A flight simulation training device based on virtual reality

Abstract

The invention relates to the technical field of flight simulation training, in particular to a flight simulation training device based on virtual reality, comprising an integrated cockpit, an operating table installed on the integrated cockpit and a seat installed on the integrated cockpit, wherein a supporting device is provided at the bottom of the seat, and an installation cavity is provided at the bottom of the integrated cockpit; the flight simulation training device based on virtual reality can support the seat through the provided supporting device, and can simulate an emergency situation when the pilot performs simulation training through the provided emergency simulation training device, and the emergency situation is simulated by shaking the seat in the present invention, and the pilot can control the emergency situation in time through a control device, and when the pilot has poor psychological quality and cannot accurately operate the control device in this situation, the shaking of the seat becomes more intense, further realizing the function of training the psychological state of the pilot when encountering an emergency situation.

Description

Technical Field

[0001] The present invention relates to the technical field of flight simulation training, in particular to a flight simulation training device based on virtual reality. Background Art

[0002] The flight simulation training device is designed to meet the requirements of rapid assembly and disassembly, multiple modes of transportation, and unrestricted deployment sites. It adopts a highly integrated design and integrates the following components according to their functions: an integrated cockpit, an external power supply board, a power control board, a system startup board, a simulated seat, a main control computer, a high-performance computer, a positioner, a certain type of XR helmet glasses (offline version), a simulated joystick, a simulated throttle lever, and rudder pedals. It is transported in an integrated package and the power cord and network cable are used to achieve unified power supply and data exchange for the simulation system during use. When facing emergencies, pilots not only need to master essential flying skills but also possess strong psychological qualities, including calmness, decisiveness, and adaptability. Cultivating and training these psychological qualities often requires a realistic or highly simulated environment, which traditional flight simulation training devices cannot provide. Therefore, we propose a flight simulation training device based on virtual reality. Summary of the Invention

[0003] The purpose of the present invention is to provide a flight simulation training device based on virtual reality to solve the problems raised in the above background technology.

[0004] To achieve the above-mentioned object, the present invention provides the following technical solution: a virtual reality-based flight simulation training device, comprising an integrated cockpit, an operating console mounted on the integrated cockpit, and a seat mounted on the integrated cockpit, wherein a support device is provided at the bottom of the seat, and a mounting cavity is provided at the bottom of the integrated cockpit; An emergency simulation training device is provided at the installation cavity, and the emergency simulation training device cooperates with the support device to perform emergency simulation training on the pilot sitting on the seat; The integrated cockpit is provided with a control device, and the control device is connected to the emergency simulation training device.

[0005] The support device includes a support column, a support seat, a roller and a support spring. There are multiple support columns, and the multiple support columns are fixedly installed around the bottom of the seat. The bottom of the support column is located inside the installation cavity, and the support seat is installed at the bottom of the support column. The support column is slidably connected to the integrated cockpit, and the roller is rotatably connected to the support seat, and the roller is connected to the emergency simulation training device. The support spring is sleeved on the outside of the support column, and the top and bottom ends of the support spring are fixedly connected to the bottom of the seat and the integrated cockpit respectively.

[0006] The emergency simulation training device includes a support rod, a support platform, a rotating member, a lifting member and a synchronous connecting member. The support rod is rotatably connected to the bottom end of the installation cavity through a bearing seat, and the support platform is fixedly installed on the support rod. The plurality of rollers are located on the support platform. The rotating member is installed inside the installation cavity, and the rotating member is used to drive the support rod. The support platform is surrounded by a plurality of movable openings, the lifting member is installed inside the installation cavity, and the lifting member is connected to the plurality of movable openings, the synchronous connecting member is connected to the lifting member, and the synchronous connecting member is connected to the control device, and the emergency simulation training device is provided to achieve the purpose of emergency simulation training for pilots.

[0007] Among them, the rotating part includes a rotating motor, a first rotating gear and a second rotating gear. The rotating motor is fixedly installed inside the installation cavity, and the output end of the rotating motor is fixedly connected to the first rotating gear. The first rotating gear is meshed with the second rotating gear, and the second rotating gear is fixedly sleeved on the outside of the support rod. Through the rotating part provided, the support rod is driven.

