Flight simulator

Abstract

The embodiment of the utility model provides a flight simulator which comprises a simulation platform, a simulator and a carrying assembly, the simulator is detachably arranged on the simulation platform, the simulator comprises a forecabin assembly, the forecabin assembly comprises a forecabin body and a forecabin platform, the forecabin body is detachably connected with the forecabin platform, and the forecabin platform is detachably connected with the forecabin platform. A first mounting groove is formed in the bottom of the forecabin platform, the carrying assembly comprises a first air floating plate, and the first air floating plate can be mounted in the first mounting groove to assist in carrying the forecabin platform. According to the flight simulator, the first air floating plate is adopted to carry the forecabin assembly, and the forecabin assembly is in a suspended state during carrying, so that the friction force between the forecabin assembly and the ground or the simulation platform can be reduced, the forecabin assembly can be conveniently moved, and due to the fact that the force needed by movement is greatly reduced, the movement is convenient. And the limitation on the moving direction and angle is small, so that the moving efficiency of the forecabin assembly is improved.

Description

Technical Field

[0001] The utility model relates to the technical field of aircraft simulation equipment, in particular to a flight simulator. Background Art

[0002] A flight simulator is a highly complex technical system that provides pilots with a safe and cost-effective training platform by accurately simulating an aircraft's flight environment, operating interfaces, and flight conditions. A flight simulator typically includes a cockpit, visual display system, motion platform, and other controls consistent with the target aircraft model, capable of simulating the entire flight process, from takeoff to landing, as well as various weather and emergency scenarios. Flight simulators are widely used in pilot training, aircraft design verification, and aviation safety research. They not only improve the efficiency and safety of flight training but also provide important support for the continued development and technological innovation of the aviation industry.

[0003] Existing methods for replacing the cockpit of a flight simulator mostly involve using pulleys and slide rails, which is laborious to move and inconvenient to replace. Utility Model Content

[0004] The utility model provides a flight simulator, which is used to solve the defect of the flight simulator in the prior art that it is laborious to move, and realizes efficient replacement of the flight simulator.

[0005] The utility model provides a flight simulator, comprising:

[0006] Simulation platform;

[0007] a simulator, the simulator being detachably mounted on the simulation platform, the simulator comprising a front cabin assembly, the front cabin assembly comprising a front cabin body and a front cabin platform, the front cabin body being detachably connected to the front cabin platform, and a first mounting slot being provided at a bottom of the front cabin platform;

[0008] A transport assembly includes a first air floating plate, and the first air floating plate can be installed in the first installation groove to assist in transporting the front cabin platform.

[0009] In some embodiments, the simulator further comprises a rear cabin assembly, the rear cabin assembly being detachably connected to the front cabin assembly, the rear cabin assembly comprising a rear cabin body and a rear cabin platform, the rear cabin body being connected to the front cabin body, the rear cabin body being detachably connected to the rear cabin platform, and a second mounting slot being provided at the bottom of the rear cabin platform;

[0010] The transport assembly includes a second air floating plate, which can be installed in the second installation groove to assist in transporting the rear cabin platform.

[0011] In some embodiments, the simulator further comprises:

[0012] A ball screen, wherein the ball screen cover is arranged on the outer peripheral side of the front cabin assembly;

[0013] A gantry is provided between the rear cabin assembly and the front cabin assembly, and the gantry is connected to the spherical screen. The gantry includes a conversion door, and the conversion door is detachably provided on the gantry. The conversion door is provided with a matching hole, and the shape of the matching hole is adapted to the cross-sectional shape of the front cabin body.

[0014] In some embodiments, the first air flotation plate and the second air flotation plate both include a plate body and an air bag, the air bag is arranged at the bottom of the plate body and is sealed with the plate body, the plate body is provided with an air inlet and an air outlet, the air outlet is arranged at the bottom of the plate body, and the air inlet and the air outlet are both connected to the air bag.

[0015] In some embodiments, the plate body is provided with multiple air cavities, the multiple air bags are connected one by one with the multiple air cavities, the multiple air cavities are arranged at intervals on the outer periphery of the air outlet, and each air cavity is connected with the air outlet.

[0016] In some embodiments, the transport assembly further includes a lifting platform, which is disposed behind the simulation platform.

[0017] In some embodiments, the rear cabin body includes a bulkhead, a door panel and a bottom platform, the door panel is detachably connected to the bulkhead, the bottom platform is arranged at the bottom of the bulkhead, and the rear cabin platform is embedded on the bottom platform.

