Short-range unmanned aerial vehicle simulator
The near-range drone simulator addresses the limitation of existing simulators by incorporating advanced wind simulation systems, enhancing pilot training in realistic environments to improve drone operation skills and adaptability.
Patent Information
- Application Number
- CN202422001905.2
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-08-19
- Publication Date
- 2025-07-15
- Estimated Expiration
- 2034-08-19
AI Technical Summary
The existing drone simulator cannot truly simulate different wind directions and environments, and cannot directly cooperate with real drones for training, resulting in poor training results.
A short-range drone simulator is designed, including a circumference room and a direct room, with a hair dryer and a swinging air duct to simulate various airflow environments, and a control panel and display screen to achieve simulation training of the real environment.
Effectively simulate various airflow environments, improve drone control capabilities and adaptability, and enhance training effects.
Smart Images

Figure CN223108444U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the technical field of unmanned aerial vehicle simulation, in particular to a short-range unmanned aerial vehicle simulator. Background Art
[0002] At present, the unmanned aerial vehicle simulation teaching device is an indispensable auxiliary device in the simulation learning of unmanned aerial vehicle driving, and is widely used in the operation and driving of unmanned aerial vehicles. The operator sits on the seat and simulates the operation of the console to achieve the effect of simulation learning.
[0003] The utility model patent with the publication number of CN210515755U proposes a unmanned aerial vehicle flight simulator, which includes a simulation room body. The left and right ends and the front and rear ends of the inner side of the simulation room body are respectively fixedly connected with a first blowing housing and a second blowing housing. The upper and lower sides of the inside of the first blowing housing and the second blowing housing are respectively fixedly connected with fixing rods. One side of the fixing rod is fixedly connected with a motor, and one side of the motor is connected with a blowing fan blade through a motor shaft. Ventilation holes are respectively arranged on one side of the first blowing housing and the second blowing housing. Through the blowing housing on the simulation room body and the blowing fan blades in the blowing housing, the utility model can blow out winds in different directions from the left and right sides and the front and rear sides, so as to train the personnel in the flight of unmanned aerial vehicles under real different wind directions. This training method is closer to reality, can effectively improve the training effect, and is beneficial to the more practical use of a unmanned aerial vehicle flight simulator.
[0004] However, the above technical solution can only simulate the operation of the unmanned aerial vehicle through virtual driving, and the simulation of the real environment is insufficient. Moreover, it cannot be directly combined with real unmanned aerial vehicles for training, and the operation of unmanned aerial vehicles in different wind directions in the environment cannot be further trained, and different flight environments cannot be simulated.
[0005] Therefore, a short-range unmanned aerial vehicle simulator is proposed. Summary of the Invention
[0006] The purpose of the utility model is to provide a short-range unmanned aerial vehicle simulator to solve the problems raised in the above background art.
[0007] To achieve the above purpose, the utility model provides the following technical solutions:
[0008] A short-range unmanned aerial vehicle simulator includes a simulation room, which is composed of a circumferential flight room and a straight flight room, and the two are communicated;
[0009] A console is arranged at the center of the inside of the circumferential flight room, and a set of unmanned aerial vehicles for short-range training is placed on the console;
[0010] Inner walls are provided in both the circumferential flight room and the straight flight room, and a double-layer structure is formed, and a communicating installation space is left between the layers;
[0011] There is a hair dryer for orbiting flight training in the installation space of the orbiting flight room;
[0012] There is a side hair dryer and a front hair dryer for high and low flight training in the installation space of the straight flight room. There is a swinging air duct cooperating with the side hair dryer on the inner wall of the straight flight room. The swinging air duct is provided with a swinging device, and there is a straight air duct cooperating with the front hair dryer on the inner wall of the straight flight room.
[0013] Furthermore, a simulated seat is provided inside the orbiting flight room, which is convenient for sitting down to control the drone.
[0014] Furthermore, the console is provided with a display screen and a convex part for conveniently placing the drone set.
[0015] Furthermore, the drone set includes a drone body and a remote controller.
[0016] Furthermore, there is an entrance on the inner wall of the orbiting flight room, and the orbiting flight room is provided with a notch cooperating with the entrance, which is convenient for entering the simulator for simulation training.