[0008] The lifting member includes a lifting block, a limiting member, a guide ring, an extension plate, a reinforcement plate and a matching member. There are multiple lifting blocks, and the multiple lifting blocks slide through the moving opening respectively. A lifting inclined surface is provided on one side of the lifting block. There are multiple limiting members, and the multiple limiting members are respectively located on one side of the inside of the moving opening. The guide ring is slidably connected to the outside of the plurality of jacking blocks, and a positioning ring is installed on the inner ring of the guide ring. A limiting slide groove is provided on the outside of the jacking block and at a position corresponding to the positioning ring. The positioning ring is slidably connected to the plurality of limiting slide grooves. There are multiple extension plates, and the multiple extension plates are fixedly installed around the outside of the guide ring. A reinforcement rod slides through the extension plate, and the multiple reinforcement rods are fixedly installed inside the installation cavity; The reinforcing plate is fixedly mounted on the outside of the guide ring, and two fittings are provided. The two fittings are connected to the reinforcing plate, and both fittings are connected to the synchronous connecting piece. The lifting piece is provided to lift the roller.

[0009] Among them, the limiting member includes a limiting block, the limiting block is T-shaped, and one end of the limiting block is fixedly connected to one side of the inside of the moving port, a limiting groove is provided on one side of the lifting block and corresponds to the position of the limiting block, and the lifting block is slidingly connected to the limiting block through the limiting groove, and the limiting member is provided to achieve the function of limiting and guiding the lifting block.

[0010] Among them, the matching parts include a lifting plate, a guide rod and a moving block. The lifting plate is fixedly installed on one side of the bottom of the reinforcing plate, and the guide rod is fixedly installed on the side of the lifting plate away from the reinforcing plate. The moving block is provided with an inclined groove, and the guide rod slides through the inclined groove. The moving block is slidably connected inside the installation cavity. The moving block is connected to the synchronous connecting part, and the guide ring is connected through the matching parts.

[0011] Wherein, the synchronous connecting member includes a moving screw, a first spur bevel gear, a second spur bevel gear and a connecting rod, the moving screw is provided with two, the two moving screws respectively pass through the two moving blocks, and the moving screw is threadedly connected to the moving block, the outer side of the moving screw is rotatably sleeved with two fixed plates, and the fixed plates are installed inside the mounting cavity, the first spur bevel gear is fixedly installed at one end of the moving screw, and the first spur bevel gear is meshed with the second spur bevel gear, and the two ends of the connecting rod are respectively fixedly connected to the two second spur bevel gears; Two connecting plates are rotatably sleeved on the outer side of the connecting rod, and the two connecting plates are fixedly installed at the bottom end of the installation cavity. The connecting rod is connected to the control device, and through the synchronous connecting piece, the two moving blocks are connected and driven.

[0012] In which, the control device includes a control rod, a rotating seat, a rotating shaft, a side panel and a driving member. The integrated cockpit is provided with a sliding port at the front end of the seat, and the sliding port is connected to the mounting cavity. The control rod slides through the sliding port, and the rotating seat is fixedly installed at the bottom of the control rod. The rotating seat is U-shaped, and the rotating seat is fixedly sleeved on the outside of the rotating shaft. There are two side panels, and both side panels are fixedly installed at the bottom end of the mounting cavity, and the two side panels are rotatably connected to the two ends of the rotating shaft. The driving member is installed on the rotating shaft, and the driving member is connected to the connecting shaft. Through the control device provided, the function of adjusting and controlling the state of the seat is realized.

[0013] Among them, the driving member includes a first driving gear and a second driving gear, the first driving gear is fixedly sleeved on the outside of the rotating shaft, and the second driving gear is fixedly sleeved on the outside of the connecting rod, the first driving gear is meshed and connected with the second driving gear, and the connecting rod is synchronously driven by the provided driving member.

