A flight simulation training device

Abstract

The utility model provides a kind of simulation flight image training device, it is related to simulation flight training technical field, comprising: virtual big screen, the inside of virtual big screen is provided with vibrating mechanism.The utility model, by the person who needs to be trained is seated in the seat of a bus, then according to the control of operator to controller, it can let virtual big screen and vibrating mechanism make corresponding action, when operator simulates take-off scene operator can be controlled upward by being controlled to controller, to let the display content in virtual big screen and the air cavity in front of air cavity on chassis by mounting seat and connecting buckle rod butt joint be inflated by air pump, and the air cylinder in the air cylinder in front of integrated frame is lifted up to let the front of integrated frame be raised to simulate take-off state, contrary operation down simulation drops, this kind of innovative imaging technology not only realizes the effect of broad field of view and far depth of field in limited space, also greatly enhances the immersion of driving experience and visual impact.

Description

Technical Field

[0001] This utility model relates to the field of flight simulation training technology, and in particular to a flight simulation image training device. Background Technology

[0002] With the continuous development of the aviation industry and the increasing demand for pilot training, flight simulation training systems, as an important means to improve pilots' operational capabilities, save training costs, and ensure flight safety, have been widely used in various fields such as civil aviation, military training, and flight instruction. Flight simulation training devices can provide pilots with a comprehensive training experience in areas such as control practice, emergency response training, and visual recognition without actual flight, playing a crucial role in improving flight skills.

[0003] Traditional flight simulators primarily consist of a physical control console, display equipment, and a simple dynamic feedback system to simulate the operational environment and flight states during flight. Existing technologies generally suffer from limitations such as monotonous simulation effects, weak immersion, lagging dynamic feedback, and limited viewing angles. Some simulators only provide a limited field of view through a front-facing screen, failing to achieve the wide field of view and three-dimensional depth of field of real flight. Their dynamic feedback mechanisms are often simple electric actuators, which cannot accurately reproduce complex states during flight such as takeoff, descent, or turbulence, resulting in a lack of realistic training experience for users. Furthermore, existing devices are mostly fixed in their physical structure, lacking the ability to respond in real-time to operational actions. Especially during training, the lack of sufficient dynamic feedback makes it difficult to accurately convey changes in flight attitude to the user, thus affecting their judgment and the development of operational habits. Therefore, we provide a flight simulator image training device. Utility Model Content

[0004] The purpose of this invention is to overcome the shortcomings of existing technologies and provide a simulated flight image training device.

[0005] To achieve the above objectives, the present invention adopts the following technical solution: a simulated flight image training device, comprising: an image mechanism, the image mechanism including a virtual large screen and a single hanging screen, the inner surface of the virtual large screen being provided with the single hanging screen, and the inner side of the virtual large screen being provided with a vibration mechanism; A vibration mechanism includes a chassis, a mounting base on the chassis, a connecting rod on the mounting base, an air chamber at one end of the connecting rod, an air pump on the air chamber, a mother air cylinder on one side of the air pump, a daughter air damping rod in the mother air cylinder, a docking ring at one end of the daughter air damping rod, a mounting bracket in the docking ring, and a control mechanism at one end of the mounting bracket. The control mechanism includes an integrated frame, a docking frame at the bottom of the integrated frame, a back support frame on one side of the integrated frame, a cylinder rod in the back support frame, a seating seat at one end of the cylinder rod, and a controller at the opposite end of the integrated frame located on the back support frame.

[0006] In a preferred embodiment, the inner surface of the virtual screen surrounds the outer surface of the vibration mechanism and the control mechanism, the single hanging screen is suspended on the inner surface of the virtual screen, and the mounting base is mounted on the chassis.

[0007] In a preferred embodiment, one end of the connecting rod is abutted against the mounting base, the end of the connecting rod away from the mounting base is welded to the air chamber, and one end of the air pump is abutted against the air chamber.

