Simulated missile launching unmanned aerial vehicle mount
By designing a drone to simulate bomb delivery and using wireless communication and probe devices to simulate bombing and being attacked, the safety and portability issues of drone bombing were solved, and flexible live-fire combat training simulations were realized.
Patent Information
- Application Number
- CN202520124590.2
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2025-01-20
- Publication Date
- 2025-12-26
- Estimated Expiration
- 2035-01-20
AI Technical Summary
Existing drone bombing methods pose safety risks and are difficult to meet the requirements of miniaturization and portability, thus failing to effectively simulate the diversity of live-fire combat training.
Design a simulated missile delivery drone mount, comprising a cavity shell with an open top, a main control board, a positioning module, a wireless communication module, and a smoke canister device. The wireless communication module receives the missile delivery signal, the positioning module uses feedback information to calculate the missile delivery time, and the probe receives the impact signal to trigger the smoke canister to simulate the impact state, thereby achieving simulated attack and damage effects.
It achieves miniaturization and portability of UAVs, can safely simulate bombing and being attacked, meets diverse live-fire combat training needs, reduces damage to unmanned equipment, and has strong applicability.
Smart Images
Figure CN223721177U_ABST
Abstract
Description
TECHNICAL FIELD
[0001] The utility model relates to a kind of unmanned aerial vehicle hangings, specifically to a kind of simulation bomb launching unmanned aerial vehicle hangings, belong to real soldier confrontation training technical field. BACKGROUND
[0002] With the popularization and application of real soldier confrontation training system in each training base of the army, some training equipment of hangings needs to be lightweight and miniaturized to meet the volume reduction exposed in actual simulation and carrying convenience etc.
[0003] With the improvement of some training requirements, new war mode also changes with time, and new unmanned aerial vehicle has become the most economical and effective way in confrontation. Therefore, the simulation confrontation training of miniaturized unmanned aerial vehicle needs to be fully trained.
[0004] The common unmanned aerial vehicle host machine bomb launching in market adopts bomb launching simulation, which has certain danger to personnel from high altitude, so a new simulation bomb launching mode is needed to replace physical bomb launching. SUMMARY
[0005] To solve the deficiency of prior art, the purpose of the utility model is to provide a kind of simulation bomb launching unmanned aerial vehicle hangings.
[0006] To achieve the above goal, the utility model adopts the following technical solutions:
[0007] A kind of simulation bomb launching unmanned aerial vehicle hangings, including the cavity shell of top face open mouth, the top opening of the shell is equipped with matching cover plate, the cover plate is used for hanging unmanned aerial vehicle;
[0008] The shell is equipped with main control board, and with the positioning module, wireless communication module connected with main control board;
[0009] The bottom of the shell is equipped with probe device and smoke tank device matched with main control board,
[0010] Through wireless communication module, main control board is used to transmit the positioning information fed back by positioning module to remote terminal after receiving bomb launching signal, and the remote terminal calculates the time required from bomb launching to missile landing according to positioning information, to simulate attack state;
[0011] The main control board is used to trigger smoke tank device to simulate hit state after receiving the hit signal received by probe device.
[0012] The above-mentioned probe device includes a plurality of probes provided with shell bottom surface and bottom side surface, and the probe is used to receive hit signal, including laser signal, infrared signal.
[0013] The wireless communication module includes any one of a 4G module, a 5G module, a Wi-Fi module and a data radio module.
[0014] Further, the bottom of the shell is provided with an antenna connected to the wireless communication module.
[0015] The side of the shell is provided with a display screen connected to the main control board and parameter setting buttons for setting and displaying parameters, and the parameters include ammunition types and ammunition quantities.
[0016] The utility model has the advantages that:
[0017] The utility model discloses a simulation ammunition launching unmanned aerial vehicle mounting, through the positioning module determines and feedback longitude, latitude and height state information, and according to height calculation bombarding to the time of ammunition explosion, simulation bombarding, according to longitude, latitude and ammunition type calculation damage effect.
[0018] The utility model discloses a simulation ammunition launching unmanned aerial vehicle mounting, small, light in weight, convenient to carry, can be mounted under unmanned aerial vehicle at any time, convenient to use, flexible, still can be used with air defense missile and so on counter training system, can simulate being damaged, can also simulate long-range bombarding attack, safe and reliable, will not cause harm to unmanned equipment, better meet the real soldier counter scenario, can satisfy more daily different types of training, have very strong practicality and extensive applicability. BRIEF DESCRIPTION OF DRAWINGS
[0019] Figure 1 It is structure schematic diagram of simulation ammunition launching unmanned aerial vehicle mounting.