[0014] The present invention has at least the following beneficial effects: 1. When in use, the present invention provides support for the seat through the provided support device. Simultaneously, the provided emergency simulation training device can simulate emergency situations during pilot training. The present invention simulates emergency situations by vibrating the seat, allowing the pilot to promptly control the situation through the control device. However, if the pilot's mental state is poor and they are unable to accurately operate the control device in such situations, the seat's vibration will be more intense, further training the pilot's mental state in the event of an emergency. 2. The seat of the present invention adopts a design in which the contact surface inclination angle imitates the HTY-8 flight seat, ensuring that the seat interference feeling during the pilot's body movements such as turning the head and turning around is basically consistent with the actual installation. BRIEF DESCRIPTION OF THE DRAWINGS

[0015] Figure 1 It is a schematic diagram of the overall structure of the present invention; Figure 2 It is a side view of the overall structure of the present invention; Figure 3 This is the main view of the overall structure of the present invention; Figure 4 It is a top view of the overall structure of the present invention; Figure 5 This is a schematic diagram of the seat structure of the present invention; Figure 6 This is a schematic diagram of the internal structure of the installation cavity of the present invention; Figure 7 This is a schematic diagram of the side panel structure of the present invention; Figure 8 This is a schematic diagram of the support column structure of the present invention; Figure 9 This is a schematic diagram of the support platform structure of the present invention; Figure 10 This is a schematic diagram of the guide ring structure of the present invention; Figure 11 This is a schematic diagram of the reinforcing plate structure of the present invention; Figure 12 This is a schematic diagram of the support rod structure of the present invention; Figure 13 This is a schematic diagram of the positioning ring structure of the present invention; Figure 14 This is a schematic diagram of the support plate structure of the present invention; Figure 15 This is a schematic diagram of the lifting block structure of the present invention; Figure 16 It is a schematic diagram of the structure of the limiting member of the present invention.

[0016] In the figure: 1-integrated cockpit; 11-mounting cavity; 12-slide; 2-operating table; 3-seat; 4-support device; 41-support column; 42-support seat; 43-roller; 44-support spring; 5-emergency simulation training device; 51-support rod; 52-support table; 521-moving mouth; 53-rotating member; 531-rotating motor; 532-first rotating gear; 533-second rotating gear; 6-control device; 61-control rod; 62-rotating seat; 63-rotating shaft; 64-side plate; 65-driving member; 651-first driving Gear; 652-second drive gear; 7-lifting member; 71-lifting block; 711-limiting groove; 712-slide groove; 72-limiting member; 721-limiting block; 73-guide ring; 74-extension plate; 75-reinforcement plate; 76-matching member; 761-lifting plate; 762-guide rod; 763-moving block; 77-positioning ring; 78-reinforcement support rod; 8-synchronizing connecting member; 81-moving screw rod; 811-fixed plate; 82-first straight bevel gear; 83-second straight bevel gear; 84-connecting rod; 85-connecting plate; 9-lifting plate. DETAILED DESCRIPTION

[0017] The following will clearly and completely describe the technical solutions in the embodiments of the present invention in conjunction with the accompanying drawings. Obviously, the described embodiments are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without making creative efforts are within the scope of protection of the present invention.

