UAV and its gun mount
By designing a gun mounting frame on the drone, using the weapon mount connector and the controlled weapon rack to connect with the landing gear reinforcement pipe of the drone, the problem of poor installation reliability of the drone gun barrel is solved and more stable and lightweight artillery installation improves the overall performance of the drone.
Patent Information
- Application Number
- CN202010179511.X
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- Filing Date
- 2020-03-13
- Publication Date
- 2025-02-14
- Estimated Expiration
- 2040-03-13
AI Technical Summary
The installation reliability of the gun barrel on the drone is mainly because the gun barrel is only connected to the base under the fuselage through the mounting frame, and the connection position is small, resulting in unstable installation.
Design a gun mount for a drone, which is fixed to the side of the drone's fuselage through a weapon mount connector, and is fixedly connected to the landing gear reinforcement pipe of the drone through a controlled weapon mount to ensure the connection between the two locations. , improve installation reliability.
By adding connection points, the gun barrel is ensured to be reliably installed on the drone, which improves the stability and safety of installation, while reducing the weight of the gun mount and improving the overall performance of the drone.
Smart Images

Figure CN111204461B_ABST
Abstract
Description
Technical Field
[0001] The present invention relates to the technical field of aircraft, and more specifically, to a gun mounting bracket for an unmanned aerial vehicle and also to an unmanned aerial vehicle. Background Art
[0002] The gun barrels on the drone are directly installed under the drone fuselage and installed in parallel. However, the gun barrels are only connected to the base under the fuselage through the mounting frame, with few connection positions and poor installation reliability. Therefore, how to reliably assemble the gun barrels on the drone is a problem that needs to be solved urgently by those skilled in the art. Summary of the invention
[0003] In view of this, the present invention provides a gun mounting frame for a drone, wherein the weapon mounting frame connector is used to be fixed on the side of the drone fuselage, and the control weapon frame of the gun mounting frame is fixedly connected to the landing gear reinforcement pipe of the drone, that is, the gun mounting frame is connected to two positions of the drone respectively to ensure reliable installation. The present invention also provides a drone, which uses the above-mentioned gun mounting frame to ensure reliable installation of the gun barrel.
[0004] To achieve the above object, the present invention provides the following technical solutions:
[0005] A gun mounting frame for an unmanned aerial vehicle, comprising:
[0006] A gun barrel clamp, wherein the gun barrel clamp is fixed on a controlled weapon rack; the controlled weapon rack is fixedly connected to a landing gear reinforcement tube of the UAV;
[0007] A gun barrel clamp cover, the gun barrel clamp cover is used to cooperate with the gun barrel clamp to clamp and fix the gun barrel; the gun barrel clamp cover is fixedly connected to the gun barrel clamp through a fixing piece;
[0008] A weapon rack connector, wherein the weapon rack connector is fixedly connected to the controlled weapon rack, and the weapon rack connector is used to be fixed on the side of the fuselage of the drone.
[0009] Preferably, in the above-mentioned artillery mounting bracket, the lower end of the controlled weapon rack is connected to a fixed connector, and the fixed connector is fixedly connected to the landing gear reinforcement tube via a connecting column.
[0010] Preferably, in the above-mentioned artillery mounting bracket, the two ends of the connecting column are respectively plug-fitted with the fixed connector and the landing gear reinforcement tube; the outer diameter of the connecting column is equal to the inner diameter of the insertion hole of the fixed connector and the inner diameter of the insertion hole of the landing gear reinforcement tube.
[0011] Preferably, in the above-mentioned artillery mounting bracket, both ends of the connecting column are fixedly connected to the fixed connector and the landing gear reinforcement tube through fixing parts respectively.
[0012] Preferably, in the above-mentioned artillery mounting bracket, the gun barrel clamp and the gun barrel clamp cover are fixed to each other to form a clamp assembly, and the clamp assembly is divided into two groups.
