Lithium battery for induction aircraft

Abstract

The lithium battery for the induction aircraft comprises an unmanned aerial vehicle body and a power connection socket installed on one side of the bottom end of the unmanned aerial vehicle body, and two trapezoidal hollow shells in mirror symmetry are installed at the bottom end of the unmanned aerial vehicle body; a lithium battery monomer which is used for being mutually plugged with the power connection socket and keeping electrical connection with the power connection socket is mounted between the two trapezoidal hollow shells, embedded grooves are formed in the left outer wall and the right outer wall of the lithium battery monomer, and an annular hollow sleeve is rotationally mounted in the center of the bottom of each trapezoidal hollow shell. The trapezoidal hollow shell is used for providing powerful lateral mechanical support for the battery, the clamping and embedding effect of the fan-shaped clamping plate and the embedded groove ensures that the battery is kept at a fixed position in the flying process, and the risk that the battery moves due to the inertia effect, bumping or sharp turning in the flying process is prevented.

Description

Technical Field

[0001] The utility model relates to the technical field of unmanned aerial vehicles, in particular to a lithium battery for an induction aircraft. Background Art

[0002] Sensor-based remote-controlled drone aircraft are widely used in various fields, including agricultural monitoring, environmental testing, film and television shooting, logistics and transportation, etc., and the power source of these aircraft mainly relies on lithium batteries. As the core power system of drones, lithium batteries provide the required electrical energy for the electric motor to ensure that the drone can take off, fly and land smoothly. The flight time, range and load capacity of the drone are directly related to the performance of the battery. The working principle of this type of lithium battery is mainly based on the embedding and de-embedding process of lithium ions. When charging, the external power supply applies voltage to the battery, and the lithium ions are separated from the positive electrode material, move to the negative electrode through the electrolyte, and embed in the negative electrode material. This process is accompanied by the flow of electrons from the external circuit to the negative electrode. During the discharge process, the lithium ions are separated from the negative electrode, return to the positive electrode through the electrolyte, and release energy for use by the drone's motor. At the same time, electrons flow from the negative electrode through the external circuit to the positive electrode, forming an electric current, which provides power for the drone;

[0003] For example, the shockproof and explosion-proof lithium battery pack for drones disclosed in authorization publication number CN220544101U includes a housing and lithium batteries. The housing has an opening on one side, and lithium batteries are inserted and installed inside the housing. Vertical shock absorbers are fixedly installed on the upper and lower sides of the housing, and horizontal shock absorbers are fixedly installed on the left and right sides of the housing. Buffer devices are fixedly installed between the multiple lithium batteries. The buffer devices prevent the multiple lithium batteries from colliding with each other. The vertical and horizontal shock absorbers cushion the impact, thereby preventing the lithium battery pack from vibrating violently when the drone hits the ground, thereby extending the service life of the lithium battery pack. However, during the implementation of the above technical solution, the lithium battery still uses a plug to connect to the socket on the drone to form an electrical connection. However, during flight, the drone may experience rapid acceleration, deceleration, and turning movements. At this time, the lithium battery, under the action of inertia, moves with the drone's battery socket, resulting in an unstable connection and intermittent power supply interruptions. This is particularly dangerous during flight and can easily cause the drone to lose power at high altitude and crash. Utility Model Content

[0004] The purpose of the present utility model is to provide a lithium battery for an induction aircraft, in which a lithium battery cell is placed between two trapezoidal hollow shells for resisting lateral forces, and a plug at the tail end of the lithium battery cell is connected to a power socket on the drone body. At this time, a fan-shaped clamping plate at the bottom end of the trapezoidal hollow shell is screwed into an embedded groove on the outer wall of the lithium battery cell, thereby utilizing the locking effect of the fan-shaped clamping plate and the embedded groove to prevent the lithium battery cell from moving back and forth, thereby solving the problems raised in the above-mentioned background technology.