[0018] Example 1 See also Figures 1 to 5 A virtual reality-based flight simulation training device includes an integrated cockpit 1, an operating console 2 mounted on the integrated cockpit 1, and a seat 3 mounted on the integrated cockpit 1. The simulator is a highly integrated product with pre-assembled internal structures and wiring. Therefore, disassembly or assembly of the simulator requires only a two-person support team. It primarily consists of an integrated cockpit, an external power supply board, a power control board, a system startup board, a simulated seat 3, a high-performance computer, a positioner, an offline version of a certain type of XR helmet glasses, a simulated joystick, a simulated throttle lever, and rudder pedals. The integrated cockpit 1 adopts an integrated structural design and is made entirely of aluminum alloy. The lightweight structure design keeps the total weight of the cockpit under 110kg, excluding electronic products such as computers and monitors. The internal structure, dimensions and layout of the cockpit are designed and laid out based on the internal structure of the J-16 aircraft. The left control panel adopts a movable structure design to facilitate trainees to enter and exit the cockpit. The backrest of the simulated seat 3 adopts the inclination angle of the HTY-8 seat 3. To ensure a user experience that closely resembles actual combat, the simulator's seat 3 features a contact surface angle that mimics the HTY-8 flight seat 3. This ensures that the pilot's body movements, such as turning their head and turning, are disturbed by the seat 3 in a manner consistent with the actual seat 3. Seat 3 utilizes a hardened sponge covered in canvas for support. The headrest and backrest are split, allowing the headrest to be removed and inserted between the joystick and the packaging during transport, reducing the transport height and providing cushioning for the joystick, providing better protection during transport. A support device 4 is provided at the bottom of the seat 3, and a mounting cavity 11 is provided at the bottom of the integrated cabin 1; See also Figures 6 to 8 The support device 4 includes a support column 41, a support seat 42, a roller 43 and a support spring 44. There are multiple support columns 41, and the multiple support columns 41 are fixedly installed around the bottom of the seat 3. The bottom of the support column 41 is located inside the installation cavity, and the support seat 42 is installed at the bottom of the support column 41. The support column 41 is slidably connected to the integrated cockpit 1, the roller 43 is rotatably connected to the support seat 42, and the roller 43 is connected to the emergency simulation training device 5; The support spring 44 is sleeved on the outside of the support column 41, and the top and bottom ends of the support spring 44 are fixedly connected to the bottom of the seat 3 and the integrated cabin 1 respectively; Furthermore, the plurality of support columns 41 are provided with reinforcing ribs inside, thereby ensuring the support strength of the support columns 41 and enabling the support columns 41 to provide stable support. An emergency simulation training device 5 is provided at the mounting cavity 11, and the emergency simulation training device 5 cooperates with the support device 4 to perform emergency simulation training on the pilot sitting on the seat 3; See also Figures 6 to 16 The emergency simulation training device 5 includes a support rod 51, a support platform 52, a rotating member 53, a lifting member 7 and a synchronous connecting member 8. The support rod 51 is rotatably connected to the bottom end of the installation cavity 11 through a bearing seat, and the support platform 52 is fixedly installed on the support rod 51. A plurality of rollers 43 are located on the support platform 52. The rotating member 53 is installed inside the installation cavity 11, and the rotating member 53 is used to drive the support rod 51; The support platform 52 is provided with a plurality of movement openings 521 around it. In the present invention, the width of the roller 43 is greater than the width of the movement openings 521, thereby ensuring that the roller 43 rolls along the plurality of movement openings 521 of the support platform 52. The lifting member 7 is installed inside the installation cavity 11, and the lifting member 7 is connected to the multiple moving ports 521, the synchronous connecting member 8 is connected to the lifting member 7, and the synchronous connecting member 8 is connected to the control device 6; See also Figure 12The rotating member 53 includes a rotating motor 531, a first rotating gear 532 and a second rotating gear 533. The rotating motor 531 is fixedly installed inside the installation cavity 11, and the output end of the rotating motor 531 is fixedly connected to the first rotating gear 532. The first rotating gear 532 is meshed with the second rotating gear 533, and the second rotating gear 533 is fixedly sleeved on the outside of the support rod 51.

[0019] See also Figures 9 to 11 The lifting member 7 includes a lifting block 71, a limiting member 72, a guide ring 73, an extension plate 74, a reinforcement plate 75 and a matching member 76. There are multiple lifting blocks 71, and the multiple lifting blocks 71 slide through the moving opening 521 respectively. A lifting inclined surface is provided on one side of the lifting block 71. At the same time, in this embodiment, the inclined surface angles of the multiple lifting inclined surfaces are in the same direction. There are multiple limiting members 72, and the multiple limiting members 72 are respectively located on one side of the inside of the moving opening 521; The guide ring 73 is slidably connected to the outside of the plurality of lifting blocks 71, and a positioning ring 77 is installed on the inner ring of the guide ring 73. A sliding groove 712 is provided on the outside of the lifting block 71 and at a position corresponding to the positioning ring 77. The positioning ring 77 is slidably connected to the plurality of sliding grooves 712. There are multiple extension plates 74, which are fixedly mounted around the outside of the guide ring 73. A reinforcement rod 78 slides through the extension plate 74, and the reinforcement rods 78 are fixedly mounted inside the mounting cavity 11. The reinforcing plate 75 is fixedly mounted on the outside of the guide ring 73 . Two fitting pieces 76 are provided. The two fitting pieces 76 are connected to the reinforcing plate 75 , and both fitting pieces 76 are connected to the synchronous connecting piece 8 .

