CN116092350A - Double-seat teaching flight simulation equipment and flight simulation cabin - Google Patents

Abstract

The invention relates to the technical field of flight simulation, and provides a double-seat teaching flight simulation cabin which comprises a seat assembly, a screen assembly, a foot rudder simulation assembly and an operation simulation assembly, wherein the seat assembly is arranged at one end of simulation equipment, and a computer host and an accelerator simulation assembly are further arranged on the seat assembly; the screen component is fixedly arranged at the other end of the simulation equipment; the foot rudder simulation assembly is fixedly arranged between the seat assembly and the screen assembly; the operation simulation assembly is connected with the screen assembly, and further comprises a chassis frame and a ceiling frame, wherein the chassis frame is arranged at the bottom of the simulation cabin, and the ceiling frame is correspondingly arranged with the chassis frame, so that the gap of the middle-low-end non-professional double-seat teaching flight simulator is filled.

Description

Double-seat teaching flight simulation equipment and flight simulation cabin

Technical Field

The invention relates to the technical field of flight simulation, in particular to a double-seat teaching flight simulation device and a flight simulation cabin.

Background

At present, on the market, the flight simulator is divided into a professional simulator and a non-professional simulator, the professional simulator restores various flight instruments of a real machine by 1:1, then an aircraft windshield is changed into a screen, a linkage hydraulic system is arranged below the simulator, high simulation is realized, the real flight condition can be restored higher, but the manufacturing cost of the professional flight simulator is millions and tens of millions, the professional flight simulator cannot be popularized at all, and some flight simulators are even more expensive than the real machine.

The non-professional flight simulator is crude and low in price, and can realize partial simulation functions, but the non-professional flight simulator is more entertainment-oriented, almost single-seat, and inconvenient for teaching.

The applicant found that the prior art has at least the following technical problems: the non-professional simulator teaching is inconvenient, and the problem that a learner demonstrates and a learner follows simulated flight teaching in real flight teaching cannot be realized.

Disclosure of Invention

The invention aims to provide a double-seat teaching flight simulation device and a flight simulation cabin, which at least solve the problem of inconvenient teaching of a non-professional simulation machine in the prior art. The preferred technical solutions of the technical solutions provided by the present invention can produce a plurality of technical effects described below.

In order to achieve the above purpose, the present invention provides the following technical solutions:

according to some embodiments of the present invention, an aspect provides a two-seat teaching flight simulation device, which is characterized by comprising:

the seat assembly is arranged at one end of the simulation equipment, and a computer host and an accelerator simulation assembly are further arranged on the seat assembly;

the screen component is fixedly arranged at the other end of the simulation equipment; the screen assembly comprises a main screen and a secondary screen which are connected with the computer host;

the foot rudder simulation assembly is fixedly arranged between the seat assembly and the screen assembly;

the operation simulation assembly is connected with the screen assembly, and is arranged between the seat assembly and the screen assembly and corresponds to the foot rudder simulation assembly;

the seat assembly is provided with an operating system control switch and a main power switch, and the operating system control switch is connected with the computer host, the foot rudder simulation assembly, the operation simulation assembly and the throttle simulation assembly.

According to some embodiments of the present invention, a two-seat teaching flight simulation apparatus is provided, the seat assembly including a bottom frame, a seat frame disposed on the bottom frame, a first equipment bay, and a second equipment bay;

the top of the bottom frame is provided with the seat frame, a first equipment cabin and a second equipment cabin;

the bottom of the seat frame is fixedly connected with the bottom frame, a seat is arranged at the top of the seat frame in a sliding manner, the seat frame is connected with the seat in a sliding manner through a seat sliding rail, and the seat can slide along the seat sliding rail towards the screen assembly;

the seat comprises a seat frame, a computer host, a first equipment cabin, a second equipment cabin, a first equipment cabin and a second equipment cabin, wherein one side of the seat frame is provided with the first equipment cabin, the computer host is arranged in the first equipment cabin, and the back and the top of the first equipment cabin are respectively hinged with a cabin door and a cabin cover;

the other side of the seat frame is provided with a second equipment cabin, at least one second equipment cabin is arranged, and the top of the second equipment cabin is provided with a throttle simulation assembly.

According to the double-seat teaching flight simulation device provided by some embodiments of the invention, the accelerator simulation assembly comprises an accelerator lever sliding platform, an accelerator lever and a sliding platform sliding rail, the accelerator lever sliding platform is in sliding connection with the top of the second device cabin through the sliding platform sliding rail, the accelerator lever sliding platform can slide towards the screen assembly, and the accelerator lever is arranged at the top of the accelerator lever sliding platform.

