Integrated unmanned aerial vehicle structure with firearm mounting function

Abstract

The utility model relates to an integrated unmanned aerial vehicle structure, in particular to an integrated unmanned aerial vehicle structure with a gun mounting function. The integrated unmanned aerial vehicle structure with the firearm mounting function comprises a vehicle body fusion integrated support, a flying platform vehicle arm, a first mounting plate, a trigger release steering engine position and the like. A machine body fusion integrated support is arranged at the top of the mounting frame and used for mounting a gun, a trigger groove is formed in the machine body fusion integrated support, and a trigger release steering engine position is arranged in the middle of the left side of the machine body fusion integrated support. The unmanned aerial vehicle body integrates the design of the integrated support, the Picatini guide rail limiting mechanism and the grab handle clamping mechanism, the unmanned aerial vehicle and the gun are designed to be of an integrated structure, and instability of a traditional external hanging type design is avoided.

Description

TECHNICAL FIELD

[0001] The utility model relates to an integrated unmanned plane structure, especially an integrated unmanned plane structure with a gun mounting function. BACKGROUND

[0002] In recent years, the unmanned plane technology develops rapidly, and its application range has been expanded from the traditional aerial photography, surveying and mapping to logistics transportation, patrol security and tactical use fields. In some specific scenarios, such as special combat tasks or security purposes, the unmanned plane needs to carry and operate specific equipment, such as guns, to perform precise strikes, deterrence or defense tasks. However, realizing the stable integration of the unmanned plane and the gun needs to overcome many technical challenges, such as load balancing, vibration control and trigger stability. In addition, the reliability and operation safety of such equipment are crucial, which directly relates to the success of the task and the safety of the environment. At present, some unmanned planes on the market can realize the equipment mounting function, but there are still the following main problems in actual use:

[0003] Most of the existing mounting designs adopt an external mounting structure, which lacks an integrated design with the fuselage of the unmanned plane. This structure easily leads to the center of gravity deviation in flight, affecting the stability and maneuverability of the unmanned plane. SUMMARY

[0004] In order to overcome the shortcomings of the existing unmanned plane mounting design, which is mostly external, lacks an integrated design with the fuselage of the unmanned plane, and easily causes the center of gravity deviation in flight, affecting the stability, the utility model can provide an integrated unmanned plane structure with a gun mounting function.

[0005] The technical scheme of the utility model is as follows: an integrated unmanned plane structure with a gun mounting function, comprising a fuselage integrated support and a mounting rack, the mounting rack top is provided with the fuselage integrated support, the fuselage integrated support is provided with a trigger slot, the left side middle part of the fuselage integrated support is provided with a trigger release rudder position, the front part of the left end of the fuselage integrated support is provided with a picatinny rail limiting, the rear side of the fuselage integrated support is provided with a handle clamping mechanism, the mounting rack is provided with a plurality of flight platform arms, the bottom of the mounting rack is provided with a first mounting plate, and the top of the first mounting plate is provided with an unmanned plane control system.

[0006] As a preferred technical scheme of the utility model, it further comprises a second mounting plate, a fixed plate, a connecting rod and a compression spring, the mounting rack top is provided with the fixed plate, the fixed plate top is provided with the connecting rod, the connecting rod outer side is provided with the second mounting plate, the second mounting plate is provided with a mounting hole, the fuselage integrated support is connected to the top of the second mounting plate through the mounting hole, the connecting rod outer side is provided with the compression spring, and the compression spring is connected between the fixed plate and the second mounting plate.

[0007] As a preferred technical scheme of the utility model, the camera calibration position is further arranged on the fuselage integrated all-in-one support.

[0008] As a preferred technical scheme of the utility model, the gun mounting angle in the fuselage integrated all-in-one support is accurately calculated and adjusted, so that the muzzle is slightly raised.

[0009] As a preferred technical scheme of the utility model, the reinforcing structure is further arranged on the bottom of the two flight platform arms on the rear side.

[0010] As a preferred technical scheme of the utility model, the gun is symmetrically arranged along the central axis of the first mounting plate.

