Unmanned aerial vehicle power supply capable of being quickly assembled and installation method thereof

Abstract

The invention discloses an unmanned aerial vehicle power source capable of being rapidly assembled and an installation method thereof, and relates to the technical field of unmanned aerial vehicle power sources, the unmanned aerial vehicle power source comprises a battery bin, the battery bin is fixedly connected to the outer wall of the bottom of an unmanned aerial vehicle body, a shell is inserted into the battery bin, and a battery body is fixedly connected into the shell; one end of a wiring terminal is inserted into the shell, a first positioning assembly used for fixing the shell is arranged at the bottom of the battery bin, a second positioning assembly used for locking the shell is arranged in the battery bin, and a driving assembly is arranged in the shell. According to the invention, the two sides of the shell are locked and fixed, and in the whole mounting process, people only need to complete one action of inserting the shell into the battery compartment, so that the quick mounting of the battery body is realized, and the mounting efficiency of people on the battery body is improved.

Description

Technical Field

[0001] The present invention relates to the technical field of unmanned aerial vehicle power supply, and in particular to a quickly assembled unmanned aerial vehicle power supply and an installation method thereof. Background Art

[0002] Unmanned aircraft is referred to as "drone". It is an unmanned aircraft that is controlled by radio remote control equipment and self-contained program control devices. Drone is actually a general term for unmanned aerial vehicles.

[0003] In order to ensure continuous flight, traditional drones are generally connected to a power supply to achieve continuous power supply to the drone. At present, in order to ensure the connection stability of the power supply and prevent the power supply from falling off during use, existing drones are all provided with a receiving slot for the power supply on the drone body, and the receiving slot is generally composed of a side shell, an upper shell and a lower shell, and then during assembly, the power supply is inserted into the receiving slot from top to bottom. However, such a design makes it difficult to plug and unplug the power supply, which is inconvenient for people to install the power supply.

[0004] After searching, the Chinese utility model patent with announcement number CN213636197U discloses a drone battery assembly that is easy to install, wherein the limiting slide rail drives the battery body to slide into the limiting slide groove, the positioning column is engaged in the fixing hole, the support plate supports the support column, the support column limits the restoring spring, the rotating member drives the limiting member to rotate, and the limiting member is engaged in the limiting hole to fix the battery body.

[0005] Based on the existing technologies, the above patents still have the following deficiencies: the entire battery assembly is locked and fixed only by a set of limiters, and its locking ability is limited, which results in the battery assembly having a relatively poor stability after being fixed, and is prone to loosening and falling when the drone is working. Therefore, a drone power supply that can be quickly assembled and its installation method are urgently needed to solve the above problems. Summary of the invention

[0006] In view of the problems in the related art, the present invention proposes a quickly assembled drone power supply and an installation method thereof to overcome the above-mentioned technical problems existing in the existing related art.

[0007] The technical solution of the present invention is achieved in this way:

[0008] A power supply for a drone that can be quickly assembled includes a battery compartment, the battery compartment is fixedly connected to the bottom outer wall of the drone body, a shell is inserted into the battery compartment, a battery body is fixedly connected to the shell, and one end of a terminal is inserted into the shell.

[0009] A first positioning assembly for fixing the shell is provided at the bottom of the battery compartment;

[0010] A second positioning assembly for locking the shell is provided inside the battery compartment;

[0011] A driving assembly is disposed inside the housing;

[0012] The second positioning assembly includes a guide column and a second spring fixedly connected to the inner wall of one side of the battery compartment, the circumferential outer wall of the guide column is sleeved with a baffle frame, the top outer wall of the shell is fixedly connected to a push rod, one side outer wall of the push rod contacts one side outer wall of the baffle frame, both side inner walls of the battery compartment are fixedly connected to a third spring, one end of the third spring is fixedly connected to a block, both side outer walls of the shell are provided with a slot, one end of the block passes through the inside of the slot, one side outer wall of the block is fixedly connected to a movable column, one end of the movable column away from the block extends to the outside of the battery compartment, one end of the movable column extending to the outside of the battery compartment is fixedly connected to a bent rod, both side outer walls of the battery compartment are provided with a through slot, and one end of the bent rod away from the movable column passes through the inside of the through slot.