[0013] Preferably, in the above-mentioned artillery mounting bracket, the gun barrel clamp is a block structure with a preset height, one end of the gun barrel clamp along the height direction is fixedly connected to the controlled weapon rack, and the other end of the gun barrel clamp along the height direction is provided with an arc-shaped notch for fitting the gun barrel; the gun barrel clamp cover is arc-shaped for fitting the outer wall of the gun barrel.
[0014] Preferably, in the above-mentioned artillery mounting bracket, the weapon rack connector is fixedly connected to the controlled weapon rack via a fixing piece, and the weapon rack connector is used to be fixed to the side of the fuselage of the UAV via a fixing piece.
[0015] A drone comprises a gun mounting frame, wherein the gun mounting frame is the gun mounting frame described in any one of the above technical solutions.
[0016] Preferably, in the above-mentioned UAV, a mounting plate is fixed on the fuselage of the UAV, and the weapon rack connector is fixed to the mounting plate via a fixing member.
[0017] Preferably, in the above-mentioned UAV, the UAV is a crossed twin-rotor unmanned helicopter.
[0018] The invention provides a gun mounting frame for an unmanned aerial vehicle, comprising a gun barrel clamp, a gun barrel clamp cover and a weapon rack connector; the gun barrel clamp is fixed on a controlled weapon rack; the controlled weapon rack is fixedly connected to a landing gear reinforcement pipe of the unmanned aerial vehicle; the gun barrel clamp cover is used for cooperating with the gun barrel clamp and clamping and fixing the gun barrel; the gun barrel clamp cover is fixedly connected to the gun barrel clamp through a fixing piece; the weapon rack connector is fixedly connected to the controlled weapon rack, and the weapon rack connector is used for fixing to a side of a fuselage of the unmanned aerial vehicle.
[0019] In the gun mounting frame of the UAV provided by the present invention, the weapon rack connector is used to be fixed on the side of the fuselage of the UAV, and the controlled weapon rack of the gun mounting frame is fixedly connected to the landing gear reinforcement pipe of the UAV, that is, the gun mounting frame is connected to the UAV at two positions to ensure that the gun barrel is reliably installed.
[0020] The present invention also provides a UAV, which uses the above-mentioned gun mounting bracket to ensure reliable assembly of the gun barrel. BRIEF DESCRIPTION OF THE DRAWINGS
[0021] In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings required for use in the embodiments or the description of the prior art will be briefly introduced below. Obviously, the drawings described below are only some embodiments of the present invention. For ordinary technicians in this field, other drawings can be obtained based on these drawings without paying creative work.
[0022] Figure 1 A schematic diagram of the three-dimensional structure of a gun mounting frame of a UAV provided in an embodiment of the present invention;
[0023] Figure 2 A schematic diagram of the side view structure of a gun mounting frame of a UAV provided in an embodiment of the present invention;
[0024] in, Figure 1-Figure 2 middle:
[0025] Gun barrel 1; gun barrel clamp 2; controlled weapon rack 3; gun barrel clamp cover 4; fixed connector 5; connecting column 6; weapon rack connector 7; landing gear reinforcement tube 8. DETAILED DESCRIPTION
[0026] The embodiment of the present invention discloses a gun mounting frame for a drone, wherein the weapon mounting frame connector is used to be fixed on the side of the drone fuselage, and the control weapon frame of the gun mounting frame is fixedly connected to the landing gear reinforcement pipe of the drone, that is, the gun mounting frame is connected to two positions of the drone respectively to ensure reliable installation. The embodiment of the present invention also discloses a drone, which uses the above-mentioned gun mounting frame to ensure reliable installation of the gun barrel.
[0027] The following will be combined with the drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the present invention.
[0028] See also Figure 1-Figure 2 An embodiment of the present invention provides a gun mounting frame for an unmanned aerial vehicle, comprising a gun barrel card 2, a gun barrel card cover 4 and a weapon rack connector 7; the gun barrel card 2 is fixed on a controlled weapon rack 3; the controlled weapon rack 3 is fixedly connected to a landing gear reinforcement tube 8 of the unmanned aerial vehicle; the gun barrel card cover 4 is used to cooperate with the gun barrel card 2 and clamp and fix the gun barrel 1; the gun barrel card cover 4 is fixedly connected to the gun barrel card 2 through a fixing piece; the weapon rack connector 7 is fixedly connected to the controlled weapon rack 3, and the weapon rack connector 7 is used to be fixed to the side of the fuselage of the unmanned aerial vehicle.
