Unmanned aerial vehicle flight simulation platform

Abstract

The utility model belongs to the technical field of entertainment equipment, and particularly relates to an unmanned aerial vehicle flight simulation platform which comprises a six-axis adjusting supporting part, a simulation cabin connected to the upper end of the six-axis adjusting supporting part and two ladder stand frames located on the two sides of the six-axis adjusting supporting part and further comprises an environment simulation assembly used for simulating rainy day flight. The environment simulation assembly comprises a support fixedly connected to the lower end of the simulation cabin, a water tank fixedly connected to the lower end of the support, a pump body fixedly connected to the upper end of the support, a plurality of guide frames fixedly connected to the outer surface of the support and a spray head fixedly connected to one side of the support and facing the simulation cabin, and the input end of the pump body penetrates through the guide frames and extends into the water tank; the simulation platform can simulate a scene of flying in a rainy day, the simulation platform has an environment scene change function, the experience effect is enriched, the air blowing part is arranged, water drops on the outer surface of the simulation cabin are blown through the air blowing part to form raindrop runoff, the experience feeling is more real, and the experience effect of an experiencer is improved.

Description

Technical Field

[0001] This application relates to the field of entertainment equipment technology, specifically to a drone flight simulation platform. Background Technology

[0002] To enable consumers to experience the thrill of flight adventure, some flight simulation platforms exist on the market. Most of them simulate flight by moving the cockpit through a base. For example, existing technology (Chinese utility model with announcement number CN219180070U) discloses a flight simulator with a cockpit and a display screen. The user sits in the cockpit and watches the animation on the screen. The user's experience is simulated by the base working to move the cockpit. Although it can achieve a certain flight simulation effect, it lacks environmental scene changes, resulting in a monotonous experience and an unrealistic feeling, leading to a poor user experience. Utility Model Content

[0003] The purpose of this application is to provide a drone flight simulation platform to solve the technical problems mentioned in the background art.

[0004] To achieve the above objectives, this application provides the following technical solution: a drone flight simulation platform, comprising a six-axis adjustable support unit, a simulation cockpit connected to the upper end of the six-axis adjustable support unit, and two ladder frames located on both sides of the six-axis adjustable support unit.

[0005] It also includes an environmental simulation component for simulating flight in rainy weather, and the environmental simulation component includes a bracket fixed to the lower end of the simulated cockpit, a water tank fixed to the lower end of the bracket, a pump body fixed to the upper end of the bracket, multiple guide frames fixed to the outer surface of the bracket, and a nozzle fixed to one side of the bracket and facing the simulated cockpit. The input end of the pump body passes through the multiple guide frames and extends into the water tank, and the output end of the pump body is connected to the nozzle.

[0006] In one embodiment, a blower is also fixed to one side of the bracket, with the air outlet of the blower facing the simulated cockpit. The blower blows water droplets discharged from the nozzle and falling on the outer surface of the simulated cockpit, causing them to move and form raindrop runoff.

[0007] In one embodiment, the six-axis adjustable support includes a base platform, six electric cylinders movably connected to the upper end of the base platform, an upper platform movably connected to the telescopic ends of the six electric cylinders, a rotary servo motor fixed to the middle of the lower end of the upper platform, and a large rotary bearing connecting the upper end of the upper platform to the lower end of the simulated cockpit. The output shaft of the rotary servo motor passes through the upper platform and is fixed to the lower end of the simulated cockpit.

[0008] In one embodiment, the simulated cockpit includes an aircraft model cockpit located above an upper platform and whose lower end is fixedly connected to the rotating part of a large slewing bearing, multiple openings on one side of the aircraft model cockpit, multiple front window baffles fixedly connected to the inner walls of the multiple openings, and seats fixedly connected to the aircraft model cockpit.

[0009] In one embodiment, the simulated cockpit further includes four connecting rods fixed to the upper outer surface of the aircraft model cockpit, four sets of propeller motors fixed inside the four connecting rods, and four sets of flight propellers fixed to the output shafts of the four sets of propeller motors.

[0010] In one embodiment, light strips are fixed to the upper and lower ends of the four connecting rods.

