Adjustable unmanned aerial vehicle simulation training cockpit

Abstract

The utility model discloses an adjustable unmanned aerial vehicle simulation training cockpit which structurally comprises a cabin body, a first control mechanism, a second control mechanism, a transmission mechanism and a seat, a mounting frame is fixedly arranged on the upper portion of the cabin body, and the first control mechanism and the second control mechanism are both arranged on the mounting frame. The second control mechanism comprises an outer rotating shaft, the outer rotating shaft is rotationally connected with the inner side of the mounting frame and penetrates through the mounting frame, a rotating frame is fixedly arranged at the upper end of the outer rotating shaft, the first control mechanism comprises an inner rotating shaft, and the inner rotating shaft is rotationally connected with the inner side of the outer rotating shaft and penetrates through the outer rotating shaft; a driving bevel gear is fixedly arranged at the upper end of the inner rotating shaft and rotationally connected with the upper portion of the inner side of the rotating frame, and the transmission mechanism is arranged on the inner side of the rotating frame. The utility model belongs to the field of unmanned aerial vehicle cockpits, and particularly relates to an adjustable unmanned aerial vehicle simulation training cockpit.

Description

Technical Field

[0001] The utility model belongs to the field of unmanned aerial vehicle cockpits, and specifically refers to an adjustable unmanned aerial vehicle simulation training cockpit. Background Art

[0002] Drone technology is rapidly developing worldwide, and its applications are becoming increasingly widespread, encompassing a wide range of industries, including agriculture, logistics, and film and television production. To cultivate more professional drone operators, drone simulation training devices have become a crucial tool for improving pilots' skills.

[0003] Existing drone simulation training cockpits mostly provide intuitive simulated visual experience during training, but cannot truly achieve human-computer interactivity and driving experience. Physical discomfort and dizziness will still occur when actually operating the drone. Utility Model Content

[0004] The technical problem to be solved by the utility model is that dizziness easily occurs when only simulating visual real operation is performed.

[0005] In order to solve the above problems, the technical solution adopted by the present invention is as follows: The adjustable drone simulation training cockpit proposed by the present invention includes a cabin, a drone and a head-mounted display device, the upper part of the cabin is set as a transparent frame structure, the upper part of the cabin is fixed with a mounting frame, and also includes a first control mechanism, a second control mechanism, a transmission mechanism and a seat, the first control mechanism and the second control mechanism are both arranged on the mounting frame, the second control mechanism includes an outer rotating shaft, the outer rotating shaft is rotatably connected to the inner side of the mounting frame and passes through the mounting frame, and the upper end of the outer rotating shaft is fixed with a rotating frame The first control mechanism includes an inner rotating shaft, the inner rotating shaft and the inner side of the outer rotating shaft are rotatably connected and pass through the outer rotating shaft, the upper end of the inner rotating shaft is fixedly provided with a driving bevel gear, the driving bevel gear is rotatably connected to the upper inner side of the rotating frame, the transmission mechanism is arranged on the inner side of the rotating frame, the transmission mechanism includes a connecting rod and a pillar, the connecting rod is rotatably connected to the inner side of the rotating frame, one end of the connecting rod is fixedly provided with a driven bevel gear, the driven bevel gear and the driving bevel gear are meshedly connected, the lower end of the pillar is fixedly connected to the middle section of the connecting rod, and the upper end of the pillar is fixedly connected to the bottom of the seat.

[0006] Furthermore, the first control mechanism also includes a first motor and a first worm, the first worm is rotatably connected to the left side of the mounting frame and passes through the mounting frame, a first worm wheel is fixed to the lower end of the inner rotating shaft, and the first worm wheel and the first worm are meshingly connected.

[0007] Furthermore, the first motor is fixed on the front side of the mounting frame, and the first motor is connected to the first worm shaft.

[0008] Furthermore, the second control mechanism also includes a second motor and a second worm, the second worm is rotatably connected to the right side of the mounting frame and passes through the mounting frame, a second worm gear is fixed to the lower end of the outer rotating shaft, and the second worm gear and the second worm are meshingly connected.

[0009] Furthermore, the second motor is fixed on the rear side of the mounting frame, and the second motor is connected to the second worm shaft.

[0010] Furthermore, the rotating frame is configured as a U-shaped plate structure.

[0011] Furthermore, a leg rest is fixedly provided on the front side of the seat, a strap is provided between the armrests on both sides of the seat, a joystick is rotatably connected to the armrest on one side of the seat, and an operating panel is rotatably connected to the armrest on the other side of the seat, the first motor and the second motor are respectively wirelessly connected to the operating panel, and the drone is wirelessly connected to the head-mounted display device and the operating panel respectively.