[0029] In the gun mounting bracket of the UAV provided in the embodiment of the present invention, the weapon rack connector 7 is used to be fixed on the side of the fuselage of the UAV, and the controlled weapon rack 3 of the gun mounting bracket is fixedly connected to the landing gear reinforcement tube 8 of the UAV, that is, the gun mounting bracket is connected to the UAV at two positions. Compared with the installation method of the gun barrel 1 in the prior art, it can ensure that the gun barrel 1 is reliably installed.
[0030] In addition, the gun barrel in the prior art is installed at the bottom of the UAV fuselage. Since the gun barrel will generate fire when firing, the gun barrel should be installed below the UAV away from the engine and the oil circuit, resulting in the gun barrel being away from the base of the UAV at the bottom, causing the mounting frame to be a certain distance away from the base. This situation makes the entire gun barrel mounting frame relatively heavy, affecting the flight performance of the UAV. The gun mounting frame provided in this embodiment is installed on the side of the fuselage, away from the engine and the oil circuit at the bottom of the UAV, has a simpler structure and is lighter in weight, which is conducive to improving the overall performance of the UAV.
[0031] In the above-mentioned artillery mounting frame, the lower end of the controlled weapon frame 3 is connected with a fixed connector 5, and the fixed connector 5 is fixedly connected to the landing gear reinforcement tube 8 through a connecting column 6. The two ends of the connecting column 6 are respectively plugged and matched with the fixed connector 5 and the landing gear reinforcement tube 8; the outer diameter of the connecting column 6 is equal to the inner diameter of the plug-in hole on the fixed connector 5 that matches the connecting column 6, and the inner diameter of the plug-in hole on the landing gear reinforcement tube 8 that matches the connecting column 6. The two ends of the connecting column 6 are respectively fixedly connected to the fixed connector 5 and the landing gear reinforcement tube 8 through fixing parts, and the fixing parts are screws, and the screws are tightened by aviation anti-loosening nuts.
[0032] The barrel clamp 2 and the barrel clamp cover 4 are fixed to each other to form a clamp assembly. Preferably, in the gun mounting frame provided by the above embodiment, the clamp assembly is two groups, so that the recoil force of the barrel 1 after firing will not change the initial position of the barrel 1, so as to greatly improve the firing accuracy. In the clamp assembly, the barrel clamp 2 is connected to the barrel clamp cover 4 by screws and aviation lock nuts that cooperate with each other. The connection between the barrel clamp 2 and the barrel clamp cover 4 can be freely adjusted to ensure that the outer part of the barrel 1 will not be damaged by excessive pressure from the clamp assembly. The screw mounting holes of the barrel clamp 2 and the barrel clamp cover 4 in the clamp assembly are respectively designed at the connecting ears of the end. This structure can ensure convenient installation and does not affect the assembly of the barrel 1. The barrel clamp 2 is fixedly connected to the controlled weapon rack 3 by screws; the upper end of the controlled weapon rack 3 is fixedly connected to the weapon rack connector 7 by screws, and the barrel clamp 2 and the weapon rack connector 7 are located on both sides of the controlled weapon rack 3; the lower end of the controlled weapon rack 3 is fixedly connected to the fixed connector 5 by screws.
[0033] The barrel card 2 is a block structure with a preset height. One end of the barrel card 2 along the height direction is fixedly connected to the controlled weapon rack 3 by screws. The other end of the barrel card 2 along the height direction is provided with an arc-shaped notch, which is used to fit the barrel 1. The barrel card cover 4 is arc-shaped and is used to fit the outer wall of the barrel 1. The barrel card 2 is provided with a threaded hole that cooperates with the screw connecting the barrel card 2 and the controlled weapon rack 3. The threaded hole is arranged at a position with a larger size in the height direction on the barrel card 2, so that the length of the screw is set to be longer to adapt to the larger recoil force when the barrel 1 is fired, and the screw is prevented from affecting the installation of the barrel 1.