[0011] Beneficial effects: the fuselage integrated all-in-one support, the pickup dowel limit and the handle clamping mechanism are designed, the unmanned aerial vehicle and the gun are designed as an integrated structure, and the instability of the traditional external hanging type design is avoided. BRIEF DESCRIPTION OF DRAWINGS

[0012] Figure 1 It is a three-dimensional structure schematic view of the utility model.

[0013] Figure 2 It is a structure schematic view of the flight platform arm and the second mounting plate of the utility model.

[0014] Figure 3 It is a structure schematic view of the fixed plate, the connecting rod and the compression spring of the utility model.

[0015] Figure 4 It is a structure schematic view of the side of the utility model.

[0016] Marked in the figure: 1-fuselage integrated all-in-one support, 2-flight platform arm, 3-first mounting plate, 4-reinforcing structure, 5-trigger release rudder position, 6-trigger slot, 7-pickup dowel limit, 8-handle clamping mechanism, 9-camera calibration position, 10-second mounting plate, 11-fixed plate, 12-mounting hole, 13-connecting rod, 14-compression spring, 15-mounting frame. DETAILED DESCRIPTION

[0017] The utility model is described in detail below in combination with the drawings and specific embodiments, but is not as the limitation of the utility model.

[0018] An integrated unmanned aerial vehicle structure with a gun mounting function, like Figures 1-4As shown, including organic body integrated support 1 and mounting bracket 15, mounting bracket 15 top provided with organic body integrated support 1, organic body integrated support 1 for installing gun, the angle of gun installed in organic body integrated support 1 is calculated and adjusted accurately, so that the muzzle is slightly raised, which not only reduces the interference to the flight attitude of the unmanned aerial vehicle when shooting, but also effectively avoids the potential damage of gunpowder residues or hot gas to the structure of the unmanned aerial vehicle, further improves the safety and durability of the system, and the gun is symmetrically arranged along the central axis of the first mounting plate 3, so as to achieve the optimal configuration of the center of gravity, ensure that the unmanned aerial vehicle always maintains a stable attitude during flight, and further improve the reliability and operational effectiveness of the overall system, the trigger slot 6 is opened on the organic body integrated support 1, the trigger release rudder position 5 is arranged on the left side of the organic body integrated support 1, the trigger release rudder position 5 is located above the trigger slot 6, the picatinny rail limiting 7 is arranged at the front of the left end of the organic body integrated support 1, the handle clamping mechanism 8 is arranged on the rear side of the organic body integrated support 1, a plurality of flight platform arms 2 are arranged in the mounting bracket 15, the flight platform arms 2 are used for installing the aircraft, the first mounting plate 3 is arranged at the bottom of the mounting bracket 15, the unmanned aerial vehicle control system is arranged at the top of the first mounting plate 3, the aircraft is connected with the remote controller, and the unmanned aerial vehicle control system and the remote controller are electrically connected, the unmanned aerial vehicle control system and the trigger release rudder position 5 are electrically connected.

[0019] As shown in Figure 3 It also includes a second mounting plate 10, a fixed plate 11, a connecting rod 13 and a compression spring 14, the fixed plate 11 is arranged at the top of the mounting bracket 15, the connecting rod 13 is arranged at the top of the fixed plate 11, the second mounting plate 10 is sleeved outside the connecting rod 13, the mounting hole 12 is opened on the second mounting plate 10, the organic body integrated support 1 is connected at the top of the second mounting plate 10 through the mounting hole 12, the compression spring 14 is sleeved outside the connecting rod 13 and connected between the fixed plate 11 and the second mounting plate 10, when the gun is fired, the recoil force generated by the gun will make the second mounting plate 10 move downward together with the organic body integrated support 1 and the gun, the compression spring 14 will be compressed in this process, absorbing a large amount of energy, reducing the impact force directly applied to the unmanned aerial vehicle body, helping to maintain the stability of the unmanned aerial vehicle and reducing the flight attitude disturbance caused by shooting.

