Fixing clamp for unmanned aerial vehicle paddle

Abstract

The utility model discloses a fixing clamp for an unmanned aerial vehicle paddle, which comprises a bottom plate, a limiting seat and a clamping component, the limiting seat and the clamping component are respectively arranged on the bottom plate, and the limiting seat can accommodate and limit a propeller hub of the unmanned aerial vehicle paddle. The configuration number of the clamping and fixing assemblies is consistent with the number of blades of the unmanned aerial vehicle propeller blades, the clamping and fixing assemblies are arranged on the periphery of the limiting base at intervals according to the arrangement mode of the blades, and each clamping and fixing assembly can clamp and limit at least two different parts of the corresponding blade. According to the fixing clamp, the unmanned aerial vehicle paddle can be firmly supported and fixed, the machining precision and the machining quality during machining operation of the unmanned aerial vehicle paddle can be effectively improved, and the production requirement of an unmanned aerial vehicle is well met. In addition, the fixing clamp is simple and reasonable in structure, easy to machine and manufacture, low in manufacturing cost, easy to operate and use and high in production efficiency.

Description

Technical Field

[0001] The utility model relates to the technical field of fixing tooling, in particular to a fixing fixture for a UAV blade. Background Art

[0002] As is known to all, in modern industrial production processes, in order to improve the processing accuracy and quality of workpieces, fixed tooling is usually provided to support and fix the workpieces.

[0003] However, in the field of UAV technology, due to the relatively irregular shape of the blade part, the commonly used fixing tooling on the market is not well adapted to it (i.e. the blade part), and it is easy for the fixing tooling to fail to clamp and fix the blade well, resulting in the blade processing accuracy and processing quality cannot be guaranteed, and cannot meet the production requirements of UAVs.

[0004] In view of this, the present utility model is proposed. Summary of the Invention

[0005] In order to overcome the above-mentioned defects, the utility model provides a fixing fixture for UAV blades, which can firmly support / fix the UAV blades, effectively improve the processing accuracy and processing quality during the UAV blade processing operation, and well meet the production requirements of UAVs.

[0006] The technical solution adopted by the present invention to solve its technical problems is: a fixing fixture for UAV blades, the UAV blades are provided with a hub and blades connected to the hub; the fixing fixture includes a base plate, and a limit seat and a clamping assembly respectively arranged on the base plate, wherein the limit seat can accommodate and limit the hub, the configuration number of the clamping assemblies is consistent with the number of the blades, and is arranged at intervals on the periphery of the limit seat according to the arrangement of the blades, and each of the clamping assemblies can clamp and limit at least two different parts on the corresponding blade.

[0007] As a further improvement of the present invention, the limiting seat is provided with a receiving groove that matches the shape of the hub and can accommodate the hub, and a positioning member that is provided in the receiving groove and can limit the positioning of the hub.

[0008] As a further improvement of the present invention, the positioning member is a positioning pin that can be inserted into the mounting hole on the hub.

[0009] As a further improvement of the present invention, a penetration opening is provided on the receiving groove, and the penetration opening corresponds to the blades one by one to allow the blades to pass through.

[0010] As a further improvement of the present invention, the number of the blades is two, and accordingly, the number of the penetration openings is two, and the number of the clamping components is two groups, which are respectively arranged on opposite sides of the limiting seat.

[0011] As a further improvement of the present invention, the clamping assembly is provided with at least two groups of clamping members, each of the clamping members is provided with a support block capable of receiving a portion of the blade, and a pressing member capable of firmly pressing the portion of the blade against the support block.

[0012] As a further improvement of the present invention, in each of the clamping members, a supporting inclined surface matching the local shape of the blade is provided on the top side of the supporting block.

[0013] As a further improvement of the present invention, in each of the clamping members, the pressing member is a toggle clamp and is fixedly arranged on the top side of the support block.

[0014] As a further improvement of the present invention, in each of the clamping assemblies, at least two groups of the clamping members are spaced apart along the length direction of the blade.