[0005] To achieve the above-mentioned objectives, the present invention provides the following technical solutions: a lithium battery for an inductive aircraft, comprising a drone body and a power socket installed on one side of the bottom end of the drone body, wherein two mirror-symmetrical trapezoidal hollow shells are installed at the bottom end of the drone body, and a lithium battery cell for plugging into and maintaining electrical connection with the power socket is installed between the two trapezoidal hollow shells, and an embedded groove is provided on the left and right outer walls of the lithium battery cell, an annular hollow sleeve is rotatably installed at the center position of the bottom of the trapezoidal hollow shell, the bottom end of the annular hollow sleeve passes through the outside of the trapezoidal hollow shell and is installed with a fan-shaped clip, and the fan-shaped clip enters the embedded groove in a screw-in manner, an I-shaped sliding arm is slidably installed on one side of the interior of the trapezoidal hollow shell, a gear rack rotating structure for driving the annular hollow sleeve to rotate is provided on one side outer wall of the I-shaped sliding arm, and an elastic reset structure for forcing the I-shaped sliding arm to move out of the outside of the trapezoidal hollow shell is provided on one side inner wall of the trapezoidal hollow shell.

[0006] Preferably, a triangular arm is fixed to the bottom of the trapezoidal hollow shell, and the upper surface of the triangular arm is slidably matched with the lower surface of the I-shaped sliding arm.

[0007] Preferably, a baffle is fixed to one end of the I-shaped sliding arm, and the baffle is made of rubber material.

[0008] Preferably, the elastic reset structure includes a triangular seat installed on the inner wall of one side of the trapezoidal hollow shell, a coil spring installed on the outer wall of one side of the triangular seat, and a sinking cavity arranged inside the I-shaped slide arm, one end of the coil spring extends into the interior of the sinking cavity and is fixedly connected to the inner wall of one side of the sinking cavity.

[0009] Preferably, the gear rack rotating structure includes a hollow gear ring rotatably mounted at the bottom end of the drone body and a tooth groove arranged on the outer wall of one side of the I-shaped slide arm, the tooth groove and the hollow gear ring are engaged with each other, and the bottom end of the hollow gear ring is fixedly connected to the top end of the annular hollow sleeve.

[0010] Preferably, vertical rods are fixed on both sides of the bottom end of the hollow gear ring, and the bottom ends of the vertical rods are fixedly connected to the top edge position of the annular hollow sleeve.

[0011] Compared with the existing technology, the beneficial effects of the present invention are: the lithium battery for the induction aircraft is provided with a fan-shaped card plate, an I-shaped sliding arm and other structures that cooperate with each other, and the trapezoidal hollow shell provides strong lateral mechanical support for the battery, and the card-fitting effect of the fan-shaped card plate and the embedded groove ensures that the battery remains in a fixed position during the flight, preventing the risk of battery movement caused by inertia, bumps or sharp turns during the flight, and by improving the fixing method of the lithium battery, the probability of system failure caused by poor connection can be reduced, ensuring that the drone can successfully complete the flight mission and reducing the occurrence of accidents. BRIEF DESCRIPTION OF THE DRAWINGS

[0012] Figure 1 This is a schematic diagram of the main structure of the utility model;

[0013] Figure 2 This is a schematic diagram of the three-dimensional structure of the utility model Figure 1 ;

[0014] Figure 3 This is a schematic diagram of the three-dimensional structure of the utility model Figure 2 ;

[0015] Figure 4 This is a schematic diagram of the three-dimensional structure of the lithium battery cell of the present invention Figure 1 ;

[0016] Figure 5 This is a schematic diagram of the three-dimensional structure of the utility model after the trapezoidal hollow shell is removed;

[0017] Figure 6 This is a schematic diagram of the three-dimensional structure of the lithium battery cell of the present invention Figure 2 ;

[0018] Figure 7 This is a schematic diagram of the three-dimensional structure of the lithium battery cell of the present invention Figure 3 .

[0019] In the figure: 1. UAV body; 2. Lithium battery cell; 3. Power socket; 4. Embedded slot; 5. Trapezoidal hollow shell; 6. Annular hollow sleeve; 7. Fan-shaped clamping plate; 8. I-shaped sliding arm; 801. Baffle; 9. Elastic reset structure; 10. Triangular arm; 11. Gear rack rotation structure; 1101. Tooth groove; 1102. Hollow gear ring; 1103. Vertical pole. DETAILED DESCRIPTION

[0020] The following is a clear and complete description of the technical solutions in the embodiments of the present invention in conjunction with the accompanying drawings. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without making creative work are within the scope of protection of the present invention.

