A quick disassembly and assembly connector for surveying and mapping equipment for unmanned aerial vehicles

The quick disassembly and assembly connector simplifies the structure and integrates power supply, addressing the complexity and model-specific limitations of existing connectors for surveying and mapping equipment on UAVs.

CN112389664BActive Publication Date: 2024-12-20WUHAN HUACE INNOVATION TECHNOLOGY CO LTD
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Patent Information

Application Number
CN202011098788.6
Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
Filing Date
2020-10-14
Publication Date
2024-12-20
Estimated Expiration
2040-10-14

AI Technical Summary

Technical Problem

Existing connectors for surveying and mapping equipment on UAVs are complex in structure, require independent power supplies, and are generally model-specific, limiting their practicality.

Method used

A quick disassembly and assembly connector featuring a locking groove, slide groove, and clamping block mechanism with a spring-loaded stepped shaft, allowing for model-independent installation and power supply integration with the UAV.

Benefits of technology

Enables quick, model-independent assembly and disassembly of surveying and mapping equipment on UAVs, eliminating the need for separate power supplies and simplifying the connector structure.

✦ Generated by Eureka AI based on patent content.

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Abstract

The invention discloses a quick disassembly and assembly connector for surveying and mapping equipment for unmanned aerial vehicles; the invention provides a locking groove in the locking clamp, a sliding groove connected with the locking groove is provided on the locking clamp, a card block is provided in the sliding groove, a socket is provided on the card block, a step shaft is inserted in the socket, so that the step shaft can move with the card block and rotate relative to the socket, a thread is provided on the step shaft, and a threaded hole is provided on the locking clamp; a spring is also sleeved on the step shaft between the side wall of the card block and the side wall of the sliding groove; when in use, it is only necessary to install the locking clamp on the unmanned aerial vehicle and install the surveying and mapping equipment on the locking block, so that quick disassembly can be achieved without being restricted by the model of the unmanned aerial vehicle. At the same time, when the locking clamp locks the locking block, the male socket will engage with the female socket, and the surveying and mapping equipment on the locking block is powered by the power supply of the unmanned aerial vehicle, and there is no need to install an independent power supply for the surveying and mapping equipment. The structure is simple and more practical.
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Description

Technical Field

[0001] The present invention relates to the field of unmanned aerial vehicle auxiliary equipment, and in particular to a quick disassembly and assembly connector for surveying and mapping equipment for unmanned aerial vehicles. Background Art

[0002] UAV surveying and mapping is favored by surveying and mapping engineering units for its high operating efficiency, high measurement accuracy, small size and light weight. It uses UAV as a flight carrier and mounts various types of laser radar, aerial survey cameras and other surveying and mapping equipment to obtain point cloud data and impact data with geographic information coordinates, and realize the rapid measurement of spatial three-dimensional geographic information elements.

[0003] Different surveying and mapping equipment and UAV mounting connection methods vary greatly, but the most practical method at present is to use quick-release connectors to install the surveying and mapping equipment on the UAV. The use of quick-release connectors can ensure that the surveying and mapping equipment is fixed on the UAV while enabling rapid disassembly and assembly of the surveying and mapping equipment and the UAV. However, the existing connectors are not only complex in structure, but also require independent power supplies when many loads are installed on the UAV. In addition, the existing connectors are generally used in conjunction with specific models of UAVs and are not suitable for other UAVs, so they are less practical. Summary of the invention

[0004] The present invention provides a method for solving the problems that the existing connectors are not only complex in structure, but also require independent power supplies when many loads are installed on drones, and the existing connectors are generally used in conjunction with specific models of drones and are not suitable for other drones, thus having low practicality.

[0005] The technical solution of the present invention to solve the above technical problems is as follows: a quick disassembly and assembly connector for surveying and mapping equipment for unmanned aerial vehicles, the connector comprising:

[0006] The locking fixture has a locking groove in the middle of the locking fixture, the locking groove opening is upward, the locking groove is a structure with one end open and the other closed, a slide groove is opened on the locking fixture, one end of the slide groove is closed and the other end is connected to the locking groove, the slide groove is provided with a step at one end close to the locking groove, and a card block matching the slide groove is arranged in the slide groove, a through hole is opened in the middle of the card block, an insertion hole is opened on the locking fixture at the end of the through hole away from the locking groove, a threaded hole is opened on the locking fixture, a step shaft is inserted in the threaded hole, a threaded section on the step shaft is screwed into the threaded hole, and an end of the step shaft close to the through hole is inserted in the insertion hole, the step shaft can slide with the card block and can rotate relative to the insertion hole on the card block, and a spring is also sleeved on the step shaft between the side wall of the card block and the side wall of the slide groove;

[0007] A locking block, the locking block is adapted to the locking groove, the locking block is provided with a slot matched with the clamping block, and the locking block and the locking fixture are locked to each other in the slot by the clamping block;

[0008] Among them, a female socket is arranged at the bottom of the locking groove, and a male socket matching the female socket is arranged at the top of the locking block. When the locking block is inserted into the locking groove, the female socket is correspondingly inserted into the male socket.