[0018] In some embodiments, a plurality of guide wheels arranged at intervals are provided on both sides of the front cabin platform and on both sides of the rear cabin platform.

[0019] In some embodiments, there are multiple first mounting grooves, and there are multiple first air floating plates, and the multiple first air floating plates are arranged in a one-to-one correspondence with the multiple first mounting grooves.

[0020] In some embodiments, there are multiple second mounting grooves, and there are multiple second air floating plates, and the multiple second air floating plates are arranged in a one-to-one correspondence with the multiple second mounting grooves.

[0021] The flight simulator implemented in the present invention utilizes a first air float to transport the front cabin assembly. Since the front cabin assembly is in a suspended state during transport, i.e., the bottom surface of the front cabin assembly does not contact the surface of the ground or simulation platform on which it is placed, friction between the front cabin assembly and the ground or simulation platform is reduced. This allows for easy omnidirectional movement, in-place rotation, and other forms of movement that are difficult to achieve with wheeled transport. During transport, only one person is required to push the front cabin assembly. Because the force required for movement is significantly reduced and the restrictions on movement direction and angle are relatively small, the efficiency of moving the front cabin assembly is improved. BRIEF DESCRIPTION OF THE DRAWINGS

[0022] In order to more clearly illustrate the technical solutions in the present invention or the prior art, a brief introduction will be given below to the drawings required for use in the embodiments or the description of the prior art. Obviously, the drawings described below are some embodiments of the present invention. For ordinary technicians in this field, other drawings can be obtained based on these drawings without paying any creative work.

[0023] Figure 1 It is a structural schematic diagram of a flight simulator provided by the utility model.

[0024] Figure 2 The utility model is a schematic diagram of the explosion structure of the flight simulator provided by the utility model.

[0025] Figure 3 It is a structural schematic diagram of the front cabin assembly and the first support seat provided by the utility model.

[0026] Figure 4 It is a structural schematic diagram of the rear cabin assembly provided by the utility model.

[0027] Figure 5 It is a structural schematic diagram of the rear cabin assembly provided by the utility model from another perspective.

[0028] Figure 6 It is a structural schematic diagram of the gantry provided by the utility model.

[0029] Figure 7 It is a structural schematic diagram of the front cabin platform provided by the utility model.

[0030] Figure 8 It is a structural schematic diagram of the first air floating plate or the second air floating plate provided by the utility model.

[0031] Figure 9 yes Figure 8 Schematic diagram of the cross section at AA in the middle.

[0032] Figure 10 It is a structural schematic diagram of the rear cabin platform provided by the utility model.

[0033] Reference numerals:

[0034] 1. Simulation platform; 11. First support base; 12. Second support base;

[0035] 2. Simulator;

[0036] 21. Front cabin assembly; 211. Front cabin body; 212. Front cabin platform; 2121. First mounting slot;

[0037] 22. Rear cabin assembly; 221. Rear cabin body; 2211. Bulkhead; 2212. Door panel; 2213. Bottom platform; 222. Rear cabin platform; 2221. Second mounting slot; 2222. Seat;

[0038] 23. Gantry; 231. Transfer door; 2311. Matching hole; 232. Viewing door; 24. Dome screen; 25. Guide wheel;

[0039] 3. Transport assembly; 31. First air flotation plate; 32. Second air flotation plate;

[0040] 33. Plate; 34. Airbag; 35. Air inlet; 36. Air outlet; 37. Air cavity;

[0041] 38. Lifting platform. DETAILED DESCRIPTION

[0042] To make the purpose, technical solutions, and advantages of the present invention more clear, the following will be combined with the accompanying drawings to clearly and completely describe the technical solutions of the present invention. Obviously, the embodiments described are only some of the embodiments of the present invention, not all of them. 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.

[0043] In the description of the embodiments of the present invention, it should be noted that the terms "center", "longitudinal", "lateral", "upper", "lower", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", etc., indicating the orientation or positional relationship, are based on the orientation or positional relationship shown in the accompanying drawings, and are only for the convenience of describing the embodiments of the present invention and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operate in a specific orientation, and therefore should not be understood as limiting the embodiments of the present invention. In addition, the terms "first", "second", and "third" are used for descriptive purposes only and should not be understood as indicating or implying relative importance.