[0015] As a further improvement of the present invention, the base plate is in the shape of a rectangular plate. Accordingly, the limit seat and the two groups of clamping components are spaced along the length direction of the base plate and fixedly arranged on the upper side of the base plate; in addition, a handle for the operator to hold is also fixedly arranged on the upper side of the base plate.

[0016] The beneficial effects of the present invention are as follows: Compared with the prior art, ① the present invention, by adopting the limit seat and at least two sets of the clamping components, can achieve a firm support / support fixation of the UAV blades, thereby effectively improving the processing accuracy and processing quality during the UAV blade processing operation, and well meeting the production requirements of UAVs. ② The structure of the fixing fixture of the present invention is simple and reasonable, easy to process and manufacture, with low production cost, easy to operate and use, and high production efficiency. BRIEF DESCRIPTION OF THE DRAWINGS

[0017] Figure 1 This is a schematic diagram of the structure of a UAV blade in the prior art;

[0018] Figure 2 This is a schematic structural diagram of the fixing fixture of the present invention;

[0019] Figure 3 for Figure 2 An enlarged structural diagram of the limit seat shown in FIG;

[0020] Figure 4 for Figure 2 An enlarged structural diagram of the clamping fixture shown in ;

[0021] Figure 5 This is a schematic diagram of the fixing fixture of the present invention in use.

[0022] The following description is made with reference to the accompanying drawings:

[0023] 1. Fixing fixture; 10. Bottom plate; 11. Limit seat; 110. Receiving groove; 111. Positioning piece; 112. Through-hole; 12. Clamping piece; 120. Support block; 1200. Support slope; 121. Pressing piece; 13. Handle; 2. UAV propeller blade; 20. Propeller hub; 21. Blade; 22. Mounting hole. DETAILED DESCRIPTION

[0024] The preferred embodiments of the present invention are described in detail below with reference to the accompanying drawings.

[0025] Example 1:

[0026] This embodiment 1 provides a fixing fixture 1, which is used as a fixing tool for the processing of drone blades 2. The drone blades 2 adopt the conventional structure in the current drone technology field, so the brief description is as follows: Please refer to the attached Figure 1 As shown, the UAV blade 2 is provided with a hub 20 and blades 21 connected to the hub 20, wherein the hub 20 is used to connect with the motor drive mechanism in the UAV, that is, it can be understood that a plurality of mounting holes 22 are provided on the hub 20; the blades 21 can be configured to be no less than two and connected to the hub 20 at intervals according to product design requirements; when the motor drive mechanism drives the hub 20 to rotate, the blades 21 can be driven to rotate together.

[0027] Based on the above structure of the drone blade 2, the structure of the fixing fixture 1 preferably used in this embodiment 1 is: Figure 2 As shown, the fixing fixture 1 includes a base plate 10, and a limiting seat 11 and a clamping assembly respectively arranged on the base plate 10, wherein the limiting seat 11 can accommodate and limit the hub 20, the number of the clamping assemblies configured is consistent with the number of the blades 21, and is arranged at intervals on the periphery of the limiting seat 11 according to the arrangement of the blades 21, and each of the clamping assemblies can clamp and limit at least two different parts on the blade 21 corresponding to it. It can be understood that this embodiment 1 can achieve firm support / support and fixation of the drone blade 2 by adopting the limiting seat 11 and a combination of no less than two groups of the clamping assemblies (see the attached Figure 5 As shown in the figure), the machining accuracy and quality of the UAV blades can be effectively improved, which satisfies the production requirements.

[0028] The specific structure of the fixing fixture 1 described in this embodiment 1 is described in detail below.

[0029] First, regarding the limiting seat 11.