[0008] In a preferred embodiment, one end of the mother air cylinder is connected to the air chamber on one side of the air pump, the outer surface of the daughter air damping rod is nested in the mother air cylinder, and one end of the connecting ring is welded to the daughter air damping rod.

[0009] In a preferred embodiment, the end of the docking ring furthest from the sub-gas damping rod is docked to the mounting bracket, one end of the mounting bracket is welded to the docking bracket at the bottom of the integrated frame, and one end of the back support bracket is nested and welded into the integrated frame.

[0010] In a preferred embodiment, the two ends of the cylinder rod are respectively connected between the back support frame and the seat, the outer surface of the seat is nested in the integrated frame, and the outer surface of the controller is nested in the integrated frame on the opposite side of the back support frame.

[0011] Compared with the prior art, the advantages and positive effects of this utility model are as follows: This invention allows trainees to sit in a chair, and the virtual screen and vibration mechanism can be controlled by the operator via a controller. When simulating takeoff, the operator can move the controller upwards, causing the virtual screen to display content and the air chamber on the chassis connected by mounting brackets and connecting rods to be inflated by an air pump. This inflates the damping rod in the main air cylinder, causing the integrated frame to tilt upwards, thus simulating takeoff. Conversely, the operation simulates descent. This innovative imaging technology not only achieves a wide field of view and deep depth of field in a limited space, but also greatly enhances the immersiveness and visual impact of the driving experience. Attached Figure Description

[0012] Figure 1 This is a schematic diagram of the structure of a simulated flight image training device provided by this utility model.

[0013] Figure 2 This is an exploded view of the structure of a simulated flight image training device provided by this utility model.

[0014] Figure 3 A schematic diagram of the vibration mechanism structure of a simulated flight image training device provided by this utility model.

[0015] Figure 4 A schematic diagram of the control mechanism structure of a simulated flight image training device provided by this utility model.

[0016] Legend: 1. Imaging equipment; 11. Virtual large screen; 12. Single hanging screen; 2. Vibration mechanism; 21. Chassis; 22. Mounting base; 23. Connecting rod; 24. Air chamber; 25. Air pump; 26. Main air cylinder; 27. Sub-air damping rod; 28. Connecting ring; 29. ​​Mounting bracket; 3. Control mechanism; 31. Integrated frame; 32. Connecting frame; 33. Back support frame; 34. Cylinder rod; 35. Seating chair; 36. Controller. Detailed Implementation

[0017] To more clearly illustrate the overall concept of this utility model, a detailed description will be provided below with reference to the accompanying drawings and examples.

[0018] It should be noted that many specific details are set forth in the following description in order to provide a full understanding of the present invention. However, the present invention may also be implemented in other ways different from those described herein. Therefore, the scope of protection of the present invention is not limited to the specific embodiments disclosed below.

