Unmanned aerial vehicle propeller clamp assembling jig

By designing the drone paddle clamp assembly fixture, using the coordination of the positioning stage and the thimble, the problem of slow manual alignment of the paddle clamp is solved, efficient paddle clamp assembly is achieved, and production efficiency is improved.

CN223291107UActive Publication Date: 2025-09-02DONGGUAN TOPVIEW PLASTIC MFG
View PDF 0 Cites 0 Cited by

Patent Information

Application Number
CN202422851750.1
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2024-11-21
Publication Date
2025-09-02
Estimated Expiration
2034-11-21

AI Technical Summary

Technical Problem

The assembly of existing drone paddle clamps requires manual alignment, resulting in slow assembly speed and cannot meet the efficient production needs of modern industry.

Method used

A drone paddle clamp assembly fixture is designed, including a positioning stage and a thimble. Through the coordination of the positioning groove and the positioning column, the automatic alignment and fixation of the paddle clamp assembly is realized, and the assembly efficiency is improved.

Benefits of technology

Through the design of the fixture, the rapid assembly of the drone paddle clamps is achieved, and the production efficiency and product quality are improved.

✦ Generated by Eureka AI based on patent content.

Smart Images

  • Figure CN223291107U_ABST
    Figure CN223291107U_ABST
Patent Text Reader

Abstract

The utility model relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle propeller clamp assembling jig which comprises a positioning carrying table (10) and at least two ejector pins (20) matched with the positioning carrying table (10). Two first positioning columns (111) correspondingly matched with the ejector pins (20) are oppositely arranged at the bottom of the first positioning groove (11), and a second positioning groove (12) and a third positioning groove (13) are oppositely formed in the two sides of the first positioning groove (11). The device is provided with a positioning platform deck, the positioning platform deck is provided with a first positioning groove, a second positioning groove and a third positioning groove, and two first positioning columns are oppositely arranged at the bottom of the first positioning groove; the positioning platform deck and the ejector pins matched with the two first positioning columns on the positioning platform deck are arranged, and the positioning platform deck is matched with the ejector pins, so that the assembling speed of the unmanned aerial vehicle propeller clamp can be increased, and the production efficiency of products is improved.
Need to check novelty before this filing date? Find Prior Art

Description

Technical Field

[0001] The utility model relates to the technical field of unmanned aerial vehicles (UAVs), in particular to an assembly jig for propeller clamps of UAVs. Background Art

[0002] As people's living standards improve, drones are becoming increasingly commonplace in all aspects of life. A drone consists of a flight platform, powertrain, control system, navigation, and safety systems. The propellers on a drone provide power for the aircraft and are key components of the powertrain.

[0003] In the prior art, a paddle clamp includes a mounting clamp, a left paddle blade, and a right paddle blade. The mounting clamp includes an upper clamp and a lower clamp. The upper clamp and the lower clamp are clamped together, and the left and right paddle blades are connected to the left and right paddle blades respectively on the left and right sides via a rotating shaft. The left and right sides of the lower clamp are also provided with a circle of positioning grooves, and the positioning grooves are provided with an expansion positioning groove and a storage positioning groove. The left and right paddle blades can rotate freely around the rotating shaft, and the blades are expanded by the centrifugal force generated by the high-speed rotation of the paddle clamp. Currently, most paddle clamps on the market require manual assembly. During manual assembly, the alignment between the upper clamp, the lower clamp, and the left and right paddle blades is inconvenient, the assembly speed is slow, and the production efficiency of the product is reduced. This cannot meet the increasingly high requirements of modern industry and production for paddle clamp assembly.

[0004] Therefore, the existing technology needs to be improved and enhanced. Utility Model Content

[0005] In order to overcome the above-mentioned shortcomings, the utility model aims to provide a technical solution that can solve the above-mentioned problems.