[0017] Furthermore, there is an air duct on the inner wall of the orbiting flight room, and the output end of the hair dryer extends into the air duct, which is convenient for blowing air during orbiting flight to simulate the wind flow situation.
[0018] Furthermore, the swinging device includes a swinging motor and a swinging plate. The swinging motor is arranged at the top of the outlet of the swinging air duct, the swinging plate is arranged at the outlet of the swinging air duct, and the output end of the swinging motor penetrates into the swinging air duct to be connected with the swinging plate, driving the swinging plate to swing, simulating the air flow disorder, which is convenient for training.
[0019] Furthermore, the orbiting flight room is circular, and the straight flight room is rectangular.
[0020] Furthermore, the inner wall of the straight flight room is rectangular, and the inner wall of the orbiting flight room is circular.
[0021] Furthermore, a high - flying wall and a low - flying wall are successively arranged between the inner walls of the straight flight room. The high - flying wall is provided with a high - passing port, and the low - flying wall is provided with a low - passing port. The swinging air duct at the front end of the high - flying wall is flush with the high - passing port, and the swinging air duct of the low - flying wall is flush with the low - passing port, which can simulate the air flow encountered during high - flying and low - flying, and is convenient for training.
[0022] Compared with the prior art, the beneficial effects of the present utility model are:
[0023] The present utility model adopts a design that simulates various air flows encountered during the flight of the drone. Cooperating with the control of the drone for live simulation, it can effectively restore and experience the real environment, and improve the control ability of the drone and the ability to respond to emergencies. Description of the Drawings
[0024] Figure 1 is a top - view structural schematic diagram of the present utility model;
[0025] Figure 2 is a structural schematic diagram of the swinging air duct of the present utility model;
[0026] Figure 3 is a structural schematic diagram of the console of the present utility model;
[0027] Figure 4 is a structural schematic diagram of the high - flying wall of the present utility model;
[0028] Figure 5 is a structural schematic diagram of the low - flying wall of the present utility model;
[0029] Figure 6 is a side - view sectional schematic diagram of the high - flying wall and the low - flying wall of the present utility model;
[0030] Figure 7 is a schematic diagram of the unmanned aerial vehicle of the present utility model. Specific embodiments
[0031] Next, the technical solutions in the embodiments of the present utility model will be clearly and completely described in conjunction with the accompanying drawings in the embodiments of the present utility model.
[0032] Embodiment 1:
[0033] Please refer to Figure 1-7 , the present utility model provides a technical solution:
[0034] A short - range unmanned aerial vehicle simulator includes a simulation room, which is composed of a circumferential - flight room 1 and a straight - flight room 9, and the two are connected to facilitate the switching of flight training items at any time. For the convenience of unmanned aerial vehicle training, a console 7 is provided at the center inside the circumferential - flight room 1, and at the same time, a set of unmanned aerial vehicles 8 for short - range training is placed on the console 7 for easy access to unmanned aerial vehicle training;
[0035] Inner walls 2 are provided in both the circumferential - flight room 1 and the straight - flight room 9, forming a double - layer structure at this time, strengthening the sound insulation effect and safety performance. A connected installation space 101 is left between the layers to facilitate the installation of matching components, such as various hair dryers, etc.;
[0036] A hair dryer 3 for circumferential - flight training is installed in the installation space 101 located in the circumferential - flight room 1 to facilitate blowing during circumferential - flight training in the circumferential - flight room 1 to simulate the airflow environment;
[0037] In the installation space 101 located in the straight flight room 9, a side blower 10 and a front blower 12 for high and low flight training are set up, which can simulate the environment of direct airflow and side airflow. In order to achieve the disordered airflow state during flight, a swinging air duct 11 that cooperates with the side blower 10 is installed on the inner wall 2 of the straight flight room 9. At the same time, a swinging device is set on the swinging air duct 11 to simulate the disordered airflow with the swinging device, which is convenient for training. A straight air duct 13 that cooperates with the front blower 12 is installed on the inner wall 2 of the straight flight room 9, and training is carried out in the way of direct frontal blowing to simulate the environment during headwind flight;
[0038] For better cooperation in training, the circumferential flight room 1 is circular, the straight flight room 9 is rectangular, the inner wall 2 of the straight flight room 9 is rectangular, and the inner wall 2 of the circumferential flight room 1 is circular.
