Anti-falling battery compartment for unmanned aerial vehicle
By using a combined structure of a compartment cover, spring and limit rod in the drone battery compartment, the two limits of the battery are achieved, the battery is solved, the battery is shedding problem is ensured, the flight stability of the drone is allowed, and the battery compartment is allowed to be The replacement solves the battery installation problem.
Patent Information
- Application Number
- CN202421186457.1
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-05-28
- Publication Date
- 2025-01-07
- Estimated Expiration
- 2034-05-28
AI Technical Summary
The existing drone battery compartment has a condition after long-term use, causing the battery to fall off, causing the drone to fail and reduce flight stability.
A battery compartment is designed to prevent falling off, and the two types of batteries are realized through a combined structure of the compartment cover, the first spring, the first limiting rod, the fixed rod, the rotating rod, the fixed block, the second spring and the second limiting rod. The secondary limit ensures the stable position of the battery in the battery compartment, and facilitates the replacement and installation of the battery compartment through the connection between bolts and positioning blocks.
It effectively avoids the phenomenon of battery falling off, ensures the flight stability of the drone, and allows the replacement of the battery compartment, solving the battery installation problem.
Smart Images

Figure CN222310939U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the technical field of unmanned aerial vehicles, in particular to an anti-dropping battery compartment for unmanned aerial vehicles. Background Art
[0002] Unmanned aerial vehicles, referred to as "drones", are unmanned aircraft that are controlled by radio remote control equipment and self-contained program control devices, or are operated completely or intermittently autonomously by on-board computers. Existing drones need to be equipped with energy storage devices such as batteries during operation.
[0003] The battery of a drone is usually installed in the battery compartment of the drone, but the existing drone battery compartment only uses a set of limiting devices to fix the drone. When the limiting device fails after long-term use, the battery of the drone will fall off, causing the drone to malfunction and reducing the stability of the drone during flight. Utility Model Content
[0004] The purpose of the utility model is to provide an anti-drop battery compartment for a drone, so as to solve the problem proposed in the above background technology that when a limit device fails after long-term use, the battery of the drone may drop out, causing drone failure and reducing the stability of the drone during flight.
[0005] To achieve the above-mentioned purpose, the utility model provides the following technical solutions: an anti-falling battery compartment for a drone, comprising a drone body, a battery compartment body fixedly installed at the bottom of the drone body, a storage battery fixedly installed inside the battery compartment body, an anti-falling mechanism arranged on the surface of the battery compartment body, the anti-falling mechanism comprising a compartment cover, the compartment cover is snap-connected to the surface of the battery compartment body, a first spring is fixedly connected to the surface of the battery compartment body, a first limiting rod is fixedly connected to the surface of the first spring, a fixing rod is fixedly connected to the inner surface of the drone body, a rotating rod is rotatably connected to the surface of the fixing rod, a fixing block is fixedly connected to the surface of the battery compartment body, a second spring is fixedly connected to the surface of the fixing block, and a second limiting rod is fixedly connected to the surface of the second spring.
[0006] Preferably, a mounting mechanism is provided on the surface of the drone body, the mounting mechanism comprises a mounting block, a bolt is fixedly connected to the surface of the mounting block, a positioning block is fixedly connected to the surface of the battery compartment body, and a nut is threadedly connected to the surface of the bolt.
[0007] Preferably, the compartment cover is in a stepped shape, a circular hole is provided on the surface of the compartment cover, a guide hole is provided on the surface of the battery compartment body, and the first limiting rod slides through the guide hole of the battery compartment body to be inserted into the circular hole of the compartment cover.
[0008] Preferably, two groups of the fixing rods are provided, circular holes are provided on the surfaces of the fixing rods, the rotating rods rotate on the circular holes of the fixing rods, both ends of the rotating rods are limit blocks, and a group of the limit blocks is provided with a circular groove.
[0009] Preferably, all guide grooves are opened on the surface of the fixed block, the second spring is fixedly connected to the guide groove of the fixed block, the second limit rod slides on the guide groove of the fixed block, and the second limit rod is inserted into the circular groove of the rotating rod limit block.