[0011] In one embodiment, a carbon fiber trim is also attached to one side of the outer surface of the aircraft model cockpit.

[0012] In one embodiment, the inner wall of the aircraft model cockpit is also fixed with an inner safety handrail.

[0013] In one embodiment, the aircraft model cockpit is also equipped with control buttons, which are linearly connected to the light strip, propeller motor, six-axis adjustable support, and environmental simulation components.

[0014] Compared with the prior art, the beneficial effects of this application are:

[0015] 1) This application is equipped with an environmental simulation component, which can spray water onto the outer surface of the simulated cockpit to simulate a rainy flight scenario, enabling the simulation platform to have the function of changing environmental scenarios and enriching the experience. In addition, a blower is provided to blow water droplets on the outer surface of the simulated cockpit to form raindrop runoff, making the experience more realistic and improving the experience of the user.

[0016] 2) Based on the real aircraft, this application has multiple openings on one side of the cockpit of the aircraft model, making the front window transparent on three sides and providing a wider field of vision. At the same time, a six-axis + 360-degree rotating platform can better simulate the flight of the aircraft. In addition, four sets of propeller motors and flight propellers are set up to simulate the up and down rotation of the real aircraft, giving people a better and more realistic experience. Attached Figure Description

[0017] Figure 1 This is a schematic diagram of the overall structure of this application;

[0018] Figure 2 This is a schematic diagram of the simulated cockpit structure for this application;

[0019] Figure 3 This is a schematic diagram of the LED strip structure of this application;

[0020] Figure 4 This is a schematic diagram of the rotary servo motor and large slewing bearing structure of this application.

[0021] In the diagram: 1. Six-axis adjustable support; 11. Base platform; 12. Electric cylinder; 13. Upper platform; 14. Rotary servo motor; 15. Large slewing bearing; 2. Climbing ladder; 3. Simulated cockpit; 31. Aircraft model cockpit; 32. Front window baffle; 33. Control button; 34. Linkage rod; 341. Light strip; 35. Inner safety handrail; 36. Seat; 37. Propeller motor; 38. Flight propeller; 39. Carbon fiber trim; 4. Environmental simulation components; 41. Bracket; 42. Water tank; 43. Guide frame; 44. Pump body; 45. Nozzle; 46. Air blower. Detailed Implementation

[0022] The technical solutions of the embodiments of this application will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are only some embodiments of this application, and not all embodiments. Based on the embodiments of this application, all other embodiments obtained by those skilled in the art without creative effort are within the scope of protection of this application.

[0023] In the description of this application, it should be understood that the terms "upper", "lower", "front", "rear", "left", "right", "top", "bottom", "inner", "outer", etc., indicate the orientation or positional relationship based on the orientation or positional relationship shown in the accompanying drawings. They are only for the convenience of describing this application and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific orientation, or be constructed and operated in a specific orientation. Therefore, they should not be construed as limitations on this application.

[0024] Example:

[0025] Please see Figure 1-4 This application provides a technical solution: a drone flight simulation platform, including a six-axis adjustable support 1, a simulation cockpit 3 connected to the upper end of the six-axis adjustable support 1, and two climbing ladder frames 2 located on both sides of the six-axis adjustable support 1.

[0026] It also includes an environmental simulation component 4 for simulating flight in rainy weather. The environmental simulation component 4 includes a bracket 41 fixed to the lower end of the simulated cockpit 3, a water tank 42 fixed to the lower end of the bracket 41, a pump body 44 fixed to the upper end of the bracket 41, a plurality of guide frames 43 fixed to the outer surface of the bracket 41, and a nozzle 45 fixed to one side of the bracket 41 and facing the simulated cockpit 3. The input end of the pump body 44 passes through the plurality of guide frames 43 and extends into the water tank 42, and the output end of the pump body 44 is connected to the nozzle 45.

[0027] A blower 46 is also fixed to one side of the bracket 41. The air outlet of the blower 46 faces the simulated cockpit 3 and blows the water droplets discharged from the nozzle 45 onto the outer surface of the simulated cockpit 3 to move them and form raindrop runoff.