[0039] As Figure 1 shown:
[0040] For the comfort of the operator, a simulated seat 6 is installed inside the circumferential flight room 1 to facilitate the operator to sit down and operate.
[0041] As Figure 1 shown:
[0042] The control console 7 is provided with a display screen 81 and a protrusion for conveniently placing the unmanned aircraft group 8. The unmanned aircraft group 8 includes an unmanned aircraft body and a remote controller, which can display the picture of the unmanned aircraft flying, facilitating the viewing of the surrounding environment and the actual situation of the unmanned aircraft flying during training. At the same time, the protruding part can place the unmanned aircraft and the supporting remote controller when not in use.
[0043] As Figure 1 shown:
[0044] For convenient access to training, an entrance 5 is opened on the inner wall 2 of the circumferential flight room 1, and at the same time, a notch is opened in the circumferential flight room 1 to cooperate with the entrance 5.
[0045] As Figure 1 shown:
[0046] An air duct 4 is set on the inner wall 2 of the circumferential flight room 1, and the output end of the blower 3 is extended into the air duct 4, which is convenient for blowing out the airflow state simulated by the airflow when the unmanned aircraft is flying in a circular motion, facilitating simulation training.
[0047] As Figure 2 shown:
[0048] Among them, the air swing device includes a swing motor 111 and a swing plate 112. The swing motor 111 is arranged at the top of the outlet of the swing air duct 11, and the swing plate 112 is arranged at the outlet of the swing air duct 11. In order to realize the swing of the swing plate 112, the output end of the swing motor 111 is inserted into the inside of the swing air duct 11 to connect the swing plate 112. Through the power output of the swing motor 111, the swing of the swing plate 112 is driven, so that the air blown by the hair dryer 10 also swings, simulating the environment of turbulent air flow.
[0049] Embodiment 2:
[0050] The difference from Embodiment 1 is that a high-flying wall 14 and a low-flying wall 15 are sequentially arranged between the inner walls 2 of the straight flight room 9 for high and low flight training. A high-through port 141 is opened on the high-flying wall 14, and a low-through port 151 is opened on the low-flying wall 15, so that the drone flies through different height through ports during flight, simulating the training environment of up and down flight. At the same time, the swing air duct 11 at the front end of the high-flying wall 14 is flush with the high-through port 141, and the swing air duct 11 on the low-flying wall 15 is flush with the low-through port 151, which is convenient for the turbulent air flow to blow the drone during high and low flight, and further trains the stability of the control technology of the operator, killing two birds with one stone.
[0051] Working principle:
[0052] The swing motor 10, the display screen 81, the console 8, and various hair dryers are electrically connected to an external power supply. Then, the motor 10, the display screen 81, and various hair dryers are connected to the console 8. The console 8 is signal-connected to an external control switch, and the console 8 is signal-connected to the drone. After the connection is completed, the console 8 can be operated using the external control switch, and the display screen 81, the swing motor 111, various hair dryers, etc. can be controlled using the console 8. The drone can be controlled using a remote control;
[0053] When it is necessary to simulate circular flight, start the hair dryer 3 (at least four are set in the circular flight room 1) to blow air and simulate the air flow. At this time, control the drone to perform circular flight to train the ability to resist air flow interference during circular flight;
[0054] When it is necessary to simulate straight flight, start the forward hair dryer 12 to blow air and simulate the air flow. Control the drone to enter the straight flight room 9 and move against the air flow to simulate the flight ability against the wind;
[0055] The side hair dryer 10 can be started to blow air on both sides of the drone to simulate the air flow and simulate the flight ability under the interference of oncoming air flow;
[0056] The swing motor 111 can be started to drive the swing plate 112 to swing, so that the air flow blown out from the side swings, simulating turbulent air flow and simulating the flight ability during turbulent air flow.