[0020] See also Figure 16 The limiting member 72 includes a limiting block 721, which is T-shaped, and one end of the limiting block 721 is fixedly connected to one side of the inside of the moving port 521. A limiting groove 711 is provided on one side of the lifting block 71 and corresponds to the position of the limiting block 721, and the lifting block 71 is slidably connected to the limiting block 721 through the limiting groove 711.

[0021] The mating part 76 includes a lifting plate 761, a guide rod 762 and a moving block 763. The lifting plate 761 is fixedly installed on one side of the bottom of the reinforcing plate 75. The guide rod 762 is fixedly installed on the side of the lifting plate 761 away from the reinforcing plate 75. The moving block 763 is provided with an inclined groove 7631, and the guide rod 762 slides through the inclined groove 7631. The moving block 763 is slidably connected inside the installation cavity 11, and the moving block 763 is connected to the synchronous connecting part 8.

[0022] See also Figures 8 to 10The synchronous connecting member 8 includes a moving screw rod 81, a first spur gear 82, a second spur gear 83 and a connecting rod 84. The moving screw rod 81 is provided with two, and the two moving screw rods 81 respectively pass through the two moving blocks 763. At the same time, in this embodiment, the thread directions of the two moving screw rods 81 are opposite, further ensuring that the two moving screw rods 81 can provide the two moving blocks 763 with the same driving force in the same direction when rotating in the opposite directions, ensuring that the two moving blocks 763 move synchronously, and the moving screw rod 81 is threadedly connected to the moving block 763. Two fixed plates 811 are rotatably sleeved on the outer side of the moving screw rod 81, and the fixed plate 811 is installed in the installation cavity 11. The first spur gear 82 is fixedly installed on one end of the moving screw rod 81, and the first spur gear 82 is meshed with the second spur gear 83. The two ends of the connecting rod 84 are respectively fixedly connected to the two second spur gears 83; Two connecting plates 85 are rotatably sleeved on the outside of the connecting rod 84, and the two connecting plates 85 are fixedly mounted on the bottom end of the interior of the mounting cavity 11. The connecting rod 84 is connected to the control device 6. Specific implementation process: In this embodiment, when the pilot sits on the seat 3 for simulated flight training, during the training process, the console is electrically connected to the rotary motor 531, and then the rotary motor 531 is operated, so that the first rotary gear 532 drives the second rotary gear 533 to rotate, and when the second rotary gear 533 rotates, the support rod 51 further drives the support platform 52 to rotate, and when the support platform 52 rotates, it synchronously drives the lifting block 71 to rotate through the multiple moving ports 521, and further the support platform 52 drives the multiple The lifting block 71 rotates around the bottom of the plurality of rollers 43. When the lifting block 71 contacts the rollers 43, the rollers 43 and the support columns 41 move upward along the installation cavity 11. When the plurality of support columns 41 move upward, the seat 3 moves upward. When the rollers 43 are separated from the lifting block 71, the plurality of support columns 41 move downward in the vertical direction, and the seat 3 moves downward, thereby causing the pilot on the seat 3 to shake up and down as the seat 3 is in the integrated cockpit 1. This further serves the purpose of conducting simulated training in emergency situations during simulated flight. Then, the pilot makes a judgment in this state and operates the control device 6; When the pilot makes an operational error, he pulls the control device 6 toward his body, further causing the connecting rod 84 to drive the second spur helical gears at both ends to rotate. When the two second spur helical gears rotate, they respectively drive the two first spur helical gears to rotate synchronously, and the first spur helical gears drive the moving screw 81 thereon to rotate. When the two moving screws 81 rotate synchronously and in opposite directions, since the thread directions of the two moving screws 81 are set in opposite directions, the two moving blocks 763 maintain the same driving force, further causing the two moving blocks 763 to move along the direction of the support platform 52. When the two moving blocks 763 move synchronously, due to the limiting effect of the inclined groove 7631 and the limiting effect of the guide ring 73 on the multiple lifting blocks 71, the reinforcing plate 75 further drives the guide ring 73 to move upward. When the guide ring 73 moves upward, the belt drives the multiple lifting blocks 71 along the moving opening 521 through the positioning ring 77. At this time, the "protruding" area of ​​the multiple lifting blocks 71 relative to the support platform 52 is larger, resulting in an increase in the height difference of the roller 43 falling, thereby further increasing the vibration amplitude of the seat 3. When the pilot operates correctly, the plurality of lifting blocks 71 are driven downward along the movable opening 521 of the support platform 52 until the top ends of the lifting blocks 71 are moved downward to the upper surface of the movable opening 521. At this time, the plurality of rollers 43 are moved along the support platform 52, ensuring smooth movement of the plurality of rollers 43. At this time, the seat 3 does not vibrate up and down. In the above process, the pilot can make a judgment when encountering an emergency. The present invention uses the shaking of the seat 3 as a preferred embodiment.