[0020] As shown in Figure 4 It also includes a camera calibration position 9, the camera calibration position 9 is arranged at the front end of the organic body integrated support 1, and the camera is arranged on the camera calibration position 9. By fusing the gun center with the real-time picture of the camera on the camera calibration position 9, and by making the central point of the returned picture coincide with the aiming point, the accuracy of shooting and aiming is greatly improved.

[0021] As shown in Figure 1As shown, the reinforcing structure 4 is arranged at the bottom of each flight platform arm 2 at the rear side, and the reinforcing structure 4 can mechanically transmit the rearward force to the rear of the aircraft, thereby further improving the stability of the unmanned aerial vehicle.

[0022] In use, the gun is pre-installed on the fuselage integrated support 1, and the picatinny rail limiting 7 and the handle clamping mechanism 8 are locked by screws, respectively, to the gun, and then the aircraft is powered on and waits for the unmanned aerial vehicle control system to self-check. After the self-checking is completed, the ground gun calibration is started (a target paper is placed ten meters in front of the aircraft, a shot is observed, the lens angle is adjusted, and the above operation is repeated until the impact point reaches the required standard), and then the camera calibration position 9 is adjusted to determine that the bullet impact point and the crosshair (i.e. the gun center) in the flight goggles are in the same position. Subsequently, the camera calibration position 9 screw can be locked to ensure stable operation in subsequent use; after the ground calibration is completed, the remote controller can be used to unlock the aircraft and take off. When the crosshair position in the flight goggles falls on the target, the remote controller lever is turned, and the unmanned aerial vehicle control system sends a signal to the trigger release rudder, and the trigger is pulled through the trigger slot 6 to complete the trigger.

[0023] Those skilled in the art should understand that the above embodiments do not limit the utility model in any form, and any technical solution obtained by equivalent replacement or equivalent transformation falls within the protection scope of the utility model.

Claims

1. An integrated unmanned aerial vehicle structure with a gun mounting function, comprising a fuselage integrated support (1) and a mounting bracket (15), the top of the mounting bracket (15) is provided with the fuselage integrated support (1), characterized in that: The machine body integrated support (1) is provided with a trigger slot (6), a trigger release rudder position (5) is arranged at the middle of the left side of the machine body integrated support (1), a picatinny rail limiting (7) is arranged at the front of the left end of the machine body integrated support (1), a handle clamping mechanism (8) is arranged at the rear side of the machine body integrated support (1), a plurality of flight platform arms (2) are arranged in the mounting frame (15), a first mounting plate (3) is arranged at the bottom of the mounting frame (15), and a UAV control system is arranged at the top of the first mounting plate (3).

2. An integrated drone structure with gun mounting function as claimed in claim 1, wherein: Further comprising a second mounting plate (10), a fixed plate (11), a connecting rod (13) and a compression spring (14), the mounting frame (15) is provided with the fixed plate (11) at the top, the connecting rod (13) is arranged at the top of the fixed plate (11), the second mounting plate (10) is sleeved outside the connecting rod (13), the mounting hole (12) is arranged on the second mounting plate (10), the machine body integrated support (1) is connected to the top of the second mounting plate (10) through the mounting hole (12), the compression spring (14) is sleeved outside the connecting rod (13), and the compression spring (14) is connected between the fixed plate (11) and the second mounting plate (10).

3. An integrated drone structure with gun mount function as claimed in claim 2 wherein: Further comprising a camera calibration position (9), the machine body integrated support (1) is provided with the camera calibration position (9) at the front end.

4. An integrated drone structure with gun mounting function as claimed in claim 3 wherein: The gun mounting angle in the machine body integrated support (1) is accurately calculated and adjusted, so that the muzzle is slightly raised.

5. An integrated drone structure with gun mount function as claimed in claim 4 wherein: Further comprising a reinforcing structure (4), the reinforcing structure (4) is arranged at the bottom of the two flight platform arms (2) at the rear side.

6. An integrated drone structure with gun mount function as claimed in claim 5 wherein: The gun is symmetrically arranged along the central axis of the first mounting plate (3).

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