[0030] In order to realize the above-mentioned "support / support and fixation" function of the limit seat 11 and combine it with the hub 20 structure, the structure of the limit seat 11 preferably adopted in this embodiment 1 is: Figure 2 and attached Figure 3 As shown, the limiting seat 11 is provided with a receiving groove 110 that matches the shape of the hub 20 and can accommodate the hub 20, and a positioning member 111 that is provided in the receiving groove 110 and can limit the positioning of the hub 20. It can be understood that the receiving groove 110 is a contoured groove structure, which can not only accommodate the hub 20 but also limit the hub 20; when combined with the limiting effect of the positioning member 111 on the hub 20, the hub 20 can be securely positioned in the receiving groove 110. Please refer to the attached figure. Figure 5 shown.

[0031] Furthermore, the positioning member 111 is a positioning pin that can be inserted into the mounting hole 22 on the hub 20. By combining the positioning pin with the mounting hole 22 to achieve the restricted positioning of the hub 20, the operation is simple and convenient, the positioning effect is good, and the structure is simple and the production cost is low.

[0032] In addition, the positioning pin can be fixedly arranged on the inner wall of the bottom of the receiving groove 110 by tight fitting or screw connection, which is a conventional technical means and will not be described in detail here.

[0033] For further information, please refer to the attached Figure 3 As shown, the receiving groove 110 is also integrally provided with a penetration opening 112, and the penetration opening 112 corresponds to the blade 21 one by one, so that the blade 21 can pass through freely. Figure 1 The drone blade 2 shown is provided with two blades 21 that are arranged opposite to each other, and the penetration openings 112 are also provided with two blades that are arranged opposite to each other.

[0034] Next, regarding the clamping assembly.

[0035] Based on the above configuration of the blades 21 , in this embodiment 1, the clamping components are also configured in two groups and are respectively disposed on opposite sides of the limiting seat 11 to cooperate with the two blades 21 in a one-to-one correspondence.

[0036] Regarding the specific structure of the clamping assembly, the preferred embodiment 1 is as follows: Figure 2 and attached Figure 4As shown, the clamping assembly is provided with at least two sets of clamping members 12 (attached Figure 2 Two sets of clamping members 12 are shown in the figure, but the present embodiment 1 is not limited thereto). Each of the clamping members 12 is provided with a support block 120 capable of receiving / supporting a portion of the blade 21, and a pressing member 121 capable of firmly pressing the portion of the blade 21 against the support block 120. It is understandable that by combining the fixed support block 120 with the movable pressing member 121, the blade 21 can be clamped and fixed (see the attached diagram). Figure 5 as shown) or loosen.

[0037] Furthermore, in each of the clamping members 12, a supporting slope 1200 is integrally provided on the top side of the support block 120, which matches the local shape of the blade 21, so that the supporting slope 1200 can fit the local shape of the blade 21 thereon, thereby facilitating the pressing member 121 to firmly press the local part of the blade 21 against the support block 120 to avoid shaking; the pressing member 121 is preferably an elbow clamp (also known as a horizontal quick clamp), and is detachably fixed to the top side of the support block 120 by screws; the elbow clamp is easy to operate, has a good clamping effect, and has a low production cost, which is conducive to production applications.

[0038] Furthermore, in each of the clamping assemblies, at least two groups of the clamping members 12 are spaced apart along the length direction of the blade 21 to achieve balanced and stable clamping and fixing of the blade 21 .

[0039] Next, let's discuss the base plate 10 .

[0040] Based on the shape of the drone blade 2 and to save costs and facilitate installation and use, in this embodiment 1, the bottom plate 10 adopts a rectangular plate shape, which can be seen in the attached figure. Figure 2 As shown. Accordingly, the limit seat 11 is centrally located in the middle of the upper side of the base plate 10, and the two sets of clamping assemblies are respectively located on either side of the limit seat 11 along the length of the base plate 10. That is, the limit seat 11 and the two sets of clamping assemblies are spaced apart along the length of the base plate 10 and fixedly disposed on the upper side of the base plate 10. Furthermore, the limit seat 11 and the plurality of support blocks 120 are each fixed to the upper side of the base plate 10 by rivets or screws.

[0041] In addition, a handle 13 for the operator to hold is fixedly provided on the upper side of the base plate 10, that is, the operator can move the fixing fixture 1 through the handle 13. Furthermore, the handle 13 is detachably mounted on the upper side of the base plate 10 by screws.