[0023] The integrated cockpit 1 is provided with a control device 6 , and the control device 6 is connected to the emergency simulation training device 5 .

[0024] See also Figures 7 to 10The control device 6 includes a control rod 61, a rotating seat 62, a rotating shaft 63, a side plate 64 and a driving member 65. The integrated cockpit 1 is provided with a sliding port 12 at the front end of the seat 3, and the sliding port 12 is connected to the mounting cavity 11. The control rod 61 slides through the sliding port 12, and the rotating seat 62 is fixedly installed at the bottom of the control rod 61. At the same time, in this embodiment, a rubber ring is provided on the outer side of the top of the control rod 61 to facilitate manual control by the pilot. The rotating seat 62 is U-shaped and fixedly sleeved on the outer side of the rotating shaft 63. There are two side plates 64, both of which are fixedly installed at the bottom end of the mounting cavity 11, and the two side plates 64 are rotatably connected to the two ends of the rotating shaft 63. The driving member 65 is installed on the rotating shaft 63, and the driving member 65 is connected to the connecting shaft. At the same time, in this embodiment, the rotating shaft 63 is a damping type setting, thereby ensuring that the rotating shaft 63 can still be stably connected to the two side plates 64 when not subject to external force.

[0025] The driving member 65 includes a first driving gear 651 and a second driving gear 652. The first driving gear 651 is fixedly sleeved on the outside of the rotating shaft 63, and the second driving gear 652 is fixedly sleeved on the outside of the connecting rod 84. The first driving gear 651 and the second driving gear 652 are meshed and connected. Specific implementation process: When the pilot makes a control error, he holds the control stick 61 and rotates it in the direction of the seat 3. At this time, the first drive gear 651 is driven to rotate via the rotating shaft 63. When the first drive gear 651 rotates, the second drive gear 652 is further rotated. When the second drive gear 652 rotates, the connecting rod 84 is further rotated. Then, through the synchronous connecting member 8, the guide ring 73 drives the multiple lifting blocks 71 to move upward along the support platform 52. At the same time, when the pilot controls correctly, the control rod 61 is moved in the direction away from the seat 3. Then, through the connection of the synchronous connecting member 8, it is ensured that the seat 3 can be changed from a shaking state to a stable state.

[0026] Example 2 See also Figure 11 and Figures 13 to 15 , Example 2 is a further supplementary explanation of Example 1, specifically: the bottom of the support platform 52 is slidably connected to two lifting plates 9, the two lifting plates 9 are respectively fixedly connected to four reinforcing support rods 78, and the lifting plates 9 are set in an arc shape; Therefore, by further providing the two lifting plates 9 , the support platform 52 can be auxiliary supported when the support platform 52 rotates along with the support rod 51 , thereby ensuring the stability of the rotation of the support platform 52 .