According to some embodiments of the invention, a two-seat teaching flight simulation device is provided, wherein the screen assembly comprises a screen frame skeleton, a screen longitudinal adjustment sliding rail, a screen horizontal adjustment sliding rail, an adjustment sliding sleeve and a stop bolt;

the screen frame framework is longitudinally provided with the screen longitudinal adjusting slide rails, two ends of the screen horizontal adjusting slide rails are respectively arranged on the two screen longitudinal adjusting slide rails in a sliding manner, the axial direction of the screen longitudinal adjusting slide rails is perpendicular to that of the screen horizontal adjusting slide rails, the screen horizontal adjusting slide rails are sleeved with the adjusting slide sleeves, the adjusting slide sleeves are provided with stop bolts, and the stop bolts can fix the positions of the adjusting slide sleeves on the screen horizontal adjusting slide rails;

the main screen and the auxiliary screen are fixedly arranged on the screen assembly in a sliding mode through the adjusting sliding sleeve, and the main screen and the auxiliary screen are connected with the computer host.

According to some embodiments of the invention, a double-seat teaching flight simulation device is provided, wherein the simulation component comprises a foot rudder mounting rod, a foot rudder mounting plate, a foot rudder main body, an angle adjusting support rod and an angle adjusting clamping groove;

the top of foot rudder installation pole pass through the hinge with one of them one end of foot rudder mounting panel articulates, the bottom of foot rudder mounting panel other end is articulated with the one end of angle modulation bracing piece, the other end joint of angle modulation bracing piece is in the cell body of angle modulation draw-in groove, the up end of foot rudder mounting panel is provided with the foot rudder main part.

According to the double-seat teaching flight simulation equipment provided by some embodiments of the invention, the top of the chassis frame is provided with the magnetic attraction piece, two sides of the screen assembly are hinged with the cabin door, one end of the cabin door is hinged with the screen assembly, and the other end of the cabin door is magnetically attracted and connected with the magnetic attraction piece.

According to some embodiments of the present invention, a two-seat teaching flight simulation device is provided, where the operation simulation assembly includes a first telescopic assembly, a second telescopic assembly, and a simulator joystick, one end of the first telescopic assembly is fixedly connected to the screen assembly, a telescopic end of the first telescopic assembly is fixedly connected to the second telescopic assembly, and a telescopic section of the second telescopic assembly is provided with the simulator joystick

According to some embodiments of the present invention, there is provided a two-seat teaching flight simulation pod, including the two-seat teaching flight simulation apparatus, further including:

the chassis frame is arranged at the bottom of the simulation bin;

the ceiling frame is arranged corresponding to the chassis frame;

the top and the bottom of the seat component and the screen component are respectively and fixedly connected with the chassis frame and the ceiling frame.

According to the double-seat teaching flight simulation cabin provided by some embodiments of the invention, the chassis frame and the ceiling frame comprise a framework and end surface skins, the top and the bottom of the chassis frame and the ceiling frame are respectively provided with the end surface skins, and the end surface skins are arranged outside the framework;

according to some embodiments of the invention, the double-seat teaching flight simulation cabin further comprises a supporting framework, wherein the supporting framework is arranged on the back of the seat frame, the bottom of the supporting framework is fixedly connected with the bottom frame, and the top of the seat frame is fixedly connected with the ceiling frame.

One or more technical solutions in the embodiments of the present invention have at least one of the following technical effects:

the seat assembly is used for simulating seats of real flight equipment, wherein a computer host and electronic equipment such as a main screen, a secondary screen and the like in the screen assembly are arranged for simulating real flight instruments, the throttle simulation assembly is used for simulating the throttle of the real flight equipment, and the foot rudder simulation assembly and the operation simulation assembly are arranged for simulating operation devices of the real flight equipment;

the VR equipment is placed in the second equipment cabin, so that the simulation effect of the simulation equipment is further improved, and the simulation environment is more realistic;

the semi-closed flight simulation cabin is formed by arranging the chassis frame, the ceiling frame and the supporting structure in the seat assembly and the screen assembly, the frame structure adopts a fixed connection mode to enable the whole cabin door to have good stability, the left cabin door and the right cabin door only cover the height of the seat, the space above the seat to the ceiling is leaked, the internal condition of the simulation cabin can be observed, and the flight driving environment is simulated.

The simulation design is double-seat, two sets of operating devices are equipped, the two sets of operating devices can independently control the whole simulator in a time-sharing way, and the operating rights are switched through the change-over switch according to actual needs, so that simulation flight teaching can be realized more conveniently, and compared with the existing non-professional simulator, the simulation machine has higher simulation degree because VR glasses are equipped.

Drawings

In order to more clearly illustrate the embodiments of the invention or the technical solutions in the prior art, the drawings that are required in the embodiments or the description of the prior art will be briefly described, it being obvious that the drawings in the following description are only some embodiments of the invention, and that other drawings may be obtained according to these drawings without inventive effort for a person skilled in the art.

FIG. 1 is a schematic view of the overall structure of the present invention;

FIG. 2 is a schematic top view of the bottom frame of the present invention;

FIG. 3 is a schematic view of the bottom frame structure of the present invention;

FIG. 4 is a schematic view of the ceiling frame construction of the present invention;

FIG. