Unmanned aerial vehicle with unhooking release device
By designing a decoupling mechanism including the first drive motor, suspension member, rotating block, limit block, guide rod, guide block, spring, second drive motor, support member and fixed assembly on the drone, the problem of existing drones being prone to misrelease or early release of load objects during use is solved, and more stable connections and higher load-bearing capacity are achieved.
Patent Information
- Application Number
- CN202510445721.1
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Filing Date
- 2025-04-10
- Publication Date
- 2025-06-27
AI Technical Summary
When used, existing drones with decoupling release devices are complex in design and are prone to problems of accidentally releasing or early release of load objects.
A drone including a drone body and a removable decoupling mechanism is designed. The first drive motor, a suspension member and a rotating block are used to transport the material box with a connecting belt; at the same time, the limit block, a guide rod, a guide block and a spring are used to improve the connection stability between the suspension member and the connecting belt, and the second drive motor and a support member are used to improve the load-bearing capacity of the suspension member, and the disassembly and maintenance of the support member is achieved through a fixed assembly.
Improves the connection stability between the suspension and the connecting belt, enhances the load-bearing capacity of the suspension, and simplifies the removal and maintenance of the support, reducing the risk of accidentally releasing or early release of load objects.
Smart Images

Figure CN120207592A_ABST
Abstract
Description
Technical Field
[0001] The present invention relates to the technical field of unmanned aerial vehicle decoupling and release, and particularly to an unmanned aerial vehicle with a decoupling and release device. Background Art
[0002] An unmanned aerial vehicle refers to an aircraft that does not require a pilot on board. It performs flight missions through pre-set programs, remote control, or autonomous flight technology. Unmanned aerial vehicles are widely used in military reconnaissance, civilian aerial photography, agricultural plant protection, disaster survey, express delivery, and other fields, and have the advantages of high efficiency, flexibility, and low cost.
[0003] Sometimes, unmanned aerial vehicles are used for transporting items. When transporting items to the destination, it is necessary to release the transported items to the ground. Therefore, an unmanned aerial vehicle with a decoupling and release device is needed.
[0004] Existing unmanned aerial vehicles with decoupling and release devices have certain drawbacks when in use. When existing unmanned aerial vehicles with decoupling and release devices are in use, the design complexity of the decoupling and release device is relatively high. If the user operates improperly or there are faults in the device itself, it may lead to accidental release or premature release of the load object, thus causing negative consequences.
[0005] Therefore, an unmanned aerial vehicle with a decoupling and release device is proposed. Summary of the Invention
[0006] (I) Technical Problems to be Solved Aiming at the deficiencies of the prior art, the present invention provides an unmanned aerial vehicle with a decoupling and release device, which can solve the technical problems raised in the background art.
[0007] (II) Technical Solutions The present invention is implemented by the following technical solutions: An unmanned aerial vehicle with a decoupling release device, comprising an unmanned aerial vehicle main body and a decoupling mechanism detachably arranged on the unmanned aerial vehicle main body; wherein, the unmanned aerial vehicle main body transports a material box through the decoupling mechanism, connection belts are symmetrically installed on the material box, and the material box is connected to the unmanned aerial vehicle main body through the connection belts; the decoupling mechanism includes a decoupling seat detachably installed on the bottom end face of the unmanned aerial vehicle main body, several groups of suspension members symmetrically installed inside the decoupling seat and used for suspending the connection belts, and a first driving motor detachably installed outside the decoupling seat and used for controlling the rotation of the suspension members. The first driving motor and several groups of suspension members cooperate to be able to hang up the connection belts, so as to be able to transport the material box; the decoupling mechanism further includes a guide rod vertically arranged inside the decoupling seat, a guide block movably arranged on the guide rod, a spring connected to the guide block, and a limiting block arranged above the suspension member and detachably connected to the guide block. The guide block moves on the guide rod, and the spring can stretch the guide block, so that the limiting block fits with the suspension member; the decoupling mechanism further includes a second driving motor detachably arranged inside the decoupling seat, a support member detachably connected to the output shaft of the second driving motor, and a fixing component for fixedly connecting the support member and the second driving motor. The second driving motor can control the rotation of the support member, so that the support member can be connected to the suspension member; a support groove matching the suspension member is formed on the support member, and the second driving motor controls the rotation of the support member to support or separate the suspension member.
[0008] Preferably, several groups of first grooves matching the guide rod are formed inside the decoupling seat. Both the upper and lower end faces of the guide block are connected to a spring sleeved on the guide rod. Several groups of strengthening blocks connected to the guide block are arranged on one side face of the limiting block, and the limiting block drives the guide block to move on the guide rod through the strengthening blocks.
[0009] Preferably, an installation frame with a "U" - shaped structure is detachably arranged on the inner top surface of the decoupling seat, and the second driving motor is detachably arranged inside the installation frame.
[0010] Preferably, the fixing component includes a first fixing seat rotatably arranged on the bottom end face of the installation frame, a first fixing member detachably connected to the first fixing seat, and a reinforcing block fixedly arranged at the bottom end of the first fixing member. A first fixing groove matching the first fixing member is formed on the first fixing seat. A clamping block perpendicular to the first fixing groove is arranged in the first fixing groove, a clamping groove for clamping with the clamping block is formed on the first fixing member, a reinforcing groove matching the reinforcing block is formed on the first fixing seat, the reinforcing groove communicates with the first fixing groove, and the reinforcing block has a "T" - shaped structure.
[0011] Preferably, the first fixing member includes a first fixing block clamped with the clamping block and a first connecting block arranged at the bottom end of the first fixing block. The two side edges at the upper end of the first fixing block are arc - shaped surfaces.
[0012] Preferably, the fixing component further includes a second fixing member vertically disposed on the bottom end surface of the reinforcing block, a second fixing seat mounted on the support member, and a fixing rod detachably connecting the second fixing member and the second fixing seat. A second groove matching the second fixing seat is formed on the support member, a second fixing groove matching the second fixing member is formed on the second fixing seat, and a fixing hole connected to the fixing rod is formed on the second fixing member.
[0013] Preferably, a plurality of groups of rotating grooves matching the suspension members are formed on the inner side wall of the hook release seat. A rotating block detachably connected to the suspension member is rotatably disposed in the rotating groove. A rotating rod is vertically mounted between the two rotating blocks. The output shaft of the first driving motor penetrates through one side surface of the hook release seat and is detachably connected to the rotating shaft of the rotating block. The first driving motor drives the two rotating blocks to rotate through the rotating rod.
[0014] Preferably, one end of the rotating block is vertically provided with a mounting block. A mounting groove matching the mounting block is formed on one end surface of the suspension member. A rotating hole corresponding to the rotating rod is formed on the hook release seat. The rotating block can be disassembled and replaced through the mounting block.
[0015] Preferably, an arc-shaped suspension groove is formed on the suspension member. An anti-sliding block matching the connecting belt is provided on the bottom end surface of the limiting block. The anti-sliding block can improve the connection stability between the connecting belt and the suspension member.
[0016] Preferably, a plurality of groups of support feet with adjustable heights are detachably mounted on the bottom end surface of the hook release seat.
[0017] (III) Beneficial Effects Compared with the prior art, the present invention provides a drone with a hook release device, having the following beneficial effects: For the drone with a hook release device, through the hook release mechanism on the drone body, the first driving motor, the suspension member and the rotating block cooperate to transport the transportation material box through the connecting belt. The limiting block, the guiding rod, the guiding block and the spring cooperate to improve the connection stability between the suspension member and the connecting belt. The second driving motor and the support member cooperate to improve the bearing capacity of the suspension member. Through the provided first fixing seat, second fixing seat, first fixing member and second fixing member, the support member can be disassembled and maintained. BRIEF DESCRIPTION OF THE DRAWINGS
[0018] Figure 1 It is the overall structure diagram of the present invention.
[0019] Figure 2 In the present invention Figure 1 The enlarged view of part A.
[0020] Figure 3 This is a partial structure diagram of the guide block and the limit block in the present invention.
[0021] Figure 4 This is a partial structure diagram of the support member and the fixing component in the present invention.
[0022] Figure 5 This is a partial structure diagram of the first fixing member and the second fixing member in the present invention.
[0023] Figure 6 This is a partial structure diagram of the suspension member and the rotating block in the present invention.
[0024] In the figure: 1, UAV main body; 2, support feet; 3, transport material box; 4, connecting belt; 5, hook release seat; 6, suspension member; 7, first drive motor; 8, guide rod; 9, guide block; 10, spring; 11, limit block; 12, second drive motor; 13, support member; 14, support groove; 15, strengthening block; 16, mounting frame; 17, first fixing seat; 18, first fixing member; 19, reinforcing block; 20, clamping block; 21, first fixing block; 22, first connecting block; 23, second fixing member; 24, second fixing seat; 25, fixing rod; 26, rotating block; 27, rotating rod; 28, mounting block; 29, anti-slip block. Specific Embodiments
[0025] Next, in combination with the accompanying drawings and specific embodiments, the present invention will be further described. It should be noted that, on the premise of no conflict, the following-described embodiments or technical features can be arbitrarily combined to form new embodiments.
[0026] Embodiment 1: Please refer to Figures 1-6, a drone with a decoupling and release device in this embodiment, includes a drone main body 1 and a decoupling mechanism detachably arranged on the drone main body 1; wherein, the drone main body 1 transports a material box 3 through the decoupling mechanism, connection belts 4 are symmetrically installed on the material box 3, and the material box 3 is connected to the drone main body 1 through the connection belts 4; the decoupling mechanism includes a decoupling seat 5 detachably installed on the bottom end surface of the drone main body 1, several groups of suspension members 6 symmetrically installed inside the decoupling seat 5 and used for hanging the connection belts 4, and a first driving motor 7 detachably installed outside the decoupling seat 5 and used for controlling the rotation of the suspension members 6. The first driving motor 7 and several groups of suspension members 6 cooperate to hang the connection belts 4, so as to transport the material box 3; the decoupling mechanism further includes a guide rod 8 vertically arranged inside the decoupling seat 5, a guide block 9 movably arranged on the guide rod 8, a spring 10 connected to the guide block 9, and a limit block 11 arranged above the suspension member 6 and detachably connected to the guide block 9. The guide block 9 moves on the guide rod 8, and the spring 10 can stretch and contract the guide block 9, so that the limit block 11 fits with the suspension member 6; the decoupling mechanism further includes a second driving motor 12 detachably arranged inside the decoupling seat 5, a support member 13 detachably connected to the output shaft of the second driving motor 12, and a fixing component for fixedly connecting the support member 13 and the second driving motor 12. The second driving motor 12 can control the rotation of the support member 13, so that the support member 13 can be connected to the suspension member 6; a support groove 14 matching the suspension member 6 is formed on the support member 13. The second driving motor 12 controls the rotation of the support member 13 to support or separate the suspension member 6. Start the first driving motor 7 to drive the suspension member 6 to rotate, place the connection belt 4 on the suspension member 6, so that the limit block 11 drives the guide block 9 to move on the guide rod 8, and then the limit block 11 limits the connection belt 4. Start the second driving motor 12 to drive the support member 13 to rotate to the position of the suspension member 6, so that the suspension member 6 is connected to the support groove 14, and the support member 13 supports the suspension member 6.
[0027] Several groups of first grooves matching the guide rod 8 are formed inside the decoupling seat 5. Both the upper and lower end surfaces of the guide block 9 are connected to the spring 10 sleeved on the guide rod 8. Several groups of strengthening blocks 15 connected to the guide block 9 are arranged on one side surface of the limit block 11. The limit block 11 drives the guide block 9 to move on the guide rod 8 through the strengthening blocks 15. Move the limit block 11 to drive the strengthening blocks 15 to move, and the strengthening blocks 15 drive the guide block 9 to move on the guide rod 8, so that the guide block 9 drives the spring 10 to stretch and contract.
[0028] An installation frame 16 with a "U" - shaped structure is detachably arranged on the inner top surface of the decoupling seat 5, and the second driving motor 12 is detachably arranged inside the installation frame 16.
[0029] The fixing assembly includes a first fixing seat 17 rotatably arranged on the bottom end surface of the mounting frame 16, a first fixing member 18 detachably connected to the first fixing seat 17, and a reinforcing block 19 fixedly arranged at the bottom end of the first fixing member 18. A first fixing groove matching the first fixing member 18 is formed on the first fixing seat 17. A clamping block 20 clamped with the first fixing member 18 is vertically arranged in the first fixing groove. A clamping groove engaged with the clamping block 20 is formed on the first fixing member 18. A reinforcing groove matching the reinforcing block 19 is formed on the first fixing seat 17. The reinforcing groove is communicated with the first fixing groove. The reinforcing block 19 is in a "T" - shaped structure. Move the first fixing member 18 to remove the first fixing member 18 from the first fixing groove and remove the clamping block 20 from the clamping groove to disassemble and maintain the first fixing member 18. Start the second driving motor 12. When the second driving motor 12 rotates forward, drive the first fixing seat 17 to rotate. The first fixing seat 17 drives the reinforcing block 19 to rotate through the first fixing member 18, and the reinforcing block 19 drives the support member 13 to rotate, so that the support member 13 approaches the suspension member 6 and connects the suspension member 6 to the support groove 14 to support the suspension member 6. When the second driving motor 12 rotates in reverse, the support member 13 moves away from the suspension member 6, and the suspension member 6 is removed from the support groove 14, facilitating the suspension member 6 to release the connecting belt 4.
[0030] The first fixing member 18 includes a first fixing block 21 clamped with the clamping block 20 and a first connecting block 22 arranged at the bottom end of the first fixing block 21. The two side edges at the upper end of the first fixing block 21 are arc - shaped surfaces.
[0031] The fixing assembly further includes a second fixing member 23 vertically arranged on the bottom end surface of the reinforcing block 19, a second fixing seat 24 installed on the support member 13, and a fixing rod 25 detachably connecting the second fixing member 23 and the second fixing seat 24. A second groove matching the second fixing seat 24 is formed on the support member 13. A second fixing groove matching the second fixing member 23 is formed on the second fixing seat 24. A fixing hole connected to the fixing rod 25 is formed on the second fixing member 23. The reinforcing block 19 drives the second fixing member 23 to rotate. The second fixing member 23 drives the support member 13 to rotate through the second fixing seat 24. Disassemble the fixing rod 25 from the fixing hole and disassemble the second fixing member 23 from the second fixing groove, so that the second fixing member 23 is disassembled and separated from the second fixing seat 24, and the support member 13 is disassembled and separated from the second fixing member 23.
[0032] On the inner side wall of the decoupling seat 5, several groups of rotating grooves matching the suspension member 6 are provided. In the rotating grooves, a rotating block 26 detachably connected to the suspension member 6 is rotatably arranged. A rotating rod 27 is vertically installed between two groups of rotating blocks 26. The output shaft of the first driving motor 7 penetrates through one side surface of the decoupling seat 5 and is detachably connected to the rotating shaft of the rotating block 26. The first driving motor 7 drives the two groups of rotating blocks 26 to rotate through the rotating rod 27. When the first driving motor 7 is started, the rotating block 26 is driven to rotate. The rotating block 26 drives the other rotating block 26 to rotate through the rotating rod 27. The rotating block 26 drives the suspension member 6 to rotate. When the first driving motor 7 rotates forward, the suspension member 6 rotates upward, and the connecting belt 4 can be suspended. When the first driving motor 7 rotates in reverse, the suspension member 6 rotates downward, and the connecting belt 4 can be decoupled and released.
[0033] One end of the rotating block 26 is vertically provided with a mounting block 28. On one end face of the suspension member 6, a mounting groove matching the mounting block 28 is provided. On the decoupling seat 5, a rotating hole corresponding to the rotating rod 27 is provided. The rotating block 26 can be disassembled and replaced through the mounting block 28. The suspension member 6 is rotated, the mounting block 28 is disassembled from the mounting groove, and the suspension member 6 is disassembled from the mounting block 28.
[0034] On the suspension member 6, a suspension groove in an arc structure is provided. On the bottom end face of the limiting block 11, an anti-sliding block 29 matching the connecting belt 4 is provided. The anti-sliding block 29 can improve the connection stability between the connecting belt 4 and the suspension member 6.
[0035] On the bottom end face of the decoupling seat 5, several groups of height-adjustable support feet 2 are detachably installed. The support feet 2 prevent the decoupling seat 5 from directly contacting the ground. For this UAV with a decoupling and release device, the first driving motor 7 is started to drive the suspension member 6 to rotate. The connecting belt 4 is placed on the suspension member 6, so that the limiting block 11 drives the guiding block 9 to move on the guiding rod 8. Then, the limiting block 11 limits the connecting belt 4. The second driving motor 12 is started to drive the supporting member 13 to rotate to the position of the suspension member 6, so that the suspension member 6 is connected to the supporting groove 14, and the supporting member 13 supports the suspension member 6; The limiting block 11 is moved to drive the strengthening block 15 to move. The strengthening block 15 drives the guiding block 9 to move on the guiding rod 8, so that the guiding block 9 drives the spring 10 to expand and contract; Start the second drive motor 12. When the second drive motor 12 rotates forward, it drives the first fixed seat 17 to rotate. The first fixed seat 17 drives the reinforcement block 19 to rotate through the first fixing member 18, and the reinforcement block 19 drives the support member 13 to rotate, so that the support member 13 approaches the suspension member 6, connects the suspension member 6 with the support groove 14, and supports the suspension member 6. When the second drive motor 12 rotates reversely, the support member 13 is separated from the suspension member 6, and the suspension member 6 is removed from the support groove 14, facilitating the suspension member 6 to release the connecting belt 4; Remove the fixing rod 25 from the fixing hole and remove the second fixing member 23 from the second fixing groove, so that the second fixing member 23 is disassembled and separated from the second fixed seat 24, and the support member 13 is disassembled and separated from the second fixing member 23; Start the first drive motor 7 to drive the rotating block 26 to rotate. The rotating block 26 drives another rotating block 26 to rotate through the rotating rod 27, and the rotating block 26 drives the suspension member 6 to rotate. When the first drive motor 7 rotates forward, the suspension member 6 rotates upward and can suspend the connecting belt 4. When the first drive motor 7 rotates reversely, the suspension member 6 rotates downward to unhook and release the connecting belt 4. For the UAV with a decoupling and releasing device, through the decoupling mechanism on the UAV main body 1 provided, the first drive motor 7, the suspension member 6 and the rotating block 26 can cooperate to transport the transportation material box 3 through the connecting belt 4. The limiting block 11, the guide rod 8, the guide block 9 and the spring 10 cooperate to improve the connection stability between the suspension member 6 and the connecting belt 4. The second drive motor 12 and the support member 13 cooperate to improve the bearing capacity of the suspension member 6. Through the provided first fixed seat 17, second fixed seat 24, first fixing member 18 and second fixing member 23, the support member 13 can be disassembled and maintained.
[0036] The above embodiments are only the preferred embodiments of the present invention and cannot be used to limit the protection scope of the present invention. Any non-substantial changes and substitutions made by those skilled in the art on the basis of the present invention belong to the protection scope required by the present invention.
Claims
1. A drone with a release device, characterized in that: include: A drone body (1) and a decoupling mechanism detachably arranged on the drone body (1); The drone body (1) transports the material box (3) through a decoupling mechanism, and the transport material box (3) is symmetrically mounted with a connecting belt (4); The decoupling mechanism comprises a decoupling seat (5) detachably mounted on the bottom end surface of the drone body (1), a plurality of groups of suspension members (6) symmetrically mounted on the inner side of the decoupling seat (5) and suspending the connecting belt (4), and a first driving motor (7) detachably mounted on the outer side of the decoupling seat (5) and controlling the suspension members (6) to rotate; The unhooking mechanism further comprises a guide rod (8) vertically arranged inside the unhooking seat (5), a guide block (9) movably arranged on the guide rod (8), a spring (10) connected to the guide block (9), and a limit block (11) arranged above the hanging member (6) and detachably connected to the guide block (9); The unhooking mechanism further comprises a second drive motor (12) detachably arranged inside the unhooking seat (5), a support member (13) detachably connected to an output shaft of the second drive motor (12), and a fixing assembly that fixes the support member (13) to the second drive motor (12); The support member (13) is provided with a support groove (14) matching the suspension member (6), and the second drive motor (12) controls the support member (13) to rotate so as to support or separate the suspension member (6).
2. The drone with a decoupling release device according to claim 1, characterized in that: The unhooking seat (5) is provided with a plurality of first grooves matching the guide rod (8) inside, the upper and lower end surfaces of the guide block (9) are connected to the spring (10) sleeved on the guide rod (8), and one side surface of the limit block (11) is provided with a plurality of reinforcing blocks (15) connected to the guide block (9).
3. The drone with a decoupling release device according to claim 1, characterized in that: A mounting frame (16) in a "U"-shaped structure is detachably provided on the inner top surface of the unhooking seat (5), and the second driving motor (12) is detachably provided on the inner side of the mounting frame (16).
4. The drone with a decoupling release device as claimed in claim 3, characterized in that: The fixing assembly comprises a first fixing seat (17) rotatably arranged on the bottom end surface of the installation frame (16), a first fixing member (18) detachably connected to the first fixing seat (17), and a reinforcing block (19) fixedly arranged at the bottom end of the first fixing member (18), the first fixing seat (17) being provided with a first fixing groove matching the first fixing member (18), and a clamping block (20) being vertically arranged in the first fixing groove and clamped with the first fixing member (18).
5. The drone with a decoupling release device as claimed in claim 4, characterized in that: The first fixing member (18) comprises a first fixing block (21) clamped with the clamping block (20) and a first connecting block (22) arranged at the bottom end of the first fixing block (21), and both sides of the upper end of the first fixing block (21) are arc-shaped surfaces.
6. The drone with a decoupling release device as claimed in claim 4, characterized in that: The fixing assembly further comprises a second fixing member (23) vertically arranged on the bottom end surface of the reinforcing block (19), a second fixing seat (24) mounted on the supporting member (13), and a fixing rod (25) detachably connecting the second fixing member (23) and the second fixing seat (24); the supporting member (13) is provided with a second groove matching the second fixing seat (24).
7. The drone with a decoupling release device according to claim 1, characterized in that: The inner side wall of the unhooking seat (5) is provided with a plurality of groups of rotating grooves matching the hanging member (6), a rotating block (26) detachably connected to the hanging member (6) is rotatably arranged in the rotating groove, a rotating rod (27) is vertically installed between two groups of the rotating blocks (26), and the output shaft of the first driving motor (7) passes through a side surface of the unhooking seat (5) and is detachably connected to the rotating shaft of the rotating block (26).
8. The drone with a decoupling release device as claimed in claim 7, characterized in that: A mounting block (28) is vertically arranged at one end of the rotating block (26), a mounting groove matching the mounting block (28) is provided on one end surface of the hanging member (6), and a rotating hole corresponding to the rotating rod (27) is provided on the unhooking seat (5).
9. The drone with a release device according to claim 1, characterized in that: The hanging member (6) is provided with a hanging groove in an arc-shaped structure, and the bottom end surface of the limit block (11) is provided with an anti-sliding block (29) matching the connecting belt (4).
10. The drone with a release device according to claim 1, characterized in that: A plurality of groups of height-adjustable support feet (2) are detachably mounted on the bottom end surface of the unhooking seat (5).