[0027] It should be noted that, in this document, relational terms such as first and second, etc., are used only to distinguish one entity or operation from another entity or operation, and do not necessarily require or imply any actual relationship or order between these entities or operations. Moreover, the terms "comprises," "comprising," or any other variations thereof are intended to cover non-exclusive inclusion, such that a process, method, article, or apparatus that includes a list of elements includes not only those elements but also other elements not explicitly listed, or elements inherent to such process, method, article, or apparatus.

[0028] While embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that various changes, modifications, substitutions, and variations may be made to these embodiments without departing from the principles and spirit of the invention, and that the scope of the invention is defined by the appended claims and their equivalents.

Claims

1. A flight simulation training device based on virtual reality, comprising an integrated cockpit (1), an operating table (2) installed on the integrated cockpit (1), and a seat (3) installed on the integrated cockpit (1), characterized in that: The seat (3) is provided with a support device (4) at the bottom, and the integrated cabin (1) is provided with a mounting cavity (11) at the bottom; An emergency simulation training device (5) is provided at the installation cavity (11), and the emergency simulation training device (5) cooperates with the support device (4) to perform emergency simulation training on a pilot sitting on the seat (3); The integrated cockpit (1) is provided with a control device (6), and the control device (6) is connected to the emergency simulation training device (5).

2. A virtual reality based flight simulation training device according to claim 1, characterized in that: The support device (4) comprises a support column (41), a support seat (42), a roller (43) and a support spring (44); a plurality of the support columns (41) are provided, and the plurality of support columns (41) are fixedly mounted around the bottom of the seat (3); the bottom of the support column (41) is located inside the mounting cavity, and the support seat (42) is mounted on the bottom of the support column (41); the support column (41) is slidably connected to the integrated cabin (1), the roller (43) is rotatably connected to the support seat (42), and the roller (43) is connected to the emergency simulation training device (5); The support spring (44) is sleeved on the outside of the support column (41), and the top and bottom ends of the support spring (44) are fixedly connected to the bottom of the seat (3) and the integrated cabin (1) respectively.

3. A virtual reality based flight simulation training device according to claim 2, characterized in that: The emergency simulation training device (5) comprises a support rod (51), a support platform (52), a rotating member (53), a lifting member (7) and a synchronous connecting member (8), wherein the support rod (51) is rotatably connected to the bottom end inside the installation cavity (11) via a bearing seat, and the support platform (52) is fixedly mounted on the support rod (51), a plurality of rollers (43) are located on the support platform (52), the rotating member (53) is mounted inside the installation cavity (11), and the rotating member (53) is used to drive the support rod (51); The support platform (52) is surrounded by a plurality of movable openings (521); the lifting member (7) is installed inside the installation cavity (11), and the lifting member (7) is connected to the plurality of movable openings (521); the synchronous connecting member (8) is connected to the lifting member (7), and the synchronous connecting member (8) is connected to the control device (6).

4. A virtual reality based flight simulation training device according to claim 3, characterized in that: The rotating member (53) comprises a rotating motor (531), a first rotating gear (532) and a second rotating gear (533); the rotating motor (531) is fixedly mounted inside the mounting cavity (11); an output end of the rotating motor (531) is fixedly connected to the first rotating gear (532); the first rotating gear (532) is meshedly connected to the second rotating gear (533); and the second rotating gear (533) is fixedly sleeved on the outside of the support rod (51).

