A UAV vertical tail bonding device

Abstract

The utility model relates to a kind of unmanned plane vertical tail bonding device, belong to unmanned plane field.It includes: vertical tail positioning block (4), vertical tail mechanism positioning block (5), vertical tail positioning pin (6);The vertical tail positioning block (4) is cuboid structure, and wing clamping slot is opened in cuboid upper surface, vertical tail positioning block (4) end is equipped with vertical tail mechanism positioning hole, the vertical tail mechanism positioning block (5) is fixed in vertical tail mechanism positioning hole by vertical tail positioning pin (6), unmanned plane vertical tail (1) is placed in wing clamping slot, the bonding end of vertical tail rotating shaft assembly (3) needing to be bonded is coated with glue, vertical tail mechanism positioning block (5) is fixed on the upper side of vertical tail (1), the utility model satisfies unmanned plane vertical tail drawing paper tolerance requirement from angle and distance two aspects, improves unmanned plane vertical tail bonding work efficiency.

Description

Technical Field

[0001] This utility model belongs to the field of unmanned aerial vehicles (UAVs), specifically relating to a vertical tail fin bonding device for UAVs. Background Technology

[0002] The vertical tail fin of a certain UAV is composed of composite materials. Due to modular requirements, the vertical tail fin is designed as a foldable structure. To ensure the effectiveness of the vertical tail fin, the design drawings specify the tolerance range for its fully deployed position. To ensure bonding accuracy, traditional manual operation suffers from low efficiency and poor consistency. Therefore, a process equipment needs to be designed to efficiently and accurately complete the bonding of the vertical tail fin, ensuring the overall flight stability of the UAV. Utility Model Content

[0003] (a) Technical problems to be solved

[0004] The technical problem to be solved by this utility model is to provide a vertical tail fin bonding device for drones to complete the vertical tail fin bonding of drones in a high-efficiency and accurate manner.

[0005] (II) Technical Solution

[0006] To solve the above-mentioned technical problems, this utility model provides a vertical tail fin bonding device for unmanned aerial vehicles, including: a vertical tail fin positioning block 4, a vertical tail mechanism positioning block 5, and a vertical tail positioning pin 6.

[0007] The vertical tail fin positioning block 4 is a cuboid structure with a wing slot on the upper surface of the cuboid. The vertical tail fin positioning block 4 has a vertical tail mechanism positioning hole at its end. The vertical tail mechanism positioning block 5 is fixed in the vertical tail mechanism positioning hole by the vertical tail positioning pin 6. The UAV vertical tail fin 1 is placed in the wing slot. The bonding end of the vertical tail pivot assembly 3 that needs to be bonded is applied with glue and fixed above the vertical tail fin 1 by the vertical tail mechanism positioning block 5.

[0008] The vertical tail mechanism positioning block 5 has a U-shaped structure. The left and right sides of the vertical tail mechanism positioning block 5 are positioning parts, which are arranged in parallel and perpendicular to the body of the vertical tail mechanism positioning block 5. Screw holes are respectively opened on the positioning parts on the left and right sides of the vertical tail mechanism positioning block 5 for positioning the vertical tail rotating shaft assembly 3.

[0009] (III) Beneficial Effects

[0010] Compared with the existing technology, the present invention has the following beneficial effects: it meets the tolerance requirements of the UAV vertical tail fin drawings in terms of both angle and distance, and improves the efficiency of UAV vertical tail fin bonding work. Attached Figure Description

[0011] Figure 1 Tolerance requirements for vertical tail assembly;

[0012] Figure 2 Diagram of the vertical tail fin positioning block;

[0013] Figure 3 Diagram of the positioning block for the vertical tail mechanism;

[0014] Figure 4 Diagram of the vertical tail locating pin;

[0015] Figure 5 This is a schematic diagram of the vertical tail fin bonding. Detailed Implementation

[0016] To make the objectives, contents, and advantages of this utility model clearer, the specific embodiments of this utility model will be described in further detail below with reference to the accompanying drawings and examples.