[0013] Further, the driving assembly includes a rack fixedly connected to one end of the bent rod, the rack meshing with a first gear, the circumferential inner wall of the first gear fixedly connected with a second rotating column, both ends of the second rotating column are rotatably connected to the inner walls of both sides of the shell, the circumferential outer wall of the second rotating column is fixedly connected with a third gear, the third gear meshing with a second gear, the circumferential inner wall of the second gear fixedly connected with a third rotating column, the circumferential outer wall of the second gear meshing with a gear fan, one side inner wall of the shell fixedly connected with a fixed seat, the second rotating column and the third rotating column are both rotatably connected to the fixed seat.

[0014] Furthermore, both side outer walls of the battery compartment are provided with first ventilation holes distributed at equal distances, and both side outer walls of the shell are provided with second ventilation holes distributed at equal distances.

[0015] Furthermore, the first positioning assembly includes a second rectangular groove opened on the bottom inner wall of the shell and a first rectangular groove opened on the bottom inner wall of the battery compartment, the specifications of the first rectangular groove are the same as the specifications of the second rectangular groove, the first rectangular groove is connected to the second rectangular groove, the inner walls on both sides of the second rectangular groove are rotatably connected to the first rotating column, the circumferential outer wall of the first rotating column is fixedly connected to the sleeves distributed at equal distances, the circumferential outer wall of the sleeve is fixedly connected to the movable plate, and the end of the movable plate away from the sleeve passes through the inside of the first rectangular groove and the second rectangular groove.

[0016] Furthermore, one side outer wall of the two groups of movable plates is fixedly connected with a first spring, and one end of the first spring away from the movable plate is fixedly connected to one side inner wall of the shell.

[0017] Furthermore, the bottom outer wall of the battery compartment is fixedly connected with a side plate, the movable plate is located in the middle of the two groups of side plates, and the two groups of side plates and the movable plate form a heat dissipation channel.

[0018] Furthermore, an air inlet groove is formed on one side outer wall of the two groups of side panels, and an air guide cover is fixedly connected to one side outer wall of the two groups of side panels close to the movable plate. One end of the air guide cover is fixedly connected to a guide plate, and the cross-section of the guide plate is wavy. The air inlet groove is connected to the air guide cover.

[0019] Furthermore, a baffle is fixedly connected to an inner wall of one side of the second rectangular groove, and the battery body is fixedly connected to an inner wall of one side of the shell through a reinforcing frame.

[0020] Furthermore, a slot is provided on one side of the battery compartment, one end of the shell passes through the inside of the slot, and a connecting plate is fixedly connected to an outer wall of one side of the shell.

[0021] A method for installing a drone power supply, which uses the drone power supply that can be quickly assembled as described in the above embodiment, comprises the following steps:

[0022] S1: Insert one end of the shell into the slot at the end of the battery compartment until the battery body and the terminal are fully matched;

[0023] S2: The clamping block is clamped in the clamping grooves on both sides of the shell by the pressure of the third spring to lock the shell;

[0024] S3: When the driving assembly is working, the multiple groups of movable plates in the first positioning assembly are inserted into the first rectangular groove and the second rectangular groove, completing the secondary fixing and locking of the housing;

[0025] S4: Pull the bent rods on both sides to disengage the card block from the card slot, and then pull the shell out of the battery compartment to complete the disassembly of the shell and the battery body.

[0026] Beneficial effects of the present invention:

[0027] The present invention provides a rapidly assembled drone power supply and an installation method thereof. By providing a second positioning component, when the power supply needs to be installed, one end of the shell can be first inserted into the slot at the end of the battery compartment until the push rod at the top of the shell contacts the baffle frame. At this time, the outer walls of one side of the two groups of card blocks inside the battery compartment both contact the outer walls of one side of the baffle frame, and the third spring is in a compressed state. When the shell continues to be pushed in, the push rod pushes the baffle frame to move in a direction close to the wiring terminal until the card block is completely unobstructed by the baffle frame. At this time, the card block contacts the outer wall of one side of the shell through the elastic force of the third spring. When the battery body inside the shell is completely matched with the wiring terminal, the card slots on both sides of the shell just match the card block. At this time, the card block is instantly ejected into the card slot by the elastic force of the third spring, thereby realizing locking and fixing of the two sides of the shell. During the entire installation process, people only need to complete an action of inserting the shell into the battery compartment, thereby realizing rapid installation of the battery body and improving people's installation efficiency of the battery body.

[0028] The present invention provides a quickly assembled drone power supply and an installation method thereof. Through the provided driving component and the first positioning component, when the card block pops into the card slot, the rack at one end of the bent rod will also move into the shell body together. In the process of the rack being inserted into the shell body, the first gear meshed with the rack will be driven to rotate. The rotation of the first gear can drive the second rotating column to rotate. In the process of the second rotating column rotating, the third gear can be driven to rotate. The third gear can drive the second gear meshed with the rack to rotate together. At the same time, the second gear and the gear fan are also meshed with each other, so that the gear fan and the first gear rotate clockwise together. When the gear fan rotates clockwise, the movable plate can be rotated clockwise to a certain angle and inserted into the first rectangular groove and the second rectangular groove. By inserting the movable plates distributed at equal distances into the first rectangular groove and the second rectangular groove, the shell can be reinforced and locked, which further improves the overall stability of the battery body after installation and avoids the shell from loosening or even falling off when the drone body takes off later.

[0029] The present invention provides a quickly assembled drone power supply and an installation method thereof. Through the first positioning component, side panels, air inlet slots and air guide covers, a heat dissipation channel is formed with the two sets of side panels at the bottom of the battery compartment after the movable panel is opened. The heat dissipation channel can quickly introduce the airflow during the flight of the drone body into the battery compartment and the shell, thereby accelerating the rapid heat dissipation of the battery body inside the shell, ensuring that the battery body can always be in a suitable working temperature environment. At the same time, through the air inlet slots and air guide covers opened on one side of the side panels, the airflow in multiple directions during the flight of the drone body can be guided and collected, thereby achieving a good heat dissipation effect for the drone when performing flight missions in different directions, avoiding the occurrence of severe heating of the battery body when powered for a long time. BRIEF DESCRIPTION OF THE DRAWINGS

[0030] In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings required for use in the embodiments will be briefly introduced below. Obviously, the drawings described below are only some embodiments of the present invention. For ordinary technicians in this field, other drawings can be obtained based on these drawings without paying creative work.

[0031] Figure 1 This is a schematic diagram of the overall upward structure of the drone body after the power supply of the present invention is assembled.

[0032] Figure 2 This is a schematic diagram of the overall top view of the UAV body after the power supply of the present invention is assembled.

[0033] Figure 3 It is a schematic diagram of the overall front structure of the power supply of the present invention.

[0034] Figure 4 It is a schematic diagram of the overall inverted structure of the power supply of the present invention.

[0035] Figure 5 For the present invention Figure 4 Schematic diagram of the enlarged structure at point A in the middle.

[0036] Figure 6 It is a schematic diagram of the shell disassembly structure of the present invention.

[0037] Figure 7 For the present invention Figure 6 Schematic diagram of the enlarged structure at point B in the middle.

[0038] Figure 8 It is a schematic diagram of the disassembled structure of the shell and the battery body of the present invention.

[0039] Fig. 9 It is a schematic diagram of the overall structure of the drive assembly of the present invention.

[0040] Fig.10 For the present invention Fig. 9 Schematic diagram of the enlarged structure at point C in the middle.

[0041] Fig.11 It is a schematic cross-sectional structure diagram of the overall power supply of the present invention.

[0042] Fig.12 It is a schematic diagram of the half-section planar structure of the rack of the present invention.

[0043] Fig.13 For the present invention Fig.12 Schematic diagram of the enlarged structure at D in the middle.

[0044] In the figure:

[0045] 1. UAV body; 2. Battery compartment; 3. Shell; 4. First positioning assembly; 4001. First rectangular groove; 4002. Movable plate; 4003. Side plate; 4004. Air inlet groove; 4005. Air guide cover; 4006. Air guide plate; 4007. Casing; 4008. First rotating column; 4009. First spring; 4010. Second rectangular groove; 4011. Baffle; 5. Second positioning assembly; 5001. Guide column; 5002. Baffle frame; 5003. Second spring; 5004. Bending rod; 5005. Movable column; 5006, through slot; 5007, push rod; 5008, third spring; 5009, block; 5010, slot; 6, first ventilation hole; 7, connecting plate; 8, slot; 9, second ventilation hole; 10, terminal; 11, driving assembly; 1101, first gear; 1102, second rotating column; 1103, second gear; 1104, gear fan; 1105, third rotating column; 1106, third gear; 1107, fixing seat; 1108, rack; 12, battery body; 13, reinforcing frame. DETAILED DESCRIPTION

[0046] The technical solution of this patent is further described in detail below in conjunction with specific implementation methods.

[0047] The embodiments of the present invention are described in detail below, and examples of the embodiments are shown in the accompanying drawings, wherein the same or similar reference numerals throughout represent the same or similar elements or elements having the same or similar functions. The embodiments described below with reference to the accompanying drawings are exemplary and are only used to explain the present invention, and cannot be understood as limiting the present invention.

[0048] In the description of this patent, it should be understood that the terms "center", "up", "down", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inside", "outside", etc., indicating the orientation or position relationship, are based on the orientation or position relationship shown in the drawings, and are only for the convenience of describing this patent and simplifying the description, rather than indicating or implying that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore cannot be understood as a limitation on this patent.

[0049] In the description of this patent, it should be noted that, unless otherwise clearly specified and limited, the terms "installed", "connected", "connected", and "set" should be understood in a broad sense, for example, it can be fixedly connected or set, or it can be detachably connected or set, or connected or set in one piece. For ordinary technicians in this field, the specific meanings of the above terms in this patent can be understood according to specific circumstances.

[0050] See also Figure 1-Figure 13A rapidly assembled drone power source includes a battery compartment 2, which is fixedly connected to the bottom outer wall of a drone body 1, a housing 3 is inserted into the battery compartment 2, a battery body 12 is fixedly connected to the inside of the housing 3, and one end of a terminal 10 is inserted into the inside of the housing 3.

[0051] A first positioning assembly 4 for fixing the housing 3 is provided at the bottom of the battery compartment 2;

[0052] A second positioning assembly 5 for locking the housing 3 is provided inside the battery compartment 2;

[0053] A driving assembly 11 is disposed inside the housing 3;

[0054] The second positioning assembly 5 includes a guide column 5001 and a second spring 5003 fixedly connected to the inner wall of one side of the battery compartment 2, the circumferential outer wall of the guide column 5001 is sleeved with a baffle frame 5002, a push rod 5007 is fixedly connected to the top outer wall of the shell 3, one side outer wall of the push rod 5007 is in contact with one side outer wall of the baffle frame 5002, both sides of the inner walls of the battery compartment 2 are fixedly connected to the third spring 5008, one end of the third spring 5008 is fixedly connected to a clamping block 5009, both sides of the outer walls of the shell 3 are provided with a clamping groove 5010, and the clamping block One end of 5009 passes through the inside of the card slot 5010, and a movable column 5005 is fixedly connected to the outer wall of one side of the card block 5009. The end of the movable column 5005 away from the card block 5009 extends to the outside of the battery compartment 2. The end of the movable column 5005 extending to the outside of the battery compartment 2 is fixedly connected to the bent rod 5004. The outer walls of both sides of the battery compartment 2 are provided with through grooves 5006. The end of the bent rod 5004 away from the movable column 5005 passes through the inside of the through groove 5006. When the power supply needs to be installed, one end of the shell 3 can be first installed. Insert the battery compartment 2 into the slot 8 at the end until the push rod 5007 at the top of the shell 3 contacts the baffle 5002. At this time, the outer walls of one side of the two sets of card blocks 5009 inside the battery compartment 2 are in conflict with the outer wall of one side of the baffle 5002, and the third spring 5008 is in a compressed state. When the shell 3 continues to be pushed in, the push rod 5007 pushes the baffle 5002 to move in the direction close to the terminal 10 until the card block 5009 is completely unobstructed by the baffle 5002. At this time, the card block 5009 is elastically supported by the third spring 5008. It abuts against the outer wall of one side of the shell 3. When the battery body 12 inside the shell 3 is completely matched with the wiring terminal 10, the slots 5010 on both sides of the shell 3 just match with the blocks 5009. At this time, the blocks 5009 are instantly bounced into the slots 5010 by the elastic force of the third spring 5008, thereby locking and fixing the two sides of the shell 3. During the entire installation process, people only need to complete the action of inserting the shell 3 into the battery compartment 2, thereby realizing the rapid installation of the battery body 12 and improving people's installation efficiency of the battery body 12.

[0055] Preferably, the driving assembly 11 includes a rack 1108 fixedly connected to one end of the bent rod 5004, the rack 1108 is meshed with a first gear 1101, the circumferential inner wall of the first gear 1101 is fixedly connected to a second rotating column 1102, both ends of the second rotating column 1102 are rotatably connected to the inner walls of both sides of the shell 3, the circumferential outer wall of the second rotating column 1102 is fixedly connected to a third gear 1106, the third gear 1106 is meshed with a second gear 1103, the circumferential inner wall of the second gear 1103 is fixedly connected to a third rotating column 1105, the circumferential outer wall of the second gear 1103 is meshed with a gear fan 1104, the inner wall of one side of the shell 3 is fixedly connected to a fixed seat 1107, the second rotating column 1102 and the third rotating column 1105 are both rotatably connected to the fixed seat 1107 Then, when the block 5009 pops into the slot 5010, the rack 1108 at one end of the bent rod 5004 will also move into the shell 3. In the process of the rack 1108 being inserted into the shell 3, it will drive the first gear 1101 meshing with it to rotate. The rotation of the first gear 1101 can drive the second rotating column 1102 to rotate. In the process of the second rotating column 1102 rotating, the third gear 1106 can be driven to rotate. The third gear 1106 can drive the second gear 1103 meshing with it to rotate together. At the same time, the second gear 1103 and the gear fan 1104 are also meshed with each other, so that the gear fan 1104 and the first gear 1101 rotate clockwise together, which can provide a power source for the subsequent operation of the first positioning component 4.

[0056] Preferably, both side outer walls of the battery compartment 2 are provided with first ventilation holes 6 distributed at equal distances, and both side outer walls of the shell 3 are provided with second ventilation holes 9 distributed at equal distances, which can ensure the rapid flow of air inside the battery compartment 2 and the shell 3 and accelerate the heat dissipation of the battery body 12.

[0057] Preferably, the first positioning assembly 4 includes a second rectangular groove 4010 provided on the inner wall of the bottom of the shell 3 and a first rectangular groove 4001 provided on the inner wall of the bottom of the battery compartment 2, the specifications of the first rectangular groove 4001 are the same as those of the second rectangular groove 4010, the first rectangular groove 4001 is connected to the second rectangular groove 4010, both sides of the inner wall of the second rectangular groove 4010 are rotatably connected with the first rotating column 4008, the circumferential outer wall of the first rotating column 4008 is fixedly connected with sleeves 4007 distributed at equal distances, the circumferential outer wall of the sleeve 4007 is fixedly connected with the movable plate 4002, and the movable plate 4002 The end away from the sleeve 4007 passes through the first rectangular groove 4001 and the second rectangular groove 4010. When the gear fan 1104 rotates clockwise, the movable plate 4002 can be rotated clockwise to a certain angle and inserted into the first rectangular groove 4001 and the second rectangular groove 4010. By equidistantly distributed movable plates 4002 are inserted into the first rectangular groove 4001 and the second rectangular groove 4010, the shell 3 can be reinforced and locked, which further improves the overall stability of the battery body 12 after installation, and avoids the shell 3 from loosening or even falling off when the drone body 1 takes off later.

[0058] Preferably, one outer wall of the two sets of movable plates 4002 is fixedly connected with a first spring 4009, and one end of the first spring 4009 away from the movable plate 4002 is fixedly connected to the inner wall of one side of the shell 3, which can achieve the auxiliary reset effect of the movable plate 4002 after the shell 3 is disassembled.

[0059] Preferably, the bottom outer wall of the battery compartment 2 is fixedly connected with a side panel 4003, and the movable panel 4002 is located in the middle of the two groups of side panels 4003. The two groups of side panels 4003 and the movable panel 4002 form a heat dissipation channel. When the movable panel 4002 is opened, a heat dissipation channel is formed with the two groups of side panels 4003 at the bottom of the battery compartment 2. The heat dissipation channel can quickly introduce the airflow during the flight of the drone body 1 into the battery compartment 2 and the shell 3, thereby accelerating the rapid heat dissipation of the battery body 12 inside the shell 3, ensuring that the battery body 12 can always be in a suitable working temperature environment.

[0060] Preferably, one side outer wall of the two groups of side panels 4003 is provided with an air inlet groove 4004, and the one side outer wall of the two groups of side panels 4003 close to the movable plate 4002 is fixedly connected with an air guide cover 4005, one end of the air guide cover 4005 is fixedly connected with a guide plate 4006, the cross-section of the guide plate 4006 is wavy, and the air inlet groove 4004 is connected with the air guide cover 4005. The air inlet groove 4004 and the air guide cover 4005 provided on one side of the side panel 4003 can guide and collect airflows in multiple directions when the drone body 1 is flying, thereby achieving a good heat dissipation effect when the drone performs flight missions in different directions, avoiding the occurrence of severe heating of the battery body 12 when powered for a long time.

[0061] Preferably, a baffle 4011 is fixedly connected to an inner wall of one side of the second rectangular groove 4010, and the battery body 12 is fixedly connected to an inner wall of one side of the shell 3 through a reinforcing frame 13, thereby ensuring the stability of the battery body 12 inside the shell 3. A slot 8 is opened on one side of the battery compartment 2, and one end of the shell 3 passes through the inside of the slot 8, and a connecting plate 7 is fixedly connected to an outer wall of one side of the shell 3.

[0062] A method for installing a drone power supply, which uses a drone power supply that can be quickly assembled in the above embodiment, includes the following steps:

[0063] Step 1: Insert one end of the housing 3 into the slot 8 at the end of the battery compartment 2 until the battery body 12 is fully matched with the terminal 10;

[0064] Step 2: The clamping block 5009 is clamped in the clamping grooves 5010 on both sides of the housing 3 by the pressure of the third spring 5008 to lock the housing 3;

[0065] Step 3: When the driving assembly 11 is working, the multiple groups of movable plates 4002 in the first positioning assembly 4 are inserted into the first rectangular groove 4001 and the second rectangular groove 4010, completing the secondary fixing and locking of the housing 3;

[0066] Step 4: Pull the bent rods 5004 on both sides to disengage the block 5009 from the slot 5010 , and then pull the shell 3 out of the battery compartment 2 to complete the disassembly of the shell 3 and the battery body 12 .

[0067] In summary, with the aid of the above technical solution of the present invention, when the power supply needs to be installed, one end of the shell 3 can be first inserted into the slot 8 at the end of the battery compartment 2 until the push rod 5007 at the top of the shell 3 contacts the baffle 5002. At this time, the outer walls of one side of the two groups of blocks 5009 inside the battery compartment 2 are in conflict with the outer walls of one side of the baffle 5002, and the third spring 5008 is in a compressed state. When the shell 3 continues to be pushed in, the push rod 5007 pushes the baffle 5002 to move in the direction close to the wiring terminal 10 until the block 5009 is completely unobstructed by the baffle 5002. At this time, the block 5009 is in conflict with the outer wall of one side of the shell 3 through the elastic force of the third spring 5008. When the battery body 12 inside the shell 3 is When it is fully matched with the wiring terminal 10, the slots 5010 on both sides of the shell 3 just match with the block 5009. At this time, the block 5009 is instantly ejected into the slot 5010 by the elastic force of the third spring 5008, thereby realizing the locking and fixation of the two sides of the shell 3. During the entire installation process, people only need to complete an action of inserting the shell 3 into the battery compartment 2, thereby realizing the rapid installation of the battery body 12 and improving people's installation efficiency of the battery body 12. At the same time, when the block 5009 is ejected into the slot 5010, the rack 1108 at one end of the bent rod 5004 will also move into the shell 3 together. When the rack 1108 is inserted into the shell 3, it will drive the first gear 1101 meshing with it to rotate. The rotation of the first gear 1101 can drive the second rotating column 1102 to rotate. During the rotation of the second rotating column 1102, the third gear 1106 can be driven to rotate. The third gear 1106 can drive the second gear 1103 meshing with it to rotate together. At the same time, the second gear 1103 and the gear fan 1104 are also meshed with each other, so that the gear fan 1104 and the first gear 1101 rotate clockwise together. When the gear fan 1104 rotates clockwise, the movable plate 4002 can be rotated clockwise to a certain angle and inserted into the first rectangular groove 4001 and the second rectangular groove 4010. The movable plates 4002 distributed at equal distances are all inserted into the first rectangular groove 4001 and the second rectangular groove 4010. The shell 3 is reinforced and locked, which further improves the overall stability of the battery body 12 after installation, and avoids the shell 3 from loosening or even falling off when the drone body 1 takes off later. At the same time, after the movable plate 4002 is opened, it will form a heat dissipation channel with the two sets of side panels 4003 at the bottom of the battery compartment 2. The heat dissipation channel can quickly introduce the airflow during the flight of the drone body 1 into the battery compartment 2 and the shell 3, thereby accelerating the rapid heat dissipation of the battery body 12 inside the shell 3, ensuring that the battery body 12 can always be in a suitable working temperature environment. At the same time, the air inlet slot 4004 and the wind guide cover 4005 on one side of the side panel 4003 can guide and collect the airflow in multiple directions when the drone body 1 is flying.This achieves good heat dissipation when the drone is performing flight missions in different directions, and avoids the battery body 12 from overheating when it is powered for a long time.

[0068] The above description is only a preferred embodiment of the present invention and is not intended to limit the present invention. Any modifications, equivalent substitutions, improvements, etc. made within the spirit and principle of the present invention should be included in the protection scope of the present invention.

Claims

1. A rapidly assembled drone power source, comprising a battery compartment (2), characterized in that: The battery compartment (2) is fixedly connected to the bottom outer wall of the drone body (1); a housing (3) is inserted into the interior of the battery compartment (2); a battery body (12) is fixedly connected to the interior of the housing (3); one end of the connection terminal (10) is inserted into the interior of the housing (3); A first positioning assembly (4) for fixing the housing (3) is provided at the bottom of the battery compartment (2); A second positioning assembly (5) for locking the housing (3) is arranged inside the battery compartment (2); A driving assembly (11) is arranged inside the housing (3); The second positioning assembly (5) comprises a guide column (5001) and a second spring (5003) fixedly connected to the inner wall of one side of the battery compartment (2); the circumferential outer wall of the guide column (5001) is sleeved with a baffle frame (5002); the top outer wall of the shell (3) is fixedly connected to a push rod (5007); the outer wall of one side of the push rod (5007) is in contact with the outer wall of one side of the baffle frame (5002); the inner walls of both sides of the battery compartment (2) are fixedly connected to a third spring (5008); one end of the third spring (5008) is fixedly connected to a clamping block (5009); and the outer walls of both sides of the shell (3) are provided with clamping grooves. (5010), one end of the card block (5009) passes through the interior of the card slot (5010), one side outer wall of the card block (5009) is fixedly connected to a movable column (5005), one end of the movable column (5005) away from the card block (5009) extends to the outside of the battery compartment (2), one end of the movable column (5005) extending to the outside of the battery compartment (2) is fixedly connected to a bent rod (5004), both side outer walls of the battery compartment (2) are provided with through grooves (5006), and one end of the bent rod (5004) away from the movable column (5005) passes through the interior of the through groove (5006).