[0006] In order to achieve the above purpose, the technical solution adopted by the present utility model is:

[0007] A drone propeller clamp assembly jig includes a positioning platform and at least two ejector pins that cooperate with the positioning platform. The positioning platform is provided with at least a first positioning groove, and two first positioning columns corresponding to the ejector pins are oppositely arranged at the bottom of the first positioning groove. A second positioning groove and a third positioning groove are oppositely arranged on both sides of the first positioning groove.

[0008] As a further solution of the present invention, the positioning platform is arranged on a lower template, the ejector pin is arranged on an upper template, a first guide column is arranged on the four corners of the lower template, and a first guide sleeve is arranged on the four corners of the upper template, and the first guide column makes a linear reciprocating motion in the corresponding first guide sleeve.

[0009] As a further solution of the present invention, the ejector pin is arranged on a fixed plate, and the fixed plate is arranged on the upper template.

[0010] As a further solution of the present invention, a second guide column is provided on each of the four corners of the fixing plate, and a second guide sleeve is provided on each of the four corners of the positioning platform, and the second guide column cooperates with the corresponding second guide sleeve.

[0011] As a further solution of the present invention, a movable plate is provided on the side of the fixed plate facing the positioning platform, four connecting rods pass through the fixed plate and are connected to the movable plate, and a spring is provided on the connecting rod between the fixed plate and the movable plate.

[0012] As a further solution of the present invention, a connecting rod is provided between two adjacent second guide pillars.

[0013] As a further solution of the present invention, a support platform adapted to the inclined surface of the blade is provided in each of the second positioning groove and the third positioning groove.

[0014] As a further solution of the present invention, a second positioning column is provided at each of the four corners of the positioning platform near the second guide sleeve, and a positioning hole matching the second positioning column is provided on the movable plate.

[0015] Compared with the prior art, the beneficial effects of the present invention are:

[0016] Due to the adoption of the above-mentioned structural design, that is, a positioning platform is provided, a first positioning groove, a second positioning groove and a third positioning groove are provided on the positioning platform, two first positioning columns are relatively provided at the bottom of the first positioning groove; and a ejector pin that cooperates with the two first positioning columns on the positioning platform. Through the mutual cooperation between the positioning platform and the ejector pin, the speed of assembling the drone propeller clamp can be increased, thereby improving the production efficiency of the product. BRIEF DESCRIPTION OF THE DRAWINGS

[0017] Attachment Figure 1 This is a schematic structural diagram of an embodiment of the present utility model;

[0018] Attachment Figure 2 This is a schematic diagram of the exploded structure of an embodiment of the present utility model;

[0019] Attachment Figure 3 This is a structural diagram of the positioning platform according to an embodiment of the present utility model.

[0020] The numbers in the figure are:

[0021] 10-positioning platform, 20-thimble, 30-lower template, 40-upper template, 50-fixed plate, 60-movable plate;

[0022] 11-first positioning groove, 12-second positioning groove, 13-third positioning groove, 14-second guide sleeve, 15-support platform, 16-second positioning column;

[0023] 111-first positioning column;

[0024] 31- first guide post;

[0025] 41-first guide sleeve;

[0026] 51-second guide post, 52-connecting rod, 53-spring;

[0027] 61-Positioning hole. DETAILED DESCRIPTION

[0028] All features disclosed in this specification, or all steps in the disclosed methods or processes, except mutually exclusive features and / or steps, can be combined in any manner.

[0029] Unless otherwise stated, any feature disclosed in this specification, including any appended claims, abstract, and drawings, may be replaced by other equivalent or similar features. That is, unless otherwise stated, each feature is only an example of a series of equivalent or similar features.

[0030] In the description of the present invention, it should be understood that the terms "one end", "the other end", "outside", "upper", "inside", "horizontal", "coaxial", "center", "end", "length", "outer end", etc. indicate orientations or positional relationships based on the orientations or positional relationships shown in the accompanying drawings. They are only for the convenience of describing the present invention and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation. Therefore, they cannot be understood as limitations on the present invention.