[0019] Example 1 like Figures 1-4 As shown, this utility model provides a technical solution: a simulated flight image training device, including: an image mechanism 1, the image mechanism 1 including a virtual large screen 11 and a single hanging screen 12, the inner surface of the virtual large screen 11 is provided with the single hanging screen 12, and the inner side of the virtual large screen 1 is provided with a vibration mechanism 2, wherein the large curved reflective screen involved is coated with a vacuum aluminum film to improve brightness and uniformity. The vibration mechanism 2 includes a chassis 21, a mounting base 22 on the chassis 21, a connecting rod 23 on the mounting base 22, an air chamber 24 at one end of the connecting rod 23, an air pump 25 on the air chamber 24, a mother air cylinder 26 on one side of the air pump 25, a daughter air damping rod 27 in the mother air cylinder 26, a docking ring 28 at one end of the daughter air damping rod 27, a mounting bracket 29 in the docking ring 28, and a control mechanism 3 at one end of the mounting bracket 29. The control mechanism 3 includes an integrated frame 31, a docking frame 32 is provided at the bottom of the integrated frame 31, a back support frame 33 is provided on one side of the integrated frame 31, a cylinder rod 34 is provided in the back support frame 33, a seating seat 35 is provided at one end of the cylinder rod 34, and a controller 36 is provided at the opposite end of the integrated frame 31 to the back support frame 33. The inner surface of the virtual screen 11 surrounds the outer surface of the vibration mechanism 2 and the control mechanism 3. A single hanging screen 12 is suspended from the inner surface of the virtual screen 11. A mounting base 22 is mounted on the chassis 21. One end of the connecting rod 23 is connected to the mounting base 22, and the end of the connecting rod 23 away from the mounting base 22 is welded to the air chamber 24. One end of the air pump 25 is connected to the air chamber 24, and one end of the main air cylinder 26 is connected to the air chamber 24, located on one side of the air pump 25. The outer surface of the sub-air damping rod 27 is nested within the main air cylinder 26. The docking ring 2... One end of the 8 is welded to the sub-gas damping rod 27. The end of the docking ring 28 away from the sub-gas damping rod 27 is docked to the mounting bracket 29. One end of the mounting bracket 29 is welded to the docking bracket 32 ​​at the bottom of the integrated frame 31. One end of the back support frame 33 is nested and welded in the integrated frame 31. The two ends of the cylinder rod 34 are respectively docked between the back support frame 33 and the seat 35. The outer surface of the seat 35 is nested in the integrated frame 31. The outer surface of the controller 36 is nested in the integrated frame 31 on the opposite side of the back support frame 33.

[0020] In this embodiment, when using this training device for simulated flight training, the operator can seat the person to be trained in the seating chair 35. Then, based on the operator's control of the controller 36, the virtual screen 1 and the vibration mechanism 2 can perform corresponding actions. When simulating takeoff, the operator can control the controller 36 to move it upwards, causing the content displayed on the virtual screen 1 and the air chamber 24 on the chassis 21 (connected by the mounting base 22 and connecting rod 23) to be inflated by the air pump 25. This inflates the damping rod 27 in the main air cylinder 26, causing the integrated frame 31 to tilt upwards, simulating takeoff. Conversely, the downward movement simulates descent. This innovative imaging technology not only achieves a wide field of view and deep depth of field within a limited space but also greatly enhances the immersiveness and visual impact of the flight experience. Through this technological innovation, we not only effectively save space but also provide pilots with a more realistic and immersive visual experience, further improving the effectiveness and quality of simulated flight training and bringing revolutionary changes to pilot training.

[0021] Working principle: like Figures 1-4As shown, trainees must sit in a specially designed chair 35 to ensure they can maintain a stable and comfortable correct posture during training. Subsequently, the operator controls the training device via controller 36, thereby activating the virtual screen 1 and vibration mechanism 2, enabling the training simulation system to perform corresponding actions according to the operator's instructions.

[0022] When the operator simulates a takeoff scenario, by manipulating the controller 36 upwards, the training system responds in real time and adjusts the actions of the relevant devices. The content displayed on the virtual screen 1 updates according to the changes in flight status, presenting a more realistic flight scenario. At the same time, the air chamber 24 on the chassis 21 is activated by the inflation action of the air pump 25. The precise alignment of the mounting base 22 and the connecting rod 23 causes the sub-air damping rod 27 in front of the air chamber 24 to rise upwards, thereby causing the integrated frame 31 to tilt forward, perfectly simulating the takeoff state.

[0023] The core innovation of this flight simulation system lies in the application of aerodynamic simulation technology, which allows virtual flight and physical movements to be closely integrated, providing a more realistic flight takeoff experience. Conversely, when the operator controls the controller 36 downwards, the air chamber 24 releases gas to simulate the effect of an aircraft descending, completing training for a full takeoff and landing scenario.

[0024] This innovative simulation imaging technology not only achieves a wide field of view and a deep depth of field within a limited training space, but also significantly enhances pilots' perception of flight status during training. Through the display on the virtual screen and the synchronized movement of the vibration mechanism, pilots can more realistically feel changes in flight status, thereby increasing the immersion and visual impact of training, enabling pilots to better understand and respond to various situations that may be encountered during flight simulation.