[0028] By adopting the above scheme, the user climbs up the ladder 2 to the interior of the simulated cockpit 3. The six-axis adjustable support 1 drives the simulated cockpit 3 to move freely, simulating flight. At the same time, the pump 44 is controlled to pump water from the water tank 42 into the nozzle 45. Water droplets are discharged from the nozzle 45 and fall on the outer surface of the simulated cockpit 3, simulating a rainy day flight scenario. This gives the simulation platform the function of changing environmental scenarios, enriching the experience. At the same time, the blower 46 (which can be a blower) is controlled to generate airflow and blow water droplets on the outer surface of the simulated cockpit 3 to move, forming raindrop runoff, making the experience more realistic and improving the user's experience.

[0029] Please see Figure 2 and Figure 4 The six-axis adjustable support unit 1 includes a base platform 11, six electric cylinders 12 movably connected to the upper end of the base platform 11, an upper platform 13 movably connected to the telescopic ends of the six electric cylinders 12, a rotary servo motor 14 fixedly connected to the middle of the lower end of the upper platform 13, and a large slewing bearing 15 connecting the upper end of the upper platform 13 to the lower end of the simulated cockpit 3. The output shaft of the rotary servo motor 14 passes through the upper platform 13 and is fixedly connected to the lower end of the simulated cockpit 3.

[0030] By adopting the above scheme, the operation of the six electric cylinders 12 can drive the upper platform 13 and the simulated cockpit 3 to perform multi-degree-of-freedom motion, and the operation of the rotary servo motor 14 can drive the simulated cockpit 3 to rotate 360° on the upper platform 13 (the simulated cockpit 3 rotates on the upper platform 13 through the large slewing bearing 15). The simulated cockpit 3 can also perform rotational motion on the basis of multi-degree-of-freedom motion, which can better simulate aircraft flight.

[0031] Please see Figure 2 The simulated cockpit 3 includes an aircraft model cockpit 31 (made of fiberglass) located above the upper platform 13 and fixedly connected at its lower end to the rotating part of the large slewing bearing 15; multiple openings on one side of the aircraft model cockpit 31; multiple front window baffles 32 (made of transparent acrylic) fixedly connected to the inner walls of the multiple openings; and seats 36 fixedly connected to the aircraft model cockpit 31. An inner safety armrest 35 is also fixedly connected to the inner wall of the aircraft model cockpit 31 (for enhanced safety for users). A carbon fiber decorative section 39 (using simulated aircraft carbon fiber stickers to improve realism and the user experience) is also attached to the outer surface of one side of the aircraft model cockpit 31.

[0032] By adopting the above scheme, the cockpit 31 of the aircraft model in this application is a fiberglass model, which is reproduced at a 1:1 scale to the real aircraft, making people more comfortable and giving them a more realistic experience. Multiple openings are provided on one side of the cockpit 31, making the front window transparent on three sides, with a wider field of vision, giving people a better and more realistic experience.

[0033] Please see Figure 2 and Figure 3 The simulated cockpit 3 also includes four connecting rods 34 fixed to the upper outer surface of the aircraft model cockpit 31, four sets of propeller motors 37 fixed inside the four connecting rods 34 respectively, and four sets of flight propellers 38 fixed to the output shafts of the four sets of propeller motors 37 respectively.

[0034] LED strips 341 are fixed to the upper and lower ends of the four connecting rods 34 (to emit light and enhance the user experience).

[0035] By adopting the above solution, the propeller motor 37 (which is a mature existing technology and will not be described in detail here) can drive the flight propeller 38 to rotate, simulating the up and down rotation of the real aircraft. At the same time, the rotation of the flight propeller 38 can also generate airflow, improving the experience.

[0036] The aircraft model cockpit 31 is also equipped with control buttons 33 (consisting of a control circuit board and buttons connected to the circuit board, which is a conventional control method in the prior art and will not be described in detail here), and the control buttons 33 are linearly connected to the light strip 341, the propeller motor 37, the six-axis adjustable support 1, and the environmental simulation component 4. The working status of the above-mentioned components can be controlled by the control buttons 33.