[0034] The weapon rack connector 7 is fixedly connected to the controlled weapon rack 3 through a fixing piece, and the weapon rack connector 7 is used to be fixed to the side of the fuselage of the UAV through the fixing piece.
[0035] As provided in the above embodiment, the barrel card 2 is connected to the controlled weapon rack 3 through the threaded hole at the upper end, the controlled weapon rack 3 is fixed to the weapon rack connector 7 through the threaded hole at the upper end, the controlled weapon rack 3 is fixed to the fixed connector 5 through the threaded hole at the lower end, the fixed connector 5 is connected to the landing gear reinforcement tube 8 through the connecting column 6, and the weapon rack connector 7 is directly connected to the side of the body, so that it is directly connected to the drone by a rigid connection. The arc size of the barrel card 2 and the barrel card cover 4 is adapted to the barrel 1, ensuring that the barrel 1 is tightly fixed on the drone.
[0036] In the gun mounting frame provided by the above embodiment, each fixing part is a screw, and each screw is fastened by an aviation lock nut. The two parts connected by the screw are respectively provided with threaded holes adapted to the screws. Specifically, the upper end of the gun barrel clamp 2 has a threaded hole, and the controlled weapon rack 3 is provided with a threaded hole of the same size as the gun barrel clamp 2; the upper end of one side of the controlled weapon rack 3 is provided with three screw holes of the same size, and one end of the weapon rack connector 7 is also provided with threaded holes of the same size and number; the lower end of one end of the controlled weapon rack 3 is provided with two screw holes of the same size, and one end of the fixed connector 5 is also provided with threaded holes of the same size and number. The outer circle radius of the fixed connector 5 is exactly equal to the inner circle radius of the lower end of the controlled weapon rack 3, and can be directly inserted into the controlled weapon rack 3, and then fastened and connected by screws and aviation lock nuts; threaded holes of the same size are provided at both ends of the connecting column 6. The barrel card 2 and the barrel card cover 4 are fixedly connected by screws and aviation nuts; the barrel card 2 and the controlled weapon rack 3 are fixedly connected by screws; the controlled weapon rack 3 and the weapon rack connector 7 are fixed by screws and aviation anti-loosening nuts; the controlled weapon rack 3 and the fixed connector 5 are fixed by screws and aviation anti-loosening nuts; the fixed connector 5 and the connecting column 6 are fixed by screws and aviation anti-loosening nuts; the connecting column 6 and the landing gear reinforcement tube 8 are fixed by screws and aviation anti-loosening nuts; through the above-mentioned settings, the space and weight occupied by the artillery mounting frame are effectively reduced, and the overall performance of the UAV is further improved.
[0037] The weapon rack connector 7 and the landing gear reinforcement tube 8 have a certain position difference in space, and the position difference depends on the body width of the helicopter.
[0038] The gun barrel 1, the gun barrel clamp 2, the controlled weapon rack 3, the gun barrel clamp cover 4, the fixed connector 5, the connecting column 6, the weapon rack connector 7 and the landing frame reinforcement tube 8 are parts made of rigid materials respectively.
[0039] In the unmanned helicopter gun mounting frame provided by the embodiment of the present invention, different components are rigidly connected respectively, which can ensure the firmness of the installation of the gun barrel 1 and avoid the initial installation position of the gun barrel 1 being affected by flight vibration and gun recoil, thereby preventing the gun barrel 1 from reducing the firing accuracy; at the same time, the gun mounting frame directly fixes the gun barrel 1 tightly to the unmanned aerial vehicle through only seven rigid materials, occupies less space, simplifies the structure, reduces weight, and improves the overall performance of the unmanned aerial vehicle.