[0044] In the description of the embodiments of the present invention, it should be noted that, unless otherwise specified or limited, the terms "connected" and "connection" should be understood in a broad sense. For example, they can refer to fixed connections, detachable connections, or integral connections; mechanical connections, electrical connections; direct connections, or indirect connections through an intermediary. Those skilled in the art will understand the specific meanings of the above terms in the embodiments of the present invention based on specific circumstances.

[0045] In the embodiments of the present invention, unless otherwise expressly specified or limited, a first feature being "above" or "below" a second feature may mean that the first and second features are in direct contact, or that the first and second features are in indirect contact through an intermediate medium. Furthermore, a first feature being "above," "above," or "above" a second feature may mean that the first feature is directly above or diagonally above the second feature, or simply means that the first feature is higher in level than the second feature. A first feature being "below," "below," or "below" a second feature may mean that the first feature is directly below or diagonally below the second feature, or simply means that the first feature is lower in level than the second feature.

[0046] In the description of this specification, the description with reference to the terms "one embodiment", "some embodiments", "example", "specific example", or "some examples" means that the specific features, structures, materials or characteristics described in conjunction with the embodiment or example are included in at least one embodiment or example of the embodiment of the utility model. In this specification, the schematic representation of the above terms does not necessarily refer to the same embodiment or example. Moreover, the specific features, structures, materials or characteristics described can be combined in any one or more embodiments or examples in a suitable manner. In addition, those skilled in the art can combine and combine different embodiments or examples described in this specification and the features of different embodiments or examples without contradiction.

[0047] like Figures 1 to 10 As shown, an embodiment of the present utility model provides a flight simulator, which includes a simulation platform 1, a simulator 2 and a transport component 3.

[0048] The simulator 2 is detachably mounted on the simulation platform 1 . The simulator 2 includes a front cabin assembly 21 . The front cabin assembly 21 includes a front cabin and a front cabin platform 212 . The front cabin body 211 is detachably connected to the front cabin platform 212 . A first mounting groove 2121 is provided at the bottom of the front cabin platform 212 .

[0049] The transport assembly 3 includes a first air floating plate 31 . The first air floating plate 31 can be installed in the first installation groove 2121 to assist in transporting the front cabin platform 212 .

[0050] For example, Figure 1As shown, the bottom of the simulation platform 1 is provided with multiple groups of hydraulic rods arranged at intervals, so that the simulation platform 1 can be controlled to achieve movement with multiple degrees of freedom.

[0051] The simulator 2 is modeled after an aircraft to simulate flight operations. The front cabin assembly 21 includes a front cabin body 211 containing a cabin, and a front cabin platform 212 disposed at the bottom of the front cabin body 211. An airbag 34 is disposed at the bottom of the first air float 31, which swells up when inflated.

[0052] When the front cabin assembly 21 of the flight simulator implemented in the present invention needs to be replaced, the connector between the front cabin assembly 21 and the simulation platform 1 is first removed to separate the front cabin assembly 21 from the simulation platform 1. The first air floatation plate 31 is then installed in the first installation slot 2121. An air compressor is then used to inflate the first air floatation plate 31. The airbag 34 of the first air floatation plate 31 gradually expands, thereby gradually increasing the height of the first air floatation plate 31 and gradually lifting the front cabin platform 212 until it is clear of the simulation platform 1. When installing a new front cabin assembly 21, the first air floatation plate 31 is also used to move the front cabin assembly 21 from its original location onto the simulation platform 1.

[0053] The flight simulator implemented in the present invention utilizes a first air-floating plate 31 to transport the front cabin assembly 21. Since the front cabin assembly 21 is in a suspended state during transport, meaning that the bottom surface of the front cabin assembly 21 does not contact the ground or the surface of the simulation platform 1 on which it is placed, friction between the front cabin assembly 21 and the ground or the simulation platform 1 is reduced. This allows for easy 360-degree movement and in-place rotation, which are difficult to achieve with wheeled transport. During transport, only one person is required to push the front cabin assembly 21. Because the force required for movement is significantly reduced and the restrictions on the direction and angle of movement are relatively small, the efficiency of moving the front cabin assembly 21 is improved.

[0054] In some embodiments, the simulator 2 also includes a rear cabin assembly 22, which is detachably connected to the front cabin assembly 21. The rear cabin assembly 22 includes a rear cabin body 221 and a rear cabin platform 222. The rear cabin body 221 is connected to the front cabin body 211. The rear cabin body 221 is detachably connected to the rear cabin platform 222. A second mounting groove 2221 is provided at the bottom of the rear cabin platform 222.