[0010] Preferably, four groups of the mounting blocks and positioning blocks are provided, circular holes are opened on the surfaces of the positioning blocks, and the bolts are connected to the circular holes of the positioning blocks through holes.
[0011] Preferably, the nut is fixedly connected to the positioning block on the mounting block by means of bolts, and the battery compartment body is fixedly mounted on the bottom of the drone body by means of the positioning block and the mounting block.
[0012] Compared with the prior art, the beneficial effects of the utility model are:
[0013] 1. Through the cooperation between the compartment cover, the first spring, the first limit rod, the fixed rod, the rotating rod, the fixed block, the second spring and the second limit rod, the battery is limited twice. When a limit failure occurs in one set of limits, the other set of limits can still ensure the position of the battery inside the battery compartment body, avoiding failures during the flight of the drone and ensuring the stability of the drone.
[0014] 2. Pass the bolt through the circular hole of the positioning block to make the battery compartment body and the drone body contact and connect. The nut fixes the positioning block on the mounting block through the bolt. The battery compartment body is fixed to the bottom of the drone body through the positioning block and the mounting block. When the battery compartment body is damaged, the battery compartment body can be replaced to avoid the battery being unable to be installed on the drone body. BRIEF DESCRIPTION OF THE DRAWINGS
[0015] Figure 1 It is a front view stereoscopic schematic diagram of the structure of the utility model;
[0016] Figure 2 It is a three-dimensional schematic diagram of the structure of the utility model, viewed from the front and looking upward;
[0017] Figure 3 For this utility model Figure 2 A schematic diagram of the enlarged structure at A in the middle;
[0018] Figure 4 It is a front view and a sectional perspective schematic diagram of the bin cover structure of the utility model;
[0019] Figure 5 It is a top cross-sectional schematic diagram of the bin cover structure of the utility model.
[0020] In the figure: 1. UAV body; 11. Battery compartment body; 12. Battery; 2. Compartment cover; 21. First spring; 22. First limit rod; 23. Fixing rod; 24. Rotating rod; 25. Fixing block; 26. Second spring; 27. Second limit rod; 3. Mounting block; 31. Bolt; 32. Positioning block; 33. Nut. DETAILED DESCRIPTION
[0021] The following will be combined with the drawings in the embodiments of the utility model to clearly and completely describe the technical solutions in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all of the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the utility model.
[0022] See also Figure 1-5 , an embodiment provided by the utility model:
[0023] A battery compartment for drones with an anti-falling function comprises a drone body 1, a battery compartment body 11 is fixedly mounted on the bottom of the drone body 1, a storage battery 12 is fixedly mounted inside the battery compartment body 11, an anti-falling mechanism is arranged on the surface of the battery compartment body 11, the anti-falling mechanism comprises a compartment cover 2, the compartment cover 2 is snap-connected to the surface of the battery compartment body 11, a first spring 21 is fixedly connected to the surface of the battery compartment body 11, a first limiting rod 22 is fixedly connected to the surface of the first spring 21, a fixing rod 23 is fixedly connected to the inner surface of the drone body 1, a rotating rod 24 is rotatably connected to the surface of the fixing rod 23, a fixing block 25 is fixedly connected to the surface of the battery compartment body 11, a second spring 26 is fixedly connected to the surface of the fixing block 25, a second limiting rod 27 is fixedly connected to the surface of the second spring 26, and the high anti-falling mechanism sets two limiting positions on the battery compartment body 11 for the storage battery 12, thereby preventing the storage battery 12 from falling off the battery compartment body 11.
[0024] Furthermore, a mounting mechanism is provided on the surface of the drone body 1, and the mounting mechanism includes a mounting block 3, a bolt 31 is fixedly connected to the surface of the mounting block 3, a positioning block 32 is fixedly connected to the surface of the battery compartment body 11, and a nut 33 is threadedly connected to the surface of the bolt 31. The battery compartment body 11 is usually fixedly connected to the drone body 1. The battery compartment body 11 is installed on the drone body 1 through the mounting mechanism, which facilitates the removal of the battery compartment body 11 from the drone body 1 for replacement, thereby preventing the battery 12 from being unable to be installed after the battery compartment body 11 is damaged.