[0009] Furthermore, the locking block is an A-type structure.

[0010] Furthermore, the locking groove has two side edges that are 60-degree inclined surfaces.

[0011] Furthermore, a plurality of weight-reducing holes are opened in the middle of the locking block.

[0012] Furthermore, the bottom of the locking groove is provided with an oblique groove interconnected therewith, and the bottom of the locking block is provided with an edge protrusion matching the oblique groove.

[0013] Furthermore, a handle is provided at one end of the stepped shaft away from the clamping block.

[0014] Furthermore, the male socket and the female socket are both 30pin.

[0015] Furthermore, the slide slot is a top opening structure, and a cover plate is detachably provided at the opening.

[0016] Furthermore, the locking clamp and the locking block are both made of aluminum alloy or copper alloy.

[0017] Furthermore, an annular groove is provided on the inner wall of the insertion hole, and a snap ring matching the annular groove is provided on the step shaft.

[0018] Beneficial effects: The present invention arranges a locking groove in the locking clamp, arranges a slide groove connected to the locking groove on the locking clamp, arranges a clamping block in the slide groove, arranges a socket on the clamping block, inserts a stepped shaft into the socket, so that the stepped shaft can move with the clamping block and rotate relative to the socket, arranges a thread on the stepped shaft, and arranges a threaded hole on the locking clamp. The step shaft can be tightened in the threaded hole and can also be disengaged from the threaded hole. A spring is also sleeved on the step shaft between the side wall of the block and the side wall of the slide groove. When in use, the step shaft is rotated to make the threaded section of the step shaft disengage from the threaded hole, and the block is pushed by the elastic force of the spring, so that the block is inserted into the slot of the locking block, so that the locking block and the locking clamp are locked with each other in the slot through the block to form a complete connector. A female socket is provided at the bottom of the locking slot, and a male socket matching the female socket is provided at the top of the locking block. During installation, it is only necessary to install the locking clamp on the drone and install the surveying and mapping equipment on the locking block, which can realize quick disassembly without being restricted by the model of the drone. At the same time, when the locking clamp locks the locking block, the male socket will engage with the female socket, and the surveying and mapping equipment on the locking block is powered by the power supply of the drone, and there is no need to install an independent power supply for the surveying and mapping equipment. The structure is simple and more practical. BRIEF DESCRIPTION OF THE DRAWINGS

[0019] Figure 1 This is a schematic diagram of the overall structure of a quick disassembly and assembly connector for surveying and mapping equipment for unmanned aerial vehicles according to the present invention;

[0020] Figure 2 This is a schematic diagram of the locking block structure of a quick disassembly connector for surveying and mapping equipment for unmanned aerial vehicles according to the present invention;

[0021] Figure 3 This is a schematic diagram of the locking fixture structure of a quick disassembly connector for surveying and mapping equipment for unmanned aerial vehicles according to the present invention;

[0022] Figure 4 for Figure 3 Schematic diagram of the structure of the AA section;

[0023] Figure 5 for Figure 4 Schematic diagram of the enlarged structure of A.

[0024] In the accompanying drawings, the components represented by the reference numerals are listed as follows:

[0025] 1. Locking fixture; 2. Locking groove; 3. Slide groove; 4. Block; 5. Through hole; 6. Plug hole; 7. Threaded hole; 8. Step shaft; 9. Spring; 10. Locking block; 11. Slot; 12. Weight-reducing hole; 13. Inclined groove; 14. Edge protrusion; 15. Handle; 16. Female socket; 17. Male socket; 18. Cover plate; 19. Ring groove; 20. Snap ring. DETAILED DESCRIPTION

[0026] The principles and features of the present invention are described below in conjunction with the accompanying drawings. The examples given are only used to explain the present invention and are not used to limit the scope of the present invention.