[0037] The foregoing has shown and described the basic principles, main features, and advantages of this application. It will be apparent to those skilled in the art that this application is not limited to the details of the exemplary embodiments described above, and that this application can be implemented in other specific forms without departing from the spirit or basic characteristics of this application. Therefore, the embodiments should be regarded as exemplary and non-limiting in all respects. The scope of this application is defined by the appended claims rather than the foregoing description. Therefore, it is intended to encompass all variations falling within the meaning and scope of equivalents of the claims within this application, and no reference numerals in the claims should be regarded as limiting the scope of the claims.

[0038] Although embodiments of this application have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and variations can be made to these embodiments without departing from the principles and spirit of this application, the scope of which is defined by the appended claims and their equivalents.

Claims

1. A drone flight simulation platform, comprising a six-axis adjustable support unit (1), a simulation cockpit (3) connected to the upper end of the six-axis adjustable support unit (1), and two climbing ladders (2) located on both sides of the six-axis adjustable support unit (1), characterized in that: It also includes an environmental simulation component (4) for simulating flight in rainy weather, and the environmental simulation component (4) includes a bracket (41) fixed to the lower end of the simulated cockpit (3), a water tank (42) fixed to the lower end of the bracket (41), a pump body (44) fixed to the upper end of the bracket (41), a plurality of guide frames (43) fixed to the outer surface of the bracket (41), and a nozzle (45) fixed to one side of the bracket (41) and facing the simulated cockpit (3). The input end of the pump body (44) passes through the plurality of guide frames (43) and extends into the water tank (42), and the output end of the pump body (44) is connected to the nozzle (45).

2. The UAV flight simulation platform according to claim 1, characterized in that: A blower (46) is also fixed to one side of the bracket (41). The air outlet of the blower (46) faces the simulated cockpit (3). The blower (46) blows water droplets discharged from the nozzle (45) and falling on the outer surface of the simulated cockpit (3) to move them and form raindrop runoff.

3. The UAV flight simulation platform according to claim 2, characterized in that: The six-axis adjustable support unit (1) includes a base platform (11), six electric cylinders (12) movably connected to the upper end of the base platform (11), an upper platform (13) movably connected to the telescopic ends of the six electric cylinders (12), a rotary servo motor (14) fixedly connected to the middle of the lower end of the upper platform (13), and a large slewing bearing (15) connecting the upper end of the upper platform (13) to the lower end of the simulated cockpit (3). The output shaft of the rotary servo motor (14) passes through the upper platform (13) and is fixedly connected to the lower end of the simulated cockpit (3).

4. The UAV flight simulation platform according to claim 3, characterized in that: The simulated cockpit (3) includes an aircraft model cockpit (31) located above the upper platform (13) and fixed at its lower end to the rotating part of the large slewing bearing (15), multiple openings on one side of the aircraft model cockpit (31), multiple front window baffles (32) fixed in the inner walls of the multiple openings respectively, and seats (36) fixed in the aircraft model cockpit (31).

5. The UAV flight simulation platform according to claim 4, characterized in that: The simulated cockpit (3) also includes four connecting rods (34) fixed to the upper outer surface of the aircraft model cockpit (31), four sets of propeller motors (37) fixed inside the four connecting rods (34) respectively, and four sets of flight propellers (38) fixed to the output shafts of the four sets of propeller motors (37) respectively.

6. The UAV flight simulation platform according to claim 5, characterized in that: LED strips (341) are fixed to the upper and lower ends of the four connecting rods (34).

7. A drone flight simulation platform according to any one of claims 4-6, characterized in that: The outer surface of one side of the aircraft model cockpit (31) is also connected to a carbon fiber decorative part (39).

8. The UAV flight simulation platform according to claim 7, characterized in that: The inner wall of the aircraft model cockpit (31) is also fixed with an inner safety handrail (35).

9. The UAV flight simulation platform according to claim 8, characterized in that: The aircraft model cockpit (31) is also equipped with control buttons (33), and the control buttons (33) are linearly connected to the light strip (341), the propeller motor (37), the six-axis adjustment support (1), and the environmental simulation component (4).

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