[0055] The transport assembly 3 includes a second air floating plate 32 , which can be installed in the second installation groove 2221 to assist in transporting the rear cabin platform 222 .

[0056] For example, Figure 1 and Figure 2As shown, the rear cabin assembly 22 is located behind the front cabin assembly 21 and is detachably connected to the simulation platform 1. The rear cabin body 221 is connected to the front cabin body 211 to define a cockpit therein. The rear cabin platform 222 is located at the bottom of the rear cabin body 221. The second air floatation plate 32 has a similar structure to the first air floatation plate 31.

[0057] When the rear cabin assembly 22 of the flight simulator implemented in the present invention needs to be replaced, the connector between the rear cabin assembly 22 and the simulation platform is first removed to separate the rear cabin assembly 22 from the simulation platform 1. The rear cabin body 221 is then separated from the rear cabin platform 222. The second air floatation plate 32 is then installed in the second installation slot 2221. An air compressor is then used to inflate the second air floatation plate 32. The airbag 34 at the bottom of the second air floatation plate 32 gradually expands, thereby gradually increasing the height of the second air floatation plate 32 and gradually raising the rear cabin platform 222 until its bottom is separated from the simulation platform 1. When installing a new rear cabin assembly 22, the second air floatation plate 32 is also used to move the rear cabin assembly 22 from its original position to the corresponding position on the simulation platform 1.

[0058] The flight simulator implemented in the present invention utilizes the second air floating plate 32 to facilitate the transportation of the rear cabin assembly 22 , thereby improving transportation efficiency.

[0059] It should be noted that in the present application, different types of cockpits can be replaced by replacing the front cabin component 21 and the rear cabin component 22 without replacing the entire device, thereby facilitating the improvement of simulation efficiency.

[0060] In some embodiments, the simulator 2 further includes a spherical screen 24 and a gantry 23 , and the spherical screen 24 is covered on the outer peripheral side of the front cabin assembly 21 .

[0061] The gantry 23 is arranged between the rear cabin assembly 22 and the front cabin assembly 21, and the gantry 23 is connected to the spherical screen 24. The gantry 23 includes a conversion door 231, and the conversion door 231 is detachably arranged on the gantry 23. The conversion door 231 is provided with a matching hole 2311, and the shape of the matching hole 2311 is adapted to the cross-sectional shape of the front cabin body 211.

[0062] For example, Figure 1 As shown, a visual system is installed on the spherical screen 24 to simulate a real flight environment, and the gantry 23 is used to fix the spherical screen 24. The shape of the conversion door 231 is adapted to the cross-sectional shape of the front cabin body 211.

[0063] When the front cabin assembly 21 is replaced with a different type, the cross-sectional shape of its front cabin body 211 will change. At this time, the conversion door 231 is also replaced with a new type, so that the replaced conversion door 231 is adapted to the front cabin body 211.

[0064] In the flight simulator implemented in the present invention, when the front cabin assembly 21 is replaced, the conversion door 231 is also replaced, so there is no need to replace the entire gantry 23, thereby improving the replacement efficiency of the simulator 2.

[0065] Optionally, viewing hatches 232 are provided on both sides of the conversion door 231 .

[0066] In some embodiments, the first air float plate 31 and the second air float plate 32 both include a plate body 33 and an air bag 34. The air bag 34 is arranged at the bottom of the plate body 33 and is sealed with the plate body 33. An air inlet 35 and an air outlet 36 are provided on the plate body 33. The air outlet 36 is arranged at the bottom of the plate body 33. Both the air inlet 35 and the air outlet 36 are connected to the air bag 34.

[0067] For example, Figure 8 and Figure 9 As shown, the air outlet 36 is provided at the bottom of the plate body 33, and the opening of the air outlet 36 faces the bottom of the plate body 33. After the gas enters the plate body 33 from the air inlet 35, the airbag 34 expands and then flows out from the air outlet 36. During the transportation process, after the gas flows out from the air outlet 36, an air film is formed on the surface of the simulation platform 1 or the ground, thereby achieving the purpose of suspended transportation.

[0068] In some embodiments, a plurality of air cavities 37 are provided in the plate body 33 , and there are a plurality of air bags 34 . The plurality of air bags 34 correspond to and are connected with the plurality of air cavities 37 in a one-to-one manner.