[0027] A quick disassembly connector for surveying and mapping equipment for unmanned aerial vehicles, the connector includes a locking fixture 1 and a locking block 10. When in use, the locking block 10 is locked in the locking fixture. When disassembling, it only needs to be simply disassembled. The specific implementation method is as follows:

[0028] A locking groove 2 is arranged in the middle of the locking clamp 1, and the locking groove 2 is an A-type structure. Similarly, the locking block 10 is also an A-type structure that matches the locking groove 2; in this embodiment, the locking groove 2 has 60-degree inclined surfaces on both sides, so that the opening of the locking groove 2 is relatively large, which saves time and effort during disassembly and assembly; the locking groove 2 opens upward, and the locking groove 2 is a structure with one end open and the other end closed. A slide groove 3 is opened on the locking clamp 1, and the slide groove 3 is a top opening structure. A cover plate 18 is detachably arranged at the opening, and one end of the slide groove 3 is closed and the other end is connected to the locking clamp 1. The slots 2 are connected, and a block 4 matching the slot 3 is arranged in the slot 3. A step is arranged at one end of the slot 3 close to the locking slot 2 to prevent the block 4 from sliding out of the slot 3 due to excessive travel, and the block 4 is clamped at the port with the step surface, so that the block 4 can only move within a specific range, that is, the width of the end of the slot 3 close to the locking slot 2 is smaller than the end away from the locking slot 2; a square through hole 5 is opened in the middle of the block 4, and a socket 6 is opened on the locking fixture 1 at the end of the through hole 5 away from the locking slot 2, and a threaded hole coaxial with the socket 6 is opened on the locking fixture 1 7, a stepped shaft 8 is inserted into the threaded hole 7, and a thread is provided in the middle of the stepped shaft 8. A section of the stepped shaft 8 with a thread is screwed into the threaded hole 7. Rotating the stepped shaft 8 can make the threaded end of the stepped shaft 8 screwed into the threaded hole 7, so that the stepped shaft 8 is axially fixed, and reverse rotation can also make the threaded end of the stepped shaft 8 disengage from the threaded hole 7; the end of the stepped shaft 8 close to the through hole 5 is inserted into the insertion hole 6, and the stepped shaft 8 can slide with the block 4 and can rotate relative to the insertion hole 6 on the block 4, between the side wall of the block 4 and the side wall of the slide groove 3, A spring 9 is also sleeved on the step shaft 8. When the threaded end of the step shaft 8 is tightened in the threaded hole 7, the spring 9 is compressed and the block 4 shrinks in the slide groove 3. When the threaded section of the step shaft 8 is disengaged from the threaded hole 7, the spring 9 extends. Under the action of the elastic force of the spring 9, the block 4 moves toward the locking groove 2, and the step shaft 8 also moves with the block 4. In order to facilitate the rotation of the step shaft 8, in this embodiment, a handle 15 is provided at the end of the step shaft 8 away from the block 4. The handle 15 is a cylindrical structure and is also provided with a finger groove.

[0029] The side of the locking block 10 that contacts the end of the clamping block 4 is provided with a clamping groove 11 that matches the clamping block 4, and the locking block 10 and the locking fixture 1 are locked in the clamping groove 11 through the clamping block 4; when the stepped shaft 8 is not axially fixed, the clamping block 4 extends out of the slide groove 3 to the locking groove 2 under the action of the spring, and the end of the clamping block 4 is just stuck in the clamping groove 11, locking the locking block 10 in the locking groove 2; because the bottom of the locking groove 2 is provided with a female socket 16, the top of the locking block 10 is provided with a male socket 17 that matches the female socket 16, and the male socket 17 and the female socket 16 are both 30pin; when the locking block 10 is inserted into the locking groove 2, the female socket 16 is correspondingly inserted into the male socket 17, and the female socket 16 is connected to the power supply of the drone, and the drone's own power supply can be used to provide power for the surveying and mapping equipment installed on the locking block 10. , the surveying and mapping equipment is connected to an independent power supply for lunch break.

[0030] Furthermore, in this embodiment, in order to reduce the center connection of the connector itself as much as possible while ensuring the rigidity of the connector, a plurality of weight-reducing holes 12 are opened in the middle of the locking block 10; at the same time, the locking clamp 1 and the locking block 10 are both made of aluminum alloy or copper alloy.

[0031] Furthermore, in order to further lock the locking block 10 and prevent it from moving, an oblique groove 13 communicating with the locking groove 2 is provided at the bottom, and an edge protrusion 14 matching the oblique groove 13 is provided at the bottom of the locking block 10.