[0012] The beneficial effects achieved by the utility model using the above structure are as follows:

[0013] The adjustable drone simulation training cockpit proposed in this solution adjusts the seat angle by cooperating with the first control mechanism and the second control mechanism in conjunction with the transmission mechanism, thereby improving the human-computer interactivity of the drone simulation training cockpit, enhancing the driving experience, and preventing the physiological burden caused by dizziness due to real operation. BRIEF DESCRIPTION OF THE DRAWINGS

[0014] Figure 1 It is a schematic diagram of the overall structure of the utility model;

[0015] Figure 2 This is a schematic diagram of the internal structure of the utility model;

[0016] Figure 3 This is a schematic diagram of the first partial structure of the utility model;

[0017] Figure 4 This is a schematic diagram of the second partial structure of the utility model;

[0018] Figure 5 This is a schematic diagram of the third partial structure of the utility model;

[0019] Figure 6 This is a schematic diagram of the fourth partial structure of the present utility model.

[0020] Among them, 1. cabin, 2. mounting frame, 3. first control mechanism, 301. first motor, 302. first worm, 303. first worm gear, 304. inner rotating shaft, 305. driving bevel gear, 4. second control mechanism, 401. second motor, 402. second worm, 403. second worm gear, 404. outer rotating shaft, 405. rotating frame, 5. transmission mechanism, 501. driven bevel gear, 502. connecting rod, 503. pillar, 6. seat, 601. leg rest, 602. strap, 603. rocker, 604. operating panel.

[0021] The accompanying drawings are used to provide a further understanding of the present invention and constitute a part of the specification. Together with the embodiments of the present invention, they are used to explain the present invention and do not constitute a limitation to the present invention. DETAILED DESCRIPTION

[0022] The technical solutions in the embodiments of the present invention will be clearly and completely described below in conjunction with the drawings in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, rather than all the embodiments; based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without making creative work are within the scope of protection of the present invention.

[0023] like Figure 1-6 As shown, the utility model proposes an adjustable UAV simulation training cockpit, including a cabin body 1, the upper part of the cabin body 1 is set as a transparent frame structure, the upper part of the cabin body 1 is fixedly provided with a mounting frame 2, and also includes a first control mechanism 3, a second control mechanism 4, a transmission mechanism 5 and a seat 6, a leg rest 601 is fixedly provided on the front side of the seat 6, a strap 602 is provided between the armrests on both sides of the seat 6, a rocker 603 is rotatably connected to the armrest on one side of the seat 6, and an operating panel 604 is rotatably connected to the armrest on the other side of the seat 6.

[0024] like Figure 1-6As shown, the first control mechanism 3 and the second control mechanism 4 are both arranged on the mounting frame 2, the second control mechanism 4 includes an outer rotating shaft 404, the outer rotating shaft 404 is rotatably connected to the inner side of the mounting frame 2 and passes through the mounting frame 2, a rotating frame 405 is fixed on the upper end of the outer rotating shaft 404, and the rotating frame 405 is set as a U-shaped plate structure, the first control mechanism 3 includes an inner rotating shaft 304, the inner rotating shaft 304 is rotatably connected to the inner side of the outer rotating shaft 404 and passes through the outer rotating shaft 404, and a main rotating shaft 405 is fixed on the upper end of the inner rotating shaft 304. The driven bevel gear 305, the active bevel gear 305 and the upper inner side of the rotating frame 405 are rotatably connected. The transmission mechanism 5 is arranged on the inner side of the rotating frame 405. The transmission mechanism 5 includes a connecting rod 502 and a pillar 503. The connecting rod 502 is rotatably connected to the inner side of the rotating frame 405. A driven bevel gear 501 is fixed to one end of the connecting rod 502. The driven bevel gear 501 and the active bevel gear 305 are meshedly connected. The lower end of the pillar 503 is fixed to the middle section of the connecting rod 502, and the upper end of the pillar 503 is fixed to the bottom of the seat 6.

[0025] like Figure 3-6 As shown, the first control mechanism 3 also includes a first motor 301 and a first worm 302. The first worm 302 is rotatably connected to the left side of the mounting frame 2 and passes through the mounting frame 2. A first worm gear 303 is fixed to the lower end of the inner rotating shaft 304. The first worm gear 303 and the first worm 302 are meshingly connected. The first motor 301 is fixed to the front side of the mounting frame 2, and the first motor 301 and the first worm 302 are axially connected.