[0031] In addition, in the description of the present invention, “a plurality of” means at least two, such as two, three, etc., unless otherwise clearly and specifically defined.

[0032] Terms such as "upper", "above", "lower", and "below" used in this utility model to indicate spatial relative positions are for the purpose of convenience to describe the relationship of one unit or feature relative to another unit or feature as shown in the accompanying drawings. Terms of spatial relative position may be intended to include different orientations of the device in use or operation in addition to the orientation shown in the drawings. For example, if the device in the drawings is turned over, the units described as being "below" or "beneath" other units or features will be located "above" the other units or features. Therefore, the exemplary term "below" can encompass both the above and below orientations. The device may be otherwise oriented, rotated 90 degrees or in other orientations, and the spatially relative descriptors used herein interpreted accordingly.

[0033] In this utility model, unless otherwise specified or limited, the terms "disposed," "socketed," "connected," "through," and "inserted" should be understood in a broad sense. For example, they can refer to fixed or detachable connections, or integration; mechanical or electrical connections; direct or indirect connections through an intermediate medium; internal communication between two components or interaction between two components, unless otherwise specified. Those skilled in the art will understand the specific meanings of the above terms in this utility model based on specific circumstances.

[0034] Example:

[0035] like Figure 1-3 As shown, the present application provides a drone propeller clamp assembly jig, comprising a positioning platform 10 and four ejector pins 20 cooperating with the positioning platform 10, the four ejector pins 20 being opposite to each other in pairs, and the positioning platform 10 being provided with two first positioning grooves 11 for positioning the mounting clamp, the bottom of the first positioning groove 11 being relatively provided with two first positioning columns 111 for placing the lower clamp corresponding to the ejector pins, and the two sides of the first positioning groove 11 being relatively provided with a second positioning groove 12 for placing the left blade and a third positioning groove 13 for placing the right blade. Through the above-mentioned structural design, the mutual cooperation between the positioning platform and the ejector pins can increase the speed of assembling the drone propeller clamp and improve the production efficiency of the product.

[0036] When the present invention is working, the lower clamp is first placed in the first positioning groove 11. Since two first positioning posts 111 are provided in the first positioning groove 11, the lower clamp is fixed on the two first positioning posts 111 of the first positioning groove 11. Then the left blade and the right blade are placed in the second positioning groove 12 and the third positioning groove 13 respectively, and then the upper clamp is placed in the first positioning groove 11. Finally, the ejector pin 20 moves toward the positioning platform 10 to assemble the lower clamp, the upper clamp and the left and right blades together through the connecting piece.

[0037] Specifically, the positioning platform 10 is arranged on a lower template 30, the ejector pin 20 is arranged on a fixed plate 50, and the fixed plate 50 is arranged on the upper template 40. A first guide column 31 is provided on each of the four corners of the lower template 30, and a first guide sleeve 41 is provided on each of the four corners of the upper template 40. The first guide column 31 makes a linear reciprocating motion in the corresponding first guide sleeve 41. The first guide column 31 on the lower template 30 cooperates with the first guide sleeve of the upper template 40 to ensure precise alignment and smooth movement of the upper template 40 and the lower template 30, thereby improving the performance and reliability of the entire fixture.

[0038] Specifically, a second guide column 51 is provided on each of the four corners of the fixed plate 50, and a second guide sleeve 14 is provided on each of the four corners of the positioning platform 10. The second guide column 51 cooperates with the corresponding second guide sleeve 14. When the upper template 40 moves toward the positioning platform 10, the second guide column 51 is inserted into the corresponding second guide sleeve 14, further ensuring the precise alignment of the fixed plate 50 and the positioning platform 10.