[0040] The embodiment of the present invention further provides an unmanned aerial vehicle, comprising a gun mounting frame, wherein the gun mounting frame is the gun mounting frame provided in the above embodiment. Specifically, the rack connector 7 is fixed to the left side of the unmanned aerial vehicle. A mounting plate is fixed to the fuselage of the unmanned aerial vehicle, and the weapon rack connector 7 is fixed to the mounting plate by a fixing member; the mounting plate has a threaded hole, and the threaded hole is the same size as the threaded hole of the weapon rack connector 7. The mounting plate and the weapon rack connector 7 are preferably connected by bolts to improve the connection stability between the weapon rack connector 7 and the unmanned aerial vehicle.
[0041] The above-mentioned UAV is an unmanned helicopter, specifically a crossed twin-rotor unmanned helicopter.
[0042] The drone provided in this embodiment uses the gun mounting frame provided in the above embodiment to ensure reliable installation of the gun barrel 1. Of course, the drone provided in this embodiment also has other effects of the gun mounting frame provided in the above embodiment, which will not be repeated here.
[0043] The various embodiments in this specification are described in a progressive manner, and each embodiment focuses on the differences from other embodiments. The same or similar parts between the various embodiments can be referenced to each other.
[0044] The above description of the disclosed embodiments enables one skilled in the art to implement or use the present invention. Various modifications to these embodiments will be apparent to one skilled in the art, and the general principles defined herein may be implemented in other embodiments without departing from the spirit or scope of the present invention. Therefore, the present invention will not be limited to the embodiments shown herein, but rather to the widest scope consistent with the principles and novel features disclosed herein.
Claims
1. A gun mounting frame for an unmanned aerial vehicle, characterized in that: include: A gun barrel clamp, wherein the gun barrel clamp is fixed on a controlled weapon rack; the controlled weapon rack is fixedly connected to a landing gear reinforcement tube of the UAV; A gun barrel clamp cover, the gun barrel clamp cover is used to cooperate with the gun barrel clamp to clamp and fix the gun barrel; the gun barrel clamp cover is fixedly connected to the gun barrel clamp through a fixing piece; A weapon rack connector, the weapon rack connector is fixedly connected to the controlled weapon rack, and the weapon rack connector is used to be fixed on the side of the fuselage of the UAV; The lower end of the controlled weapon rack is connected with a fixed connector, and the fixed connector is fixedly connected to the landing gear reinforcement tube through a connecting column; The two ends of the connecting column are respectively plugged and matched with the fixed connector and the landing gear reinforcement tube; the outer diameter of the connecting column is equal to the inner diameter of the insertion hole of the fixed connector and the inner diameter of the insertion hole of the landing gear reinforcement tube; The two ends of the connecting column are fixedly connected to the fixed connector and the landing gear reinforcement tube through fixing pieces respectively; The barrel clamp and the barrel clamp cover are fixed to each other to form a clamp assembly, and the clamp assembly is divided into two groups; The weapon rack connector is fixedly connected to the controlled weapon rack via a fixing piece, and the weapon rack connector is used to be fixed to the side of the fuselage of the UAV via a fixing piece.
2. The gun mounting bracket according to claim 1, characterized in that: The gun barrel clamp is a block structure with a preset height. One end of the gun barrel clamp along the height direction is fixedly connected to the controlled weapon rack, and the other end of the gun barrel clamp along the height direction is provided with an arc-shaped notch for fitting the gun barrel; the gun barrel clamp cover is arc-shaped for fitting the outer wall of the gun barrel.
3. An unmanned aerial vehicle, comprising a gun mounting frame, characterized in that: The artillery mounting bracket is the artillery mounting bracket described in any one of claims 1-2.
4. The drone according to claim 3, characterized in that: A mounting plate is fixed on the fuselage of the UAV, and the weapon rack connector is fixed to the mounting plate via a fixing piece.
5. The drone according to claim 3, characterized in that: The unmanned aerial vehicle is a crossed twin-rotor unmanned helicopter.
Citation Information
Patent Citations
Cruising and fire-fighting integrated unmanned aerial vehicle
CN107875540A
Emission gun and unmanned aerial vehicle
CN109665104A
Unmanned aerial vehicle and artillery mounting rack thereof
CN211766324U