[0026] like Figure 3-6 As shown, the second control mechanism 4 also includes a second motor 401 and a second worm 402. The second worm 402 is rotatably connected to the right side of the mounting frame 2 and passes through the mounting frame 2. A second worm gear 403 is fixed to the lower end of the outer rotating shaft 404. The second worm gear 403 and the second worm 402 are meshingly connected. The second motor 401 is fixed to the rear side of the mounting frame 2, and the second motor 401 and the second worm 402 are axially connected.

[0027] During specific use, the driver sits on the seat 6, places the legs in the leg rest 601, and fixes the body with the strap 602, turns the operating panel 604 to the front of the driver, and wirelessly connects the drone to the head display device and the operating panel 604 respectively. The driver holds the joystick 603 to simulate the control of the drone, and the first motor 301 and the second motor 401 are wirelessly connected to the operating panel 604 respectively. According to the flight angle of the drone, the first motor 301 is started to rotate the first worm 302 forward and reverse to drive the first worm gear 303 and the inner rotating shaft 304. As well as the rotation of the active bevel gear 305, under the meshing transmission of the active bevel gear 305 and the driven bevel gear 501, the connecting rod 502, the pillar 503 and the seat 6 are controlled to rotate forward and backward, which can make the driving trainee feel the climbing and descending angles of the drone more intuitively, and start the second motor 401 to rotate the second worm 402 forward and reverse to drive the second worm gear 403, the outer rotating shaft 404 and the rotating frame 405 to rotate, which can make the driving trainee feel the rotation inclination angle of the drone more intuitively, increase the driving experience of the driving trainee, and prevent dizziness when actually operating the drone.

[0028] The above description of the present invention and its embodiments is non-limiting. The drawings show only one embodiment of the present invention, and the actual structure is not limited thereto. In short, if a person skilled in the art is inspired by the above, and does not deviate from the purpose of the present invention, without inventive design, a structure and embodiment similar to the technical solution should fall within the scope of protection of the present invention.

Claims

1. An adjustable drone simulation training cockpit, comprising a cabin, a drone, and a head-mounted display device, wherein the upper portion of the cabin is configured as a transparent frame structure, and a mounting frame is fixedly provided on the upper portion of the cabin, characterized in that: The first and second control mechanisms are both provided on the mounting frame, the second control mechanism comprising an outer rotating shaft, the outer rotating shaft being rotatably connected to the inner side of the mounting frame and passing through the mounting frame, the upper end of the outer rotating shaft being fixedly provided with a rotating frame, the first control mechanism comprising an inner rotating shaft, the inner rotating shaft being rotatably connected to the inner side of the outer rotating shaft and passing through the outer rotating shaft, the upper end of the inner rotating shaft being fixedly provided with a driving bevel gear, the driving bevel gear being rotatably connected to the inner upper part of the rotating frame, the transmission mechanism being provided on the inner side of the rotating frame, the transmission mechanism comprising a connecting rod and a pillar, the connecting rod being rotatably connected to the inner side of the rotating frame, one end of the connecting rod being fixedly provided with a driven bevel gear, the driven bevel gear and the driving bevel gear being meshedly connected, the lower end of the pillar being fixedly connected to the middle section of the connecting rod, and the upper end of the pillar being fixedly provided to the bottom of the seat.

2. The adjustable UAV simulation training cockpit according to claim 1, characterized in that: The first control mechanism also includes a first motor and a first worm. The first worm is rotatably connected to the left side of the mounting frame and passes through the mounting frame. A first worm wheel is fixed to the lower end of the inner rotating shaft. The first worm wheel and the first worm are meshedly connected.

3. The adjustable UAV simulation training cockpit according to claim 2, characterized in that: The first motor is fixed on the front side of the mounting frame, and the first motor is connected to the first worm shaft.

4. The adjustable UAV simulation training cockpit according to claim 3, characterized in that: The second control mechanism also includes a second motor and a second worm, the second worm is rotatably connected to the right side of the mounting frame and passes through the mounting frame, a second worm gear is fixed to the lower end of the outer rotating shaft, and the second worm gear and the second worm are meshedly connected.

5. The adjustable UAV simulation training cockpit according to claim 4, characterized in that: The second motor is fixed on the rear side of the mounting frame, and the second motor is connected to the second worm shaft.

6. The adjustable UAV simulation training cockpit according to claim 5, characterized in that: The rotating frame is configured as a U-shaped plate structure.

7. The adjustable UAV simulation training cockpit according to claim 6, characterized in that: A leg rest is fixedly provided on the front side of the seat, a strap is provided between the armrests on both sides of the seat, a rocker is rotatably connected to the armrest on one side of the seat, and an operating panel is rotatably connected to the armrest on the other side of the seat, the first motor and the second motor are respectively wirelessly connected to the operating panel, and the drone is wirelessly connected to the head display device and the operating panel respectively.

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