[0069] For example, Figure 8 and Figure 9 As shown, the air cavity 37 is provided at the bottom of the plate body 33, and an air bag 34 is provided under each air cavity 37. The multiple air cavities 37 are arranged in pairs, and correspondingly, the multiple air bags 34 are also arranged in pairs, and an air outlet 36 is provided between the two air cavities 37 arranged in pairs.

[0070] Optionally, in other embodiments, a plurality of the air cavities 37 are arranged at intervals on the outer peripheral side of the air outlet 36, each of the air cavities 37 is connected to the air outlet 36, and the air outlet 36 is located in the middle position of the plurality of air cavities 37. Thus, the distance between each air cavity 37 and the air outlet 36 is consistent, so that the size of each airbag 34 remains consistent, thereby avoiding rollover during transportation.

[0071] In some embodiments, the transport assembly 3 further includes a lifting platform 38 , which is located behind the simulation platform 1 .

[0072] For example, Figure 1 and Figure 2As shown, the lifting platform 38 is used to transfer the simulator 2 between the ground and the simulation platform 1. When the simulator 2 needs to be installed, the simulator 2 is moved from the ground to the lifting platform 38, and then the lifting platform 38 is moved upward to move the simulator 2 onto the simulation platform 1. When the simulator 2 needs to be replaced, the simulator 2 is first moved to the lifting platform 38, and then the lifting platform 38 is lowered to transfer the simulator 2 to the ground.

[0073] In some embodiments, the rear cabin body 221 includes a bulkhead 2211, a door panel 2212 and a bottom platform 2213. The door panel 2212 is detachably connected to the bulkhead 2211. The bottom platform 2213 is located at the bottom of the bulkhead 2211, and the rear cabin platform 222 is embedded in the bottom platform 2213.

[0074] For example, Figure 4 and Figure 5 As shown, the bulkhead 2211 comprises a roof and a wall. The roof and the wall are detachably connected, the roof and the bottom platform 2213 are detachably connected, and the wall and the bottom platform 2213 are detachably connected. A groove is provided on the bottom platform 2213, and the rear cabin platform 222 is embedded in the groove. When the rear cabin platform 222 needs to be replaced, the door panel 2212 is first removed. Then, the rear cabin platform 222 can be simply removed from the groove using the second air floatation plate 32, without having to disassemble the rear cabin body 221. This improves the efficiency of replacing the rear cabin platform 222.

[0075] In some embodiments, a plurality of guide wheels 25 arranged at intervals are provided on both sides of the front cabin platform 212 and both sides of the rear cabin platform 222 .

[0076] For example, Figure 3 、 Figure 7 and Figure 9 As shown, guide wheels 25 are provided on both sides of the front cabin platform 212 and both sides of the rear cabin platform 222. Therefore, when the front cabin platform 212 or the rear cabin platform 222 is transferred, the guide wheels 25 can facilitate the movement of the front cabin platform 212 or the rear cabin platform 222, thereby reducing the friction generated by the relative movement of the sides of the front cabin platform 212 or the rear cabin platform 222 with other objects.

[0077] In some embodiments, there are multiple first installation grooves 2121 , and there are multiple first air floating plates 31 . The multiple first air floating plates 31 are arranged in a one-to-one correspondence with the multiple first installation grooves 2121 .

[0078] For example, Figure 3 and Figure 7 As shown, the number of the first mounting slots 2121 and the number of the first air floating plates 31 are the same, that is, 2-4 first mounting slots 2121 and 2-4 first air floating plates 31 .

[0079] In some embodiments, there are multiple second mounting grooves 2221 , and there are multiple second air floating plates 32 . The multiple second air floating plates 32 are arranged in a one-to-one correspondence with the multiple second mounting grooves 2221 .

[0080] For example, Figure 9 As shown, the number of the second mounting slots 2221 and the number of the second air floating plates 32 are the same, that is, 2-4.

[0081] It is understandable that the first air floating plate 31 and the second air floating plate 32 are designed according to their installation positions, and their structures may be completely the same or different.

[0082] It is understandable that, during the process of transporting the front cabin platform 212 or the rear cabin platform 222 , the compressor always inflates the first air floating plate 31 and the second air floating plate 32 .

[0083] It can be understood that the “detachable” described in the present invention refers to bolt connection.