[0017] This embodiment provides a vertical tail bonding device for a drone, including: a vertical tail positioning block 4, a vertical tail mechanism positioning block 5, and a vertical tail positioning pin 6.

[0018] The vertical tail fin positioning block 4 is a cuboid structure with a wing slot on the upper surface of the cuboid. The vertical tail fin positioning block 4 has a vertical tail mechanism positioning hole at its end. The vertical tail mechanism positioning block 5 is fixed in the vertical tail mechanism positioning hole by the vertical tail positioning pin 6. The UAV vertical tail fin 1 is placed in the wing slot. The bonding end of the vertical tail pivot assembly 3 that needs to be bonded is applied with glue and fixed above the vertical tail fin 1 by the vertical tail mechanism positioning block 5.

[0019] The vertical tail mechanism positioning block 5 has a U-shaped structure. The left and right sides of the vertical tail mechanism positioning block 5 are positioning parts, which are arranged in parallel and perpendicular to the body of the vertical tail mechanism positioning block 5. Screw holes are respectively opened on the positioning parts on the left and right sides of the vertical tail mechanism positioning block 5 for positioning the vertical tail rotating shaft assembly 3.

[0020] like Figure 1 As shown, the distance between the centerline of the vertical tail and the vertical tail pivot assembly 3 is required to be 10.5±0.5, and the spanwise angle between the vertical tail pivot assembly 3 and the vertical tail fin 1 is 90°-91°. The process equipment of this utility model can guarantee these two key dimensions.

[0021] like Figure 5As shown, the vertical tail fin positioning block 4 is installed on a horizontal workbench. Prepare one vertical tail mechanism positioning block 5 and two vertical tail positioning pins 6. Place a vertical tail fin 1 into the wing slot on the vertical tail fin positioning block 4. A vertical tail torsion spring is connected to the vertical tail fin 1. Accurate positioning indicates that the vertical tail fin airfoil fits the slot. Fix the vertical tail mechanism positioning block 5 to the vertical tail fin positioning block 4 using the two vertical tail positioning pins 6. The vertical tail positioning pins 6 and the positioning pin holes are fitted with tolerances; smooth insertion of the positioning pins indicates accurate positioning. Apply adhesive to the bonding end of the vertical tail pivot assembly 3 to be bonded and fix it through the screw holes on the vertical tail mechanism positioning block 5. This completes the bonding operation. Let it stand for 24 hours until the adhesive is completely dry, then remove the bonded vertical tail.

[0022] The above description is only a preferred embodiment of the present utility model. It should be noted that for those skilled in the art, several improvements and modifications can be made without departing from the technical principles of the present utility model, and these improvements and modifications should also be considered within the protection scope of the present utility model.

Claims

1. A UAV vertical tail bonding device, characterized in that, include: Vertical tail fin positioning block (4), vertical tail mechanism positioning block (5), vertical tail positioning pin (6); The vertical tail fin positioning block (4) is a cuboid structure. A wing slot is opened on the upper surface of the cuboid. A vertical tail mechanism positioning hole is opened at the end of the vertical tail fin positioning block (4). The vertical tail mechanism positioning block (5) is fixed in the vertical tail mechanism positioning hole by the vertical tail positioning pin (6). The UAV vertical tail fin (1) is placed in the wing slot. Glue is applied to the bonding end of the vertical tail pivot assembly (3) that needs to be bonded. It is fixed above the vertical tail fin (1) by the vertical tail mechanism positioning block (5).

2. The UAV vertical tail bonding device as described in claim 1, characterized in that, The vertical tail mechanism positioning block (5) has a U-shaped structure. The left and right sides of the vertical tail mechanism positioning block (5) are positioning parts, which are arranged in parallel and perpendicular to the body of the vertical tail mechanism positioning block (5). Screw holes are respectively opened on the positioning parts on the left and right sides of the vertical tail mechanism positioning block (5) for positioning the vertical tail rotating shaft assembly (3).

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