[0025] Furthermore, the compartment cover 2 is in a stepped shape, a circular hole is provided on the surface of the compartment cover 2, a guide hole is provided on the surface of the battery compartment body 11, the first limiting rod 22 slides through the guide hole of the battery compartment body 11 to be inserted into the circular hole of the compartment cover 2, the elastic force of the first spring 21 acts on the first limiting rod 22, the first limiting rod 22 limits the position of the compartment cover 2 on the battery compartment body 11, one side of the compartment cover 2 is in contact with and connected to the battery 12, the compartment cover 2 limits the position of the battery 12 on the battery compartment body 11, thereby achieving the limitation of the battery 12.
[0026] Furthermore, two groups of fixed rods 23 are provided, and a circular hole is opened on the surface of the fixed rod 23. The rotating rod 24 rotates on the circular hole of the fixed rod 23. The two ends of the rotating rod 24 are limit blocks, and the limit blocks rotate with the rotating rod 24. One group of limit blocks is opened on the circular groove, and the other group of limit blocks is in contact with the surface of the battery 12. The rotating rod 24 performs secondary limiting on the battery 12 through the limit blocks. The two groups of limit blocks of the rotating rod 24 are perpendicular to 24. During the rotation process, the limit blocks of 24 gradually come into contact with the battery 12 from one side of the fixed rod 23. At this time, the rotating rod 24 needs to keep its angle unchanged.
[0027] Furthermore, all guide grooves are opened on the surface of the fixed block 25, the second spring 26 is fixedly connected to the guide groove of the fixed block 25, the second limit rod 27 slides on the guide groove of the fixed block 25, the second limit rod 27 is inserted into the circular groove of the limit block of the rotating rod 24, the elastic force of the second spring 26 acts on the second limit rod 27, and the second limit rod 27 limits the rotation of the rotating rod 24 on the fixed rod 23 through the limit block of the rotating rod 24, thereby maintaining the position of the rotating rod 24 on the fixed rod 23.
[0028] Furthermore, four groups of mounting blocks 3 and positioning blocks 32 are provided, circular holes are opened on the surfaces of the positioning blocks 32, bolts 31 are penetrated and connected to the circular holes of the positioning blocks 32, the bolts 31 limit the position of the positioning blocks 32 on the mounting blocks 3, and the mounting blocks 3 and the positioning blocks 32 are contacted and connected together, so that the mounting blocks 3 and the positioning blocks 32 are conveniently connected.
[0029] Furthermore, the width of the battery compartment body 11 is the same as the width of the drone body 1, which facilitates the installation of the battery compartment body 11. The nut 33 fixes the positioning block 32 to the mounting block 3 through the bolt 31. The battery compartment body 11 is fixedly installed on the bottom of the drone body 1 through the positioning block 32 and the mounting block 3. When the battery compartment body 11 is damaged, the battery compartment body 11 can be replaced, thereby facilitating the installation of the battery 12.
[0030] Working principle: After the battery 12 is placed inside the battery compartment body 11, the first limiting rod 22 is pulled to deform the first spring 21, and the compartment cover 2 is snap-connected to the opening of the battery compartment body 11. After the first limiting rod 22 is released, under the elastic force of the first spring 21, the first limiting rod 22 slides on the guide hole of the battery compartment body 11 to the circular hole plugged into the compartment cover 2. The first limiting rod 22 limits the position of the compartment cover 2 on the battery compartment body 11, and the compartment cover 2 limits the position of the battery 12 on the battery compartment body 11. At this time, the second limiting rod 22 slides on the fixing block 25. Rod 27, so that the second limiting rod 27 squeezes the second spring 26, and the rotating rod 24 is rotated on the surface of the fixed rod 23, so that the limiting block at one end of the rotating rod 24 contacts and connects to the battery 12, thereby again limiting the position of the battery 12 on the battery compartment body 11, and loosening the second limiting rod 27. Under the elastic force of the second spring 26, the second limiting rod 27 will slide on the fixed block 25 to the circular groove inserted into the other set of limiting blocks of the rotating rod 24, thereby limiting the rotating rod 24 from continuing to rotate on the fixed rod 23, thereby ensuring the stability of the rotating rod 24 in limiting the battery 12.