[0042] In summary, the fixing fixture of the present invention can securely support and secure drone blades, effectively improving the machining accuracy and quality of drone blades, and effectively meeting the production requirements of drones. Furthermore, the fixing fixture has a simple and rational structure, making it easy to manufacture and inexpensive, easy to operate, and highly efficient.

[0043] In the above description, many specific details are set forth in order to fully understand the present invention. However, the above description is only a preferred embodiment of the present invention. The present invention can be implemented in many other ways different from those described herein, so the present invention is not limited by the specific implementation disclosed above. At the same time, any person skilled in the art can use the above-disclosed methods and technical contents to make many possible changes and modifications to the technical solution of the present invention without departing from the scope of the technical solution of the present invention, or modify it into an equivalent embodiment of equivalent changes. Any simple modification, equivalent change and modification made to the above embodiments based on the technical essence of the present invention without departing from the content of the technical solution of the present invention still falls within the scope of protection of the technical solution of the present invention.

Claims

1. A fixing fixture for a drone blade, wherein the drone blade (2) is provided with a hub (20) and a blade (21) connected to the hub (20); characterized in that: The fixing fixture (1) comprises a base plate (10), and a limiting seat (11) and a clamping assembly respectively arranged on the base plate (10), wherein the limiting seat (11) is capable of accommodating and restricting the hub (20), the number of the clamping assemblies configured is consistent with the number of the blades (21), and the clamping assemblies are arranged at intervals on the periphery of the limiting seat (11) according to the arrangement of the blades (21), and each of the clamping assemblies is capable of clamping and restricting at least two different parts on the blade (21) corresponding thereto.

2. The fixing fixture for drone blades according to claim 1, characterized in that: The limiting seat (11) is provided with a receiving groove (110) that matches the shape of the propeller hub (20) and can accommodate the propeller hub (20), and a positioning member (111) that is provided in the receiving groove (110) and can limit the positioning of the propeller hub (20).

3. The fixing fixture for drone blades according to claim 2, characterized in that: The positioning member (111) is a positioning pin that can be inserted into the mounting hole (22) on the hub (20).

4. The fixing fixture for drone blades according to claim 2, characterized in that: The receiving groove (110) is provided with a penetration opening (112), and the penetration opening (112) corresponds to the blade (21) one by one, so as to allow the blade (21) to pass through.

5. The fixing fixture for drone blades according to claim 4, characterized in that: The blades (21) are provided in pairs, and accordingly, the penetration openings (112) are provided in pairs, and the clamping components are provided in two groups, which are respectively arranged on opposite sides of the limiting seat (11).

6. The fixing fixture for drone blades according to claim 1, characterized in that: The clamping assembly is provided with at least two groups of clamping members (12), each of the clamping members (12) being provided with a support block (120) capable of receiving a portion of the blade (21), and a pressing member (121) capable of firmly pressing the portion of the blade (21) against the support block (120).

7. The fixing fixture for drone blades according to claim 6, characterized in that: In each of the clamping members (12), a top side of the support block (120) is provided with a support inclined surface (1200) that matches the local shape of the blade (21).

8. The fixing fixture for drone blades according to claim 6, characterized in that: In each of the clamping members (12), the pressing member (121) is a toggle clamp and is fixedly arranged on the top side of the supporting block (120).

9. The fixing fixture for drone blades according to claim 6, characterized in that: In each of the clamping components, at least two groups of the clamping members (12) are arranged at intervals along the length direction of the blade (21).

10. The fixing fixture for drone blades according to claim 5, characterized in that: The bottom plate (10) is in the shape of a rectangular plate, and accordingly, the limiting seat (11) and the two groups of the clamping components are spaced apart along the length direction of the bottom plate (10) and fixedly arranged on the upper side of the bottom plate (10); In addition, a handle (13) for an operator to hold is fixedly provided on the upper side of the bottom plate (10).

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