above terms in the present invention can be understood in relation to the present scheme in specific terms according to the general idea of the present invention.
Example one
A quick-release multi-compatibility unmanned aerial vehicle battery rack is shown in figures 1-3 and comprises a battery rack 1 and a battery support plate 3.
Wherein, battery support plate 3 is used for bearing the used battery of unmanned aerial vehicle, and battery support plate 1 is used for battery support plate 3 and makes battery support plate 3 conveniently follow battery support plate 1 dismouting, and battery support plate 1 is used for fixing and uses on unmanned aerial vehicle's fuselage. When the unmanned aerial vehicle needs to replace the battery, only the battery carrier plate 3 carrying the new battery needs to be replaced on the battery rack 1.
The battery holder 1 comprises a base plate which is generally parallel to the battery carrier plate 3. Fixed mounting has the connecting piece 5 that is used for being connected with unmanned aerial vehicle's fuselage on the bottom plate, and connecting piece 5 configuration is columnar structure, and there is a connecting piece 5 in the four corners of bottom plate through screw fixed mounting respectively, and the other end of connecting piece 5 then is connected with unmanned aerial vehicle's fuselage through the screw. Two parallel and oppositely arranged sliding rails 2 are fixedly mounted on the bottom plate, the two sliding rails 2 are respectively arranged on two sides of the bottom plate, and the sliding rails 2 are usually fixed through screws.
Correspondingly, two side edges of the battery carrier plate 3 are slidably connected to the two slide rails 2, so that the battery carrier plate 3 can slide relative to the battery rack 1, and the battery carrier plate 3 can be connected and separated relative to the battery rack 1 by configuring the end portions of the slide rails 2 to be in an open structure. Correspondingly, a quick-release locking mechanism 4 for fixing the battery carrier plate 3 relative to the battery rack 1 is also fixed on the battery carrier plate 3. In this embodiment, the quick-release locking mechanism 4 is a spring bolt, and the battery rack 1 only needs to be correspondingly provided with a pin hole adapted to the spring bolt. Or in other preferred embodiments, a quick-release locking mechanism 4 can be configured to screw a locking screw on the battery carrier plate 3, and the battery rack 1 only needs to be correspondingly provided with a threaded hole or a unthreaded hole matched with the locking screw.
Meanwhile, a fastening structure (not shown in the figure) for fixing the position of the battery 6 is configured on the battery carrier plate 3, two ends of the fastening structure are fixed through hollow holes formed in the battery carrier plate 3, and the battery 6 can be fixed on the battery carrier plate 3 after the fastening structure is fixed, for example, the fastening structure is configured as a binding band or a magic tape, and the corresponding preferable hollow holes are in a long strip shape. In order to meet the fixing requirements of batteries 6 of different specifications, a plurality of hollow holes are further arranged on the battery carrier plate 3, so that the fastening structure has a plurality of fixing positions, and the fastening structure is adapted to the fixing requirements of the batteries 6 of various specifications. In addition, the weight of the battery carrier plate 3 can be effectively reduced due to the arrangement of the hollow holes.
When the battery support plate is used, after the electric quantity of the battery 6 is used up, the battery support plate 3 can be taken out of the battery frame 1 only by releasing the fixed connection relation between the battery support plate 3 and the battery frame 1 through the quick-release locking mechanism 4, the prepared battery support plate 3 loaded with a new battery is installed on the battery frame 1, and finally the battery support plate 3 is locked and fixed through the quick-release locking mechanism 4. And the battery support plate 3 that takes off and change, then through fastening structure relieve the fixed connection of battery 6, take off the battery of insufficient power and charge can, and the battery support plate 3 that vacates is then used for installing new battery 6 to the battery of another unmanned aerial vehicle changes the use. So, the battery dismouting process of the battery frame that this embodiment provided is quick and the operation of being convenient for, can improve unmanned aerial vehicle greatly and carry out the efficiency of flight task to be suitable for the use of the battery of different specifications.
It is understood that the bottom plate and the battery carrier plate 3 are configured as carbon fiber composite plates for further weight reduction.