[0020] The meanings of the marks in the drawings are as follows: 1, shell, 2, cover plate, 3, probe, 4, smoke emitting seat, 5, main board, 6, wireless communication module, 7, battery, 8, connecting shaft, 9, antenna, 10, parameter setting button. DETAILED DESCRIPTION
[0021] The utility model will be specifically introduced in connection with the drawings and specific embodiment.
[0022] A simulation ammunition launching unmanned aerial vehicle mounting is composed of a shell 1, a probe 32, a main control board, a positioning module, a wireless communication module 6, a probe device and a smoke tank device.
[0023] The shell 1 is provided with a cavity and an open top surface, the probe 32 is matched with the open surface, and the probe 32 is provided with a plurality of connecting shafts 8 for mounting the unmanned aerial vehicle.
[0024] The main control board, the positioning module and the wireless communication module 6 are all arranged in the cavity of the shell 1, and the positioning module and the wireless communication module 6 are connected to the main control board. The battery 7 supplies power through the main control board.
[0025] Preferably, the wireless communication module 6 can be selected from any one of a 4G module, a 5G module, a Wi-Fi module, a data radio module, etc.; the positioning module can be selected from any one of a GPS positioning module, a Beidou positioning module, a GLONASS positioning module, a Galileo positioning module, etc., for determining longitude, latitude and height state information.
[0026] The bottom surface and the bottom side surface of the shell 1 are provided with a probe device, so as to Figure 1 As shown in the figure, the bottom side surface is an inclined surface connecting between the bottom surface and the side surface. The probe device is composed of a plurality of probes for receiving impact signals from various angular directions, and the impact signals can be laser signals or infrared signals according to the signal emission source of the weapon.
[0027] The smoke can device is composed of a smoke emitting seat 4 and a smoke can, and the smoke can is fixedly arranged on the bottom of the shell 1 through the smoke emitting seat 4. The smoke can is connected to the main control board and is of an electronic trigger type.
[0028] In order to enhance the wireless signal, the bottom of the shell 1 is provided with an antenna 9 connected to the wireless communication module 6.
[0029] Impact mode:
[0030] The shell is mounted and flies to the target area with the unmanned aerial vehicle, and the wireless communication module 6 is used. After the main control board receives the bomb-throwing signal from the remote terminal, the state information (longitude, latitude and height) fed back by the positioning module and the ammunition information (ammunition type and ammunition quantity) carried by the shell are fed back to the remote terminal.
[0031] The remote terminal calculates the time required from the start of bomb-throwing to the landing of the missile according to the height information, and collects the positioning information of the personnel covered in the ammunition explosion simulation range according to the longitude and latitude, so as to simulate the attack and damage.
[0032] Impact mode:
[0033] The main control board is used to trigger the smoke can device after receiving the impact signal received by the probe device, so as to simulate the state of being hit, so as to simulate the real damage effect.
[0034] Preferably, the control device feeds back the impact information to the remote terminal.
[0035] In order to facilitate the setting of the ammunition, the side surface of the shell 1 is provided with a display screen and a parameter setting button 10 connected to the main control board, which is used for setting and displaying parameters, and the parameters include ammunition type and ammunition quantity.
[0036] The basic principle, main features and advantages of the present application are shown and described above. The skilled in the art should understand that the above examples do not limit the present application in any form, and any technical solution obtained by equivalent replacement or equivalent transformation falls within the protection scope of the present application.
Claims
1. A simulated munition delivery UAV payload, characterized by, The cavity shell includes a top opening, and the top opening is provided with a matched cover plate for mounting a UAV. The shell is provided with a main control board, a positioning module and a wireless communication module connected with the main control board. The bottom of the shell is provided with a probe device and a smoke tank device connected with the main control board. After receiving a bomb signal, the main control board transmits the positioning information fed back by the positioning module to a remote terminal, and the remote terminal calculates the time required from the start of bomb to the landing of the missile according to the positioning information to simulate an attack state. After receiving a strike signal received by the probe device, the main control board triggers the smoke tank device to simulate a struck state.
2. The UAV mount of claim 1, wherein, The probe device includes a plurality of probes provided with a bottom surface and a bottom side surface of the shell, and the probes are used to receive strike signals including laser signals and infrared signals.
3. The UAV mount of claim 1, wherein, The wireless communication module includes any one of a 4G module, a 5G module, a Wi-Fi module and a data transmission radio module.
4. The UAV mount of claim 3, wherein, The bottom of the shell is provided with an antenna connected with the wireless communication module.
5. The UAV mount of claim 1, wherein, The side surface of the shell is provided with a display screen and a parameter setting button connected with the main control board, which are used to set and display parameters including ammunition types and quantities.