5. A virtual reality based flight simulation training device according to claim 3, characterized in that: The lifting member (7) comprises a lifting block (71), a limiting member (72), a guide ring (73), an extension plate (74), a reinforcing plate (75) and a matching member (76); a plurality of the lifting blocks (71) are provided, and the plurality of the lifting blocks (71) respectively slide through the moving opening (521); a lifting inclined surface is provided on one side of the lifting block (71); a plurality of the limiting members (72) are provided, and the plurality of the limiting members (72) are respectively located on one side of the inside of the moving opening (521); The guide ring (73) is slidably connected to the outside of the plurality of lifting blocks (71), and a positioning ring (77) is installed on the inner ring of the guide ring (73), and a slide groove (712) is provided on the outside of the lifting block (71) and at a position corresponding to the positioning ring (77), and the positioning ring (77) is slidably connected to the plurality of slide grooves (712); A plurality of the extension plates (74) are provided, and the plurality of the extension plates (74) are fixedly mounted around the outside of the guide ring (73); a reinforcing support rod (78) is slidably penetrated through the extension plate (74), and the plurality of reinforcing support rods (78) are fixedly mounted inside the mounting cavity (11); The reinforcing plate (75) is fixedly mounted on the outside of the guide ring (73), and two matching pieces (76) are provided. The two matching pieces (76) are connected to the reinforcing plate (75), and the two matching pieces (76) are both connected to the synchronous connecting piece (8).

6. A virtual reality based flight simulation training device according to claim 5, characterized in that: The limiting member (72) comprises a limiting block (721), the limiting block (721) being T-shaped, and one end of the limiting block (721) being fixedly connected to one side of the inside of the moving opening (521), a limiting groove (711) being provided on one side of the lifting block (71) and corresponding to the position of the limiting block (721), and the lifting block (71) being slidably connected to the limiting block (721) via the limiting groove (711).

7. A virtual reality based flight simulation training device according to claim 5, characterized in that: The matching component (76) includes a lifting plate (761), a guide rod (762) and a moving block (763); the lifting plate (761) is fixedly mounted on one side of the bottom of the reinforcing plate (75); the guide rod (762) is fixedly mounted on the side of the lifting plate (761) away from the reinforcing plate (75); an inclined groove (7631) is provided on the moving block (763), and the guide rod (762) slides through the inclined groove (7631); the moving block (763) is slidably connected inside the installation cavity (11); and the moving block (763) is connected to the synchronous connecting component (8).

8. A virtual reality based flight simulation training device according to claim 7, characterized in that: The synchronous connecting member (8) comprises a moving screw (81), a first spur bevel gear (82), a second spur bevel gear (83) and a connecting rod (84); two moving screws (81) are provided, and the two moving screws (81) respectively penetrate two moving blocks (763), and the moving screw (81) is threadedly connected to the moving blocks (763); two fixing plates (811) are rotatably sleeved on the outer side of the moving screw (81), and the fixing plates (811) are installed inside the installation cavity (11); the first spur bevel gear (82) is fixedly installed on one end of the moving screw (81), and the first spur bevel gear (82) is meshedly connected to the second spur bevel gear (83); and both ends of the connecting rod (84) are fixedly connected to the two second spur bevel gears (83); Two connecting plates (85) are rotatably sleeved on the outside of the connecting rod (84), and the two connecting plates (85) are fixedly mounted on the bottom end inside the mounting cavity (11). The connecting rod (84) is connected to the control device (6).

9. A virtual reality based flight simulation training device according to claim 8, characterized in that: The control device (6) comprises a control rod (61), a rotating seat (62), a rotating shaft (63), a side plate (64) and a driving member (65); the integrated cockpit (1) is provided with a sliding opening (12) at the front end of the seat (3), and the sliding opening (12) is communicated with the mounting cavity (11); the control rod (61) slides through the sliding opening (12), and the rotating seat (62) is fixedly mounted at the bottom of the control rod (61); the rotating seat (62) is U-shaped, and the rotating seat (62) is fixedly sleeved on the outside of the rotating shaft (63); two side plates (64) are provided, and the two side plates (64) are fixedly mounted at the bottom end of the mounting cavity (11), and the two side plates (64) are rotatably connected to the two ends of the rotating shaft (63); the driving member (65) is mounted on the rotating shaft (63), and the driving member (65) is connected to the connecting shaft.

10. A virtual reality based flight simulation training device according to claim 9, characterized in that: The driving member (65) comprises a first driving gear (651) and a second driving gear (652); the first driving gear (651) is fixedly sleeved on the outside of the rotating shaft (63), and the second driving gear (652) is fixedly sleeved on the outside of the connecting rod (84); the first driving gear (651) and the second driving gear (652) are meshingly connected.

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