Example two
The difference from the first embodiment is that: in this embodiment, the bottom plate in the battery rack 1 is divided into two sub-boards which are symmetrically arranged and are independent from each other, and a connecting member 5 and a slide rail 2 are fixedly mounted on each sub-board. And, both ends of each daughter board are all fixedly mounted with connecting piece 5, correspond, all be provided with the pinhole on every daughter board, and the both sides of battery support plate 3 are provided with quick detach locking mechanism 4 respectively correspondingly.
So set up for the size of bottom plate obtains greatly reduced, thereby reduces the overall structure weight of battery frame.
EXAMPLE III
The utility model provides an unmanned aerial vehicle, includes the fuselage, still includes the many compatible formula unmanned aerial vehicle battery racks of quick detach as above embodiment of fixed mounting on the fuselage.
The embodiments of the present invention have been described in detail with reference to the accompanying drawings, but the present invention is not limited to the described embodiments. It will be apparent to those skilled in the art that various changes, modifications, substitutions and alterations can be made in the embodiments without departing from the principles and spirit of the invention, and these embodiments are still within the scope of the invention.
Claims (9)
1. The utility model provides a many compatible formula unmanned aerial vehicle battery rack of quick detach which characterized in that: the battery support plate is arranged on the battery support plate; the battery support is characterized in that a connecting piece used for being connected with a body of the unmanned aerial vehicle is fixedly arranged on the battery support, two parallel and oppositely arranged slide rails are also fixedly arranged on the battery support, and two side edges of the battery support plate are connected to the two slide rails in a sliding manner; the battery carrier plate is provided with a fastening structure for fixing the position of a battery, two ends of the fastening structure are fixed through hollow holes arranged on the battery carrier plate, and the battery carrier plate is provided with a plurality of hollow holes so that the fastening structure is suitable for fixing batteries with various specifications; and the battery support plate is also fixedly provided with a quick-release locking mechanism used for fixing the battery support plate relative to the battery rack.
2. The quick detach multi-compatible formula unmanned aerial vehicle battery rack of claim 1, characterized in that: the quick-release locking mechanism is a spring bolt, and a pin hole matched with the spring bolt is formed in the battery frame.
3. The quick release multi-compatible unmanned aerial vehicle battery stand of claim 2, wherein: the battery rack comprises a bottom plate parallel to the battery carrier plate, and the connecting piece and the sliding rail are fixedly arranged on the bottom plate.
4. The quick release multi-compatible unmanned aerial vehicle battery stand of claim 3, wherein: the bottom plate comprises two symmetrically arranged and mutually independent sub-plates, and the connecting piece and the sliding rail are fixedly installed on each sub-plate.
5. The quick release multi-compatible unmanned aerial vehicle battery stand of claim 4, wherein: each daughter board is provided with the pinhole, the both sides of battery support plate are provided with respectively correspondingly quick detach locking mechanism.
6. The quick release multi-compatible unmanned aerial vehicle battery stand of claim 4, wherein: and the connecting piece is fixedly arranged at the two ends of each daughter board.
7. The quick release multi-compatible unmanned aerial vehicle battery stand of claim 1, wherein: the hollow holes are in a long strip shape.
8. The quick release multi-compatible unmanned aerial vehicle battery stand of claim 7, wherein: the fastening structure is a bandage or a magic tape.
9. An unmanned aerial vehicle, includes the fuselage, its characterized in that: the quick release multi-compatible unmanned aerial vehicle battery holder as claimed in any one of claims 1-8, fixedly mounted on the fuselage.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202123022446.9U CN216750151U (en) | 2021-12-03 | 2021-12-03 | Quick detach many compatible formula unmanned aerial vehicle battery rack and unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202123022446.9U CN216750151U (en) | 2021-12-03 | 2021-12-03 | Quick detach many compatible formula unmanned aerial vehicle battery rack and unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN216750151U true CN216750151U (en) | 2022-06-14 |
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ID=81930389
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202123022446.9U Active CN216750151U (en) | 2021-12-03 | 2021-12-03 | Quick detach many compatible formula unmanned aerial vehicle battery rack and unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN216750151U (en) |
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2021
- 2021-12-03 CN CN202123022446.9U patent/CN216750151U/en active Active
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