[0057] A high-flying wall 14 and a low-flying wall 15 can be sequentially arranged between the inner walls 2 of the direct flight room 9. The drone is controlled to fly high or low, so that the drone flies through different height openings during the flight process, simulating an up-and-down flight training environment. In cooperation with the side blowers 10 blowing air towards each other, it is convenient for the disordered airflow to blow the drone, and anti-disorder airflow training is inserted during the high and low flight, killing two birds with one stone;
[0058] The above simulation process can be trained separately or combined according to the training requirements;
[0059] During the flight, the camera on the drone can transmit the picture to the display screen 81, which is convenient for the operator to view the environment and convenient for training. At the same time, the operator can also sit on the simulation seat 6 to avoid fatigue;
[0060] Training in the above simulation environment is particularly suitable for short-range drones, with many simulation items and a short flight distance.
[0061] Although the embodiments of the present invention have been shown and described, those of ordinary skill in the art can understand that various changes, modifications, substitutions and variations can be made to these embodiments without departing from the principles and spirit of the present invention. The scope of the present invention is defined by the appended claims and their equivalents.
Claims
1. A short-range UAV simulator, including a simulation room, characterized in that: The simulated room is composed of a flying-around room (1) and a straight-flying room (9), and the two are connected; Inside the center of the flying-around room (1), there is a control console (7), and the control console (7) is placed with an unmanned aircraft group (8) for short-range training; Both the flying-around room (1) and the straight-flying room (9) are provided with inner walls (2), and form a double-layer structure, and there is a connected installation space (101) between the layers; In the installation space (101) of the flying-around room (1), there is a hair dryer (3) for flying-around training; In the installation space (101) of the straight-flying room (9), there is a side hair dryer (10) and a front hair dryer (12) for high-and-low flying training. On the inner wall (2) of the straight-flying room (9), there is a swinging air duct (11) that cooperates with the side hair dryer (10). The swinging air duct (11) is provided with a swinging device. On the inner wall (2) of the straight-flying room (9), there is a straight air duct (13) that cooperates with the front hair dryer (12).
2. The short-range UAV simulator according to claim 1, characterized in that: Inside the flying-around room (1), there is a simulated seat (6).
3. The short-range UAV simulator according to claim 1, characterized in that: The control console (7) is provided with a display screen (81) and an outward protrusion for conveniently placing the unmanned aircraft group (8).
4. The short-range UAV simulator according to claim 3, characterized in that: The unmanned aircraft group (8) includes an unmanned aircraft body and a remote controller.
5. A short-range UAV simulator according to claim 1, characterized in that: On the inner wall (2) of the flying-around room (1), there is an entrance (5), and the flying-around room (1) is provided with a notch that cooperates with the entrance (5).
6. The short-range UAV simulator according to claim 1, characterized in that: On the inner wall (2) of the flying-around room (1), there is an air duct (4), and the output end of the hair dryer (3) extends into the air duct (4) internally.
7. A short-range unmanned aerial vehicle simulator according to claim 1, characterized in that: The swinging device includes a swinging motor (111) and a swinging plate (112). The swinging motor (111) is arranged at the top of the outlet of the swinging air duct (11), the swinging plate (112) is arranged at the outlet of the swinging air duct (11), and the output end of the swinging motor (111) penetrates into the swinging air duct (11) internally to connect the swinging plate (112).
8. A short-range unmanned aerial vehicle simulator according to claim 1, characterized in that: The flying-around room (1) is circular, and the straight-flying room (9) is rectangular.
9. The short-range UAV simulator according to claim 8, characterized in that: The inner wall (2) of the straight-flying room (9) is rectangular, and the inner wall (2) of the flying-around room (1) is circular.
10. A short-range unmanned aerial vehicle simulator according to claim 8, characterized in that: Between the inner walls of the straight-flying room (9), there are successively a high-flying wall (14) and a low-flying wall (15). The high-flying wall (14) is provided with a high-pass opening (141), the low-flying wall (15) is provided with a low-pass opening (151). The swinging air duct (11) at the front end of the high-flying wall (14) is flush with the high-pass opening (141), and the swinging air duct (11) of the low-flying wall (15) is flush with the low-pass opening (151).
Citation Information
Patent Citations
Unmanned aerial vehicle flight simulator
CN210515755U