[0032] Furthermore, in order to enable the stepped shaft 8 to rotate relative to the socket 6 and slide with the clamping block 4, in this embodiment, an annular groove 19 is always provided on the inner wall of the socket 6, and a clamping ring 20 that cooperates with the annular groove is provided on the stepped shaft 8; in fact, this structure can also be replaced by a bearing, and a bearing is provided in the socket 6, and the outer cylindrical surface of one end of the stepped shaft 8 is fixed on the inner wall of the inner ring of the bearing, which can also achieve this function.

[0033] The mechanisms, components and parts not specifically described in the present invention are all existing structures in the prior art and can be directly purchased from the market.

[0034] 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 quick disassembly connector for surveying and mapping equipment for unmanned aerial vehicles, characterized in that: The connector comprises: A locking clamp (1), wherein a locking groove (2) is arranged in the middle of the locking clamp (1), the locking groove (2) opens upward, and the locking groove (2) is a structure with one end open and the other end closed. A sliding groove (3) is arranged on the locking clamp (1), and the sliding groove (3) is closed at one end and communicates with the locking groove (2) at the other end. A step is arranged at the end of the sliding groove (3) close to the locking groove (2), and a card block (4) matching the sliding groove (3) is arranged in the sliding groove (3). A through hole (5) is arranged in the middle of the card block (4), and at the end of the through hole (5) away from the locking groove (2), a through hole (5) is arranged on the locking clamp (1) ) is provided with an insertion hole (6), the locking clamp (1) is provided with a threaded hole (7) coaxial with the insertion hole (6), a stepped shaft (8) is inserted in the threaded hole (7), a thread is provided in the middle of the stepped shaft (8), a section with a thread on the stepped shaft (8) is screwed into the threaded hole (7), an end of the stepped shaft (8) close to the through hole (5) is inserted into the insertion hole (6), the stepped shaft (8) can slide with the clamping block (4) and can rotate relative to the insertion hole (6) on the clamping block (4), and a spring (9) is also sleeved on the stepped shaft (8) between the side wall of the clamping block (4) and the side wall of the slide groove (3); and a locking block (10), wherein the locking block (10) is adapted to the locking groove (2), the locking block (10) is provided with a slot (11) matched with the card block (4), the locking block (10) and the locking fixture (1) are locked with each other in the slot (11) by the card block (4); wherein a female socket (16) is provided at the bottom of the locking groove (2), and a male socket (17) matching the female socket (16) is provided at the top of the locking block (10); when the locking block (10) is inserted into the locking groove (2), the female socket (16) is correspondingly inserted into the male socket (17), and the female socket (16) is connected to the power supply of the drone; The locking block (10) is of an A-type structure; the bottom of the locking groove (2) is provided with an oblique groove (13) which is interconnected therewith, and the bottom of the locking block (10) is provided with an edge protrusion (14) which matches the oblique groove (13).

2. The quick disassembly connector for surveying and mapping equipment for unmanned aerial vehicles according to claim 1, characterized in that: The locking groove (2) has two side edges that are 60-degree inclined surfaces.

3. The quick disassembly connector for surveying and mapping equipment for unmanned aerial vehicles according to claim 2, characterized in that: A plurality of weight-reducing holes (12) are provided in the middle of the locking block (10).

4. The quick disassembly connector for surveying and mapping equipment for unmanned aerial vehicles according to claim 1, characterized in that: A handle (15) is provided at one end of the stepped shaft (8) away from the clamping block (4).

5. The quick disassembly connector for surveying and mapping equipment for unmanned aerial vehicles according to claim 1, characterized in that: The male socket (17) and the female socket (16) are both 30 pin.

6. The quick disassembly connector for surveying and mapping equipment for unmanned aerial vehicles according to claim 1, characterized in that: The slide groove (3) is a top opening structure, and a cover plate (18) is detachably provided at the opening.

7. The quick disassembly connector for surveying and mapping equipment for unmanned aerial vehicles according to claim 1, characterized in that: The locking clamp (1) and the locking block (10) are both made of aluminum alloy or copper alloy.

8. The quick disassembly connector for surveying and mapping equipment for unmanned aerial vehicles according to claim 1, characterized in that: An annular groove (19) is provided on the inner wall of the insertion hole (6), and a snap ring (20) matching the annular groove is provided on the stepped shaft (8).