2. A rapidly assembled drone power supply according to claim 1, characterized in that: The driving assembly (11) comprises a rack (1108) fixedly connected to one end of the bent rod (5004), the rack (1108) meshing with a first gear (1101), a second rotating column (1102) fixedly connected to the circumferential inner wall of the first gear (1101), two ends of the second rotating column (1102) rotatably connected to the inner walls of both sides of the housing (3), and a third gear (1106) fixedly connected to the circumferential outer wall of the second rotating column (1102). ), the third gear (1106) is meshed with the second gear (1103), the circumferential inner wall of the second gear (1103) is fixedly connected with the third rotating column (1105), the circumferential outer wall of the second gear (1103) is meshed with a toothed fan (1104), the inner wall of one side of the shell (3) is fixedly connected with a fixed seat (1107), and the second rotating column (1102) and the third rotating column (1105) are both rotatably connected to the fixed seat (1107).

3. The rapidly assembled drone power supply according to claim 2, characterized in that: The outer walls on both sides of the battery compartment (2) are provided with first ventilation holes (6) distributed at equal distances, and the outer walls on both sides of the shell (3) are provided with second ventilation holes (9) distributed at equal distances.

4. The rapidly assembled UAV power supply according to claim 3, characterized in that: The first positioning assembly (4) comprises a second rectangular groove (4010) provided on the bottom inner wall of the shell (3) and a first rectangular groove (4001) provided on the bottom inner wall of the battery compartment (2); the specifications of the first rectangular groove (4001) are the same as those of the second rectangular groove (4010); the first rectangular groove (4001) is connected to the second rectangular groove (4010); the inner walls on both sides of the second rectangular groove (4010) are rotatably connected to first rotating columns (4008); the circumferential outer wall of the first rotating column (4008) is fixedly connected to sleeves (4007) distributed at equal distances; the circumferential outer wall of the sleeve (4007) is fixedly connected to a movable plate (4002); the end of the movable plate (4002) away from the sleeve (4007) passes through the inside of the first rectangular groove (4001) and the second rectangular groove (4010).

5. The rapidly assembled drone power supply according to claim 4, characterized in that: One side outer wall of the two groups of movable plates (4002) is fixedly connected with a first spring (4009), and one end of the first spring (4009) away from the movable plate (4002) is fixedly connected to one side inner wall of the shell (3).

6. The rapidly assembled drone power supply according to claim 5, characterized in that: The bottom outer wall of the battery compartment (2) is fixedly connected with a side panel (4003), the movable panel (4002) is located in the middle of the two groups of side panels (4003), and the two groups of side panels (4003) and the movable panel (4002) form a heat dissipation channel.

7. The rapidly assembled drone power supply according to claim 6, characterized in that: An air inlet groove (4004) is provided on one side outer wall of the two groups of side panels (4003); an air guide cover (4005) is fixedly connected to the one side outer wall of the two groups of side panels (4003) close to the movable plate (4002); one end of the air guide cover (4005) is fixedly connected to a guide plate (4006); the cross section of the guide plate (4006) is wavy; and the air inlet groove (4004) is connected to the air guide cover (4005).

8. The rapidly assembled drone power supply according to claim 7, characterized in that: A baffle (4011) is fixedly connected to an inner wall on one side of the second rectangular groove (4010), and the battery body (12) is fixedly connected to an inner wall on one side of the housing (3) via a reinforcing frame (13).

9. The rapidly assembled drone power supply according to claim 7, characterized in that: A slot (8) is provided on one side of the battery compartment (2), one end of the shell (3) passes through the inside of the slot (8), and a connecting plate (7) is fixedly connected to an outer wall of one side of the shell (3).

10. A method for installing a drone power supply, which uses a drone power supply that can be quickly assembled as described in 1-9, characterized in that: The following steps are involved: S1: inserting one end of the housing (3) into the slot (8) at the end of the battery compartment (2) until the battery body (12) and the connection terminal (10) are fully matched; S2: The clamping block (5009) is clamped in the clamping grooves (5010) on both sides of the housing (3) by the pressure of the third spring (5008), thereby locking the housing (3); S3: When the driving assembly (11) is working, the multiple groups of movable plates (4002) in the first positioning assembly (4) are inserted into the first rectangular groove (4001) and the second rectangular groove (4010), completing the secondary fixing and locking of the housing (3); S4: Pull the bent rods (5004) on both sides to disengage the clamping block (5009) from the clamping slot (5010), and then pull the shell (3) out of the battery compartment (2), thereby completing the disassembly of the shell (3) and the battery body (12).

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