[0031] The bolt 31 is passed through the circular hole of the positioning block 32 to make the battery compartment body 11 and the drone body 1 contact and connect. The nut 33 fixes the positioning block 32 on the mounting block 3 through the bolt 31. The battery compartment body 11 is fixedly mounted on the bottom of the drone body 1 through the positioning block 32 and the mounting block 3. When the battery compartment body 11 is damaged, the battery compartment body 11 can be replaced to avoid the battery 12 being unable to be installed on the drone body 1.
[0032] It is obvious to those skilled in the art that the present invention is not limited to the details of the exemplary embodiments described above, and that the present invention can be implemented in other specific forms without departing from the spirit or essential features of the present invention. Therefore, the embodiments should be regarded as exemplary and non-restrictive from any point of view, and the scope of the present invention is defined by the appended claims rather than the above description, and it is intended that all changes falling within the meaning and scope of the equivalent elements of the claims be included in the present invention. Any reference numeral in a claim should not be regarded as limiting the claim to which it relates.
Claims
1. An anti-drop battery compartment for a drone, comprising a drone body (1), characterized in that: A battery compartment body (11) is fixedly mounted on the bottom of the drone body (1), a storage battery (12) is fixedly mounted inside the battery compartment body (11), an anti-falling mechanism is arranged on the surface of the battery compartment body (11), the anti-falling mechanism comprises a compartment cover (2), the compartment cover (2) is snap-connected to the surface of the battery compartment body (11), a first spring (21) is fixedly connected to the surface of the battery compartment body (11), a first limit rod (22) is fixedly connected to the surface of the first spring (21), a fixing rod (23) is fixedly connected to the inner surface of the drone body (1), a rotating rod (24) is rotatably connected to the surface of the fixing rod (23), a fixing block (25) is fixedly connected to the surface of the battery compartment body (11), a second spring (26) is fixedly connected to the surface of the fixing block (25), and a second limit rod (27) is fixedly connected to the surface of the second spring (26).
2. The anti-drop battery compartment for drone according to claim 1, characterized in that: A mounting mechanism is arranged on the surface of the drone body (1), the mounting mechanism comprising a mounting block (3), a bolt (31) being fixedly connected to the surface of the mounting block (3), a positioning block (32) being fixedly connected to the surface of the battery compartment body (11), and a nut (33) being threadedly connected to the surface of the bolt (31).
3. The anti-drop battery compartment for drone according to claim 1, characterized in that: The compartment cover (2) is in a stepped shape, a circular hole is provided on the surface of the compartment cover (2), a guide hole is provided on the surface of the battery compartment body (11), and the first limiting rod (22) slides through the guide hole of the battery compartment body (11) to be inserted into the circular hole of the compartment cover (2).
4. The anti-drop battery compartment for drone according to claim 3, characterized in that: The fixing rod (23) is provided with two groups, and a circular hole is opened on the surface of the fixing rod (23). The rotating rod (24) rotates on the circular hole of the fixing rod (23). Both ends of the rotating rod (24) are limit blocks, and a group of limit blocks is opened with a circular groove.
5. The anti-drop battery compartment for drone according to claim 4, characterized in that: All guide grooves are formed on the surface of the fixed block (25); the second spring (26) is fixedly connected to the guide grooves of the fixed block (25); the second limit rod (27) slides on the guide grooves of the fixed block (25); and the second limit rod (27) is plugged into the circular groove of the limit block of the rotating rod (24).
6. The anti-drop battery compartment for drone according to claim 2, characterized in that: Four groups of the mounting blocks (3) and positioning blocks (32) are provided. A circular hole is provided on the surface of the positioning block (32). The bolts (31) are connected to the circular hole of the positioning block (32) through a through hole.
7. The anti-drop battery compartment for drone according to claim 6, characterized in that: The nut (33) is used to fix the positioning block (32) to the mounting block (3) via the bolt (31); the battery compartment body (11) is fixedly mounted on the bottom of the drone body (1) via the positioning block (32) and the mounting block (3).