[0084] The entire process of replacing the simulator 2 with the flight simulator implemented in the present invention is as follows: first, remove the door panel 2212 of the rear cabin assembly 22, then separate the rear cabin platform 222 from the simulator 2, then use the second air floatation plate 32 to remove the rear cabin platform 222 from the groove, then separate the front cabin platform 212 from the simulator 2, and finally use the first air floatation plate 31 to remove the front cabin assembly 21. The above is the disassembly process; the process of installing a new simulator 2 is the reverse of the above process.

[0085] In other embodiments, a first support base 11 and a second support base 12 are provided on the simulator 2. The first support base 11 is connected to the front cabin platform 212 to support the front cabin assembly 21, and the second support base 12 is connected to the rear cabin platform 222.

[0086] Optionally, seats 2222 are provided on the rear cabin platform 222 .

[0087] Finally, it should be noted that the above embodiments are only used to illustrate the technical solutions of the present invention, rather than to limit it. Although the present invention has been described in detail with reference to the aforementioned embodiments, those skilled in the art should understand that they can still modify the technical solutions described in the aforementioned embodiments, or make equivalent replacements for some of the technical features therein. However, these modifications or replacements do not deviate the essence of the corresponding technical solutions from the spirit and scope of the technical solutions of the various embodiments of the present invention.

Claims

1. A flight simulator, characterized in that: include: Simulation platform; a simulator, the simulator being detachably mounted on the simulation platform, the simulator comprising a front cabin assembly, the front cabin assembly comprising a front cabin body and a front cabin platform, the front cabin body being detachably connected to the front cabin platform, and a first mounting slot being provided at a bottom of the front cabin platform; A transport assembly includes a first air floating plate, and the first air floating plate can be installed in the first installation groove to assist in transporting the front cabin platform.

2. The flight simulator according to claim 1, wherein The simulator further includes a rear cabin assembly, the rear cabin assembly being detachably connected to the front cabin assembly, the rear cabin assembly comprising a rear cabin body and a rear cabin platform, the rear cabin body being connected to the front cabin body, the rear cabin body being detachably connected to the rear cabin platform, and a second mounting slot being provided at the bottom of the rear cabin platform; The transport assembly includes a second air floating plate, which can be installed in the second installation groove to assist in transporting the rear cabin platform.

3. The flight simulator according to claim 2, wherein: The simulator also includes: A ball screen, wherein the ball screen cover is arranged on the outer peripheral side of the front cabin assembly; A gantry is provided between the rear cabin assembly and the front cabin assembly, and the gantry is connected to the spherical screen. The gantry includes a conversion door, and the conversion door is detachably provided on the gantry. The conversion door is provided with a matching hole, and the shape of the matching hole is adapted to the cross-sectional shape of the front cabin body.

4. The flight simulator according to claim 2, wherein: The first air flotation plate and the second air flotation plate both include a plate body and an airbag. The airbag is arranged at the bottom of the plate body and is sealed with the plate body. An air inlet and an air outlet are provided on the plate body. The air outlet is arranged at the bottom of the plate body. Both the air inlet and the air outlet are connected to the airbag.

5. The flight simulator according to claim 4, characterized in that The plate body is provided with a plurality of air cavities, the plurality of air bags are connected one by one with the plurality of air cavities, the plurality of air cavities are arranged at intervals on the outer periphery of the air outlet, and each of the air cavities is connected with the air outlet.

6. The flight simulator according to claim 1, wherein: The transport assembly further comprises a lifting platform, which is arranged behind the simulation platform.

7. The flight simulator according to claim 2, wherein: The rear cabin body includes a bulkhead, a door panel and a bottom platform. The door panel is detachably connected to the bulkhead. The bottom platform is arranged at the bottom of the bulkhead, and the rear cabin platform is embedded on the bottom platform.

8. The flight simulator according to claim 2, wherein: Both sides of the front cabin platform and both sides of the rear cabin platform are provided with a plurality of guide wheels arranged at intervals.

9. The flight simulator according to claim 1, wherein: There are a plurality of the first mounting grooves, and a plurality of the first air floating plates. The plurality of the first air floating plates are arranged in a one-to-one correspondence with the plurality of the first mounting grooves.

10. The flight simulator according to claim 2, wherein: There are a plurality of the second mounting grooves, and a plurality of the second air floating plates. The plurality of the second air floating plates are arranged in a one-to-one correspondence with the plurality of the second mounting grooves.

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