[0025] This technological innovation has enabled us to save space, avoiding the bulky space and complex equipment required by traditional flight simulators. This compact and efficient system allows pilots to gain a superior training experience in a more realistic training environment. This not only significantly improves the effectiveness and quality of flight training but also revolutionizes pilot training, making it more efficient, economical, and realistic, providing pilots with a more solid technical foundation for real flight missions.

[0026] Those skilled in the art should understand that the discussion of any of the above embodiments is merely exemplary and is not intended to imply that the scope of the present invention (including the claims) is limited to these examples; within the framework of the present invention, the technical features of the above embodiments or different embodiments can also be combined, the steps can be implemented in any order, and there are many other variations of different aspects of the present invention as described above, which are not provided in the details for the sake of brevity.

[0027] This utility model is intended to cover all such substitutions, modifications, and variations that fall within the broad scope of the appended claims. Therefore, any omissions, modifications, equivalent substitutions, improvements, etc., made within the spirit and principles of this utility model should be included within the protection scope of this utility model.

Claims

1. A simulated flight image training device, characterized in that, include: The imaging mechanism (1) includes a virtual screen (11) and a single hanging screen (12). The inner surface of the virtual screen (11) is provided with a single hanging screen (12), and the inner side of the virtual screen (11) is provided with a vibration mechanism (2). The vibration mechanism (2) includes a chassis (21), a mounting base (22) is provided on the chassis (21), a connecting rod (23) is provided on the mounting base (22), an air chamber (24) is provided at one end of the connecting rod (23), an air pump (25) is provided on the air chamber (24), a mother air cylinder (26) is provided on one side of the air pump (25), a daughter air damping rod (27) is provided in the mother air cylinder (26), a docking ring (28) is provided at one end of the daughter air damping rod (27), a mounting frame (29) is provided in the docking ring (28), and a control mechanism (3) is provided at one end of the mounting frame (29). The control mechanism (3) includes an integrated frame (31), a docking frame (32) is provided at the bottom of the integrated frame (31), a back support frame (33) is provided on one side of the integrated frame (31), a cylinder rod (34) is provided in the back support frame (33), a seating chair (35) is provided at one end of the cylinder rod (34), and a controller (36) is provided at the opposite end of the integrated frame (31) and the back support frame (33).

2. The simulated flight image training device according to claim 1, characterized in that: The inner surface of the virtual screen (11) surrounds the outer surface of the vibration mechanism (2) and the control mechanism (3), the single hanging screen (12) is suspended on the inner surface of the virtual screen (11), and the mounting base (22) is mounted on the chassis (21).

3. The simulated flight image training device according to claim 2, characterized in that: One end of the connecting rod (23) is connected to the mounting base (22), the other end of the connecting rod (23) away from the mounting base (22) is welded to the air chamber (24), and one end of the air pump (25) is connected to the air chamber (24).

4. The simulated flight image training device according to claim 1, characterized in that: One end of the mother air cylinder (26) is connected to the air chamber (24) on one side of the air pump (25). The outer surface of the daughter air damping rod (27) is nested in the mother air cylinder (26). One end of the docking ring (28) is welded to the daughter air damping rod (27).

5. The simulated flight image training device according to claim 1, characterized in that: The end of the docking ring (28) away from the sub-gas damping rod (27) is docked on the mounting frame (29), one end of the mounting frame (29) is welded to the docking frame (32) at the bottom of the integrated frame (31), and one end of the back support frame (33) is nested and welded in the integrated frame (31).

6. The simulated flight image training device according to claim 1, characterized in that: The two ends of the cylinder rod (34) are respectively connected between the back support frame (33) and the seat (35). The outer surface of the seat (35) is nested in the integrated frame (31), and the outer surface of the controller (36) is nested in the integrated frame (31) on the opposite side of the back support frame (33).

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