[0021] See also Figure 1-7 The utility model provides an embodiment: a lithium battery for an induction aircraft, comprising a drone body 1 and a power socket 3 installed on one side of the bottom end of the drone body 1, two mirror-symmetrical trapezoidal hollow shells 5 are installed at the bottom end of the drone body 1, a lithium battery cell 2 for plugging into and maintaining electrical connection with the power socket 3 is installed between the two trapezoidal hollow shells 5, and an embedded groove 4 is provided on the left and right outer walls of the lithium battery cell 2, an annular hollow sleeve 6 is rotatably installed at the center position of the bottom of the trapezoidal hollow shell 5, the bottom end of the annular hollow sleeve 6 passes through the outside of the trapezoidal hollow shell 5 and is installed with a fan-shaped clamping plate 7, the fan-shaped clamping plate 7 is screwed into the embedded groove 4, an I-shaped sliding arm 8 is slidably installed on one side of the interior of the trapezoidal hollow shell 5, and a baffle 801 is fixed at one end of the I-shaped sliding arm 8, and the baffle 801 is made of a rubber component;

[0022] A gear rack rotating structure 11 is provided on one side outer wall of the I-shaped slide arm 8 for driving the annular hollow sleeve 6 to rotate, and an elastic reset structure 9 is provided on one side inner wall of the trapezoidal hollow shell 5 for forcing the I-shaped slide arm 8 to move out of the trapezoidal hollow shell 5;

[0023] The gear rack rotating structure 11 includes a hollow gear ring 1102 rotatably mounted at the bottom end of the drone body 1 and a tooth groove 1101 provided on the outer wall of one side of the I-shaped sliding arm 8. The tooth groove 1101 and the hollow gear ring 1102 are meshed with each other. The bottom end of the hollow gear ring 1102 is fixedly connected to the top end of the annular hollow sleeve 6. Vertical rods 1103 are fixed on both sides of the bottom end of the hollow gear ring 1102. The bottom end of the vertical rod 1103 is fixedly connected to the top edge of the annular hollow sleeve 6.

[0024] When the lithium battery cell 2 needs to be removed from the drone body 1, the user manually pushes the I-shaped sliding arm 8 toward the inner side of the trapezoidal hollow shell 5, and the I-shaped sliding arm 8 drives the hollow gear ring 1102 to rotate through the tooth groove 1101, and then the hollow gear ring 1102 drives the annular hollow sleeve 6 and the fan-shaped clamping plate 7 to rotate through the vertical rod 1103, and then the fan-shaped clamping plate 7 is screwed out of the outside of the embedded groove 4, thereby disconnecting the embedded connection between the fan-shaped clamping plate 7 and the lithium battery cell 2, and the user can normally pull out the lithium battery cell 2 from the power socket 3. The operator only needs to screw in or out the fan-shaped clamping plate 7 to easily take out or put in the lithium battery. This design not only improves the efficiency of battery replacement, but also reduces the risk of damage caused by frequent operations;

[0025] A triangular arm 10 is fixed to the bottom of the trapezoidal hollow shell 5, and the upper surface of the triangular arm 10 is slidably fitted with the lower surface of the I-shaped sliding arm 8;

[0026] The elastic reset structure 9 includes a triangular seat installed on the inner wall of one side of the trapezoidal hollow shell 5, a coil spring installed on the outer wall of one side of the triangular seat, and a sink cavity arranged inside the I-shaped slide arm 8. One end of the coil spring extends to the inside of the sink cavity and is fixedly connected to the inner wall of one side of the sink cavity. When the I-shaped slide arm 8 is no longer subjected to external force, the coil spring in the elastic reset structure 9 forces the I-shaped slide arm 8 to move outward, thereby causing the gear rack rotation structure 11, the annular hollow sleeve 6, and the sector clamping plate 7 to move in the opposite direction, causing the sector clamping plate 7 to reset and wait for the next battery connection.