[0039] Specifically, a movable plate 60 is provided on the side of the fixed plate 50 facing the positioning platform 10, and four connecting rods 52 pass through the fixed plate 50 and are connected to the movable plate 60. A connecting rod 52 is provided between two adjacent second guide columns 51, and the connecting rod 52 is a light rod bolt. A spring 53 is provided on the connecting rod 52 between the fixed plate 50 and the movable plate 60. When the fixed plate 50 moves with the upper template 40, the second guide column 51 on the fixed plate 50 is inserted into the second guide sleeve 14 on the positioning platform 10, the movable plate 60 contacts the positioning platform 10, and the fixed plate 50 continues to move. Since a spring 53 is provided between the fixed plate 50 and the movable plate 60, the fixed plate 50 applies a force on the movable plate 60 through the spring 53, thereby playing a buffering role.

[0040] Specifically, a support platform 15 adapted to the inclined surface of the blade is provided in each of the second positioning groove 12 and the third positioning groove 13. The two support platforms 15 are in opposite directions and are used to adapt to and support the blade to prevent the blade from being installed upside down.

[0041] Specifically, a second positioning column 16 is provided at each of the four corners of the positioning platform 10 near the second guide sleeve 14 , and a positioning hole 61 is provided on the movable plate 60 to cooperate with the second positioning column 16 for accurately positioning the movable plate 60 .

[0042] In summary, the present invention solves the deficiencies in the prior art through the above-mentioned structural design, and has the characteristics of reasonable structure, high efficiency, and high speed.

[0043] The above description is merely a specific embodiment of the present invention, but the scope of protection of the present invention is not limited thereto. Any changes or substitutions that do not require creative effort should be included within the scope of protection of the present invention. Therefore, the scope of protection of the present invention should be based on the scope of protection defined in the claims.

Claims

1. A drone propeller clamp assembly fixture, characterized by: The invention comprises a positioning platform (10) and at least two ejector pins (20) matched with the positioning platform (10), wherein the positioning platform (10) is provided with at least one first positioning groove (11), two first positioning columns (111) correspondingly matched with the ejector pins (20) are relatively provided at the bottom of the first positioning groove (11), and a second positioning groove (12) and a third positioning groove (13) are relatively provided on both sides of the first positioning groove (11).

2. The drone propeller clamp assembly jig according to claim 1, characterized in that: The positioning platform (10) is arranged on a lower template (30), the ejector pin (20) is arranged on an upper template (40), a first guide column (31) is arranged on each of the four corners of the lower template (30), and a first guide sleeve (41) is arranged on each of the four corners of the upper template (40), and the first guide column (31) performs linear reciprocating motion in the corresponding first guide sleeve (41).

3. The drone propeller clamp assembly jig according to claim 2, characterized in that: The ejector pin (20) is arranged on a fixed plate (50), and the fixed plate (50) is arranged on the upper template (40).

4. The drone propeller clamp assembly jig according to claim 3, characterized in that: A second guide column (51) is provided on each of the four corners of the fixing plate (50), and a second guide sleeve (14) is provided on each of the four corners of the positioning platform (10), and the second guide column (51) is matched with the corresponding second guide sleeve (14).

5. The drone propeller clamp assembly jig according to claim 4, characterized in that: A movable plate (60) is provided on one side of the fixed plate (50) facing the positioning platform (10), four connecting rods (52) pass through the fixed plate (50) and are connected to the movable plate (60), and a spring (53) is provided on the connecting rod (52) between the fixed plate (50) and the movable plate (60).

6. The drone propeller clamp assembly jig according to claim 5, characterized in that: A connecting rod (52) is provided between two adjacent second guide pillars (51).

7. The drone propeller clamp assembly jig according to claim 6, characterized in that: A support platform (15) adapted to the inclined surface of the blade is provided in each of the second positioning groove (12) and the third positioning groove (13).

8. The drone propeller clamp assembly jig according to claim 7, characterized in that: A second positioning column (16) is provided at each of the four corners of the positioning platform (10) near the second guide sleeve (14), and a positioning hole (61) matching the second positioning column (16) is provided on the movable plate (60).