[0027] When the embodiment of the present application is in use, first, the lithium battery cell 2 is accurately placed in a predetermined position between the two trapezoidal hollow shells 5. The shape of the trapezoidal hollow shell 5 enables it to firmly wrap the two sides of the battery cell, providing a solid support structure. Its trapezoidal design helps to withstand lateral forces from all directions during flight, ensuring that the lithium battery cell 2 will not be displaced due to inertia during flight. After the lithium battery cell 2 is placed between the two trapezoidal hollow shells 5, the tail end plug of the lithium battery cell 2 is connected to the power socket 3 of the drone body 1. The electrical connection between the plug and the socket is the key to battery power supply and can transmit the battery's electrical energy to various systems of the drone. Before this, the user needs to manually push the I-shaped slide arm 8 toward the inside of the trapezoidal hollow shell 5 so that the I-shaped slide arm 8 gradually sinks into the trapezoidal hollow shell 5. The linear motion of the I-shaped slide arm 8 is converted into the annular hollow sleeve 6 through the gear rack rotating structure 11. The rotation of the fan-shaped card plate 7 causes the two fan-shaped card plates 7 to swing toward each other until the large end of the fan-shaped card plate 7 swings to the outside of the drone to avoid the fan-shaped card plate 7 blocking the connection of the trapezoidal hollow shell 5 and the lithium battery cell 2. When the battery plug is connected to the socket, the user releases the I-shaped slide arm 8, and the elastic action of the elastic reset structure 9 forces the I-shaped slide arm 8 to move out of the trapezoidal hollow shell 5, and the gear rack rotation structure 11 forces the annular hollow sleeve 6 and the fan-shaped card plate 7 to reset. At this time, the fan-shaped card plate 7 is screwed in and engaged with the embedded groove 4 on the outer wall of the lithium battery cell 2. The embedded structure can effectively prevent the lithium battery cell 2 from moving back and forth, ensuring the stable position of the battery during flight. At this time, the connection between the lithium battery cell 2 and the drone body 1 can work stably and reliably, improving the connection stability between the battery and the drone body, reducing the risk of power connection interruption, and ensuring that the drone can fly stably.

Claims

1. A lithium battery for induction aircraft, characterized by: The invention comprises a drone body (1) and an electrical socket (3) installed at one side of the bottom end of the drone body (1), wherein two mirror-symmetrical trapezoidal hollow shells (5) are installed at the bottom end of the drone body (1), and a lithium battery cell (2) for plugging into and maintaining electrical connection with the electrical socket (3) is installed between the two trapezoidal hollow shells (5), and the left and right outer walls of the lithium battery cell (2) are both provided with an embedded groove (4), and an annular hollow sleeve (6) is rotatably installed at the center position of the bottom of the trapezoidal hollow shell (5), and the annular hollow sleeve (6) The bottom end of the trapezoidal hollow shell (5) passes through the outside of the trapezoidal hollow shell and is installed with a fan-shaped card plate (7). The fan-shaped card plate (7) is screwed into the embedded groove (4). An I-shaped sliding arm (8) is slidably installed on one side of the interior of the trapezoidal hollow shell (5). A gear rack rotating structure (11) for driving the annular hollow sleeve (6) to rotate is provided on one side outer wall of the I-shaped sliding arm (8). An elastic reset structure (9) for forcing the I-shaped sliding arm (8) to move out of the outside of the trapezoidal hollow shell (5) is provided on one side inner wall of the trapezoidal hollow shell (5).

2. The lithium battery for induction aircraft according to claim 1, characterized in that: A triangular arm (10) is fixed to the bottom of the trapezoidal hollow shell (5), and the upper surface of the triangular arm (10) and the lower surface of the I-shaped sliding arm (8) are in sliding engagement.

3. The lithium battery for induction aircraft according to claim 1, characterized in that: A baffle (801) is fixed to one end of the I-shaped sliding arm (8), and the baffle (801) is made of a rubber material.

4. The lithium battery for induction aircraft according to claim 1, characterized in that: The elastic reset structure (9) comprises a triangular seat mounted on the inner wall of one side of the trapezoidal hollow shell (5), a coil spring mounted on the outer wall of one side of the triangular seat, and a sink cavity provided inside the I-shaped sliding arm (8), one end of the coil spring extending into the interior of the sink cavity and fixedly connected to the inner wall of one side of the sink cavity.

5. The lithium battery for induction aircraft according to claim 1, characterized in that: The gear rack rotating structure (11) comprises a hollow gear ring (1102) rotatably mounted on the bottom end of the drone body (1) and a tooth groove (1101) provided on the outer wall of one side of the I-shaped sliding arm (8), wherein the tooth groove (1101) and the hollow gear ring (1102) are meshed with each other, and the bottom end of the hollow gear ring (1102) is fixedly connected to the top end of the annular hollow sleeve (6).

6. The lithium battery for induction aircraft according to claim 5, characterized in that: Vertical rods (1103) are fixed on both sides of the bottom end of the hollow tooth ring (1102), and the bottom ends of the vertical rods (1103) are fixedly connected to the top edge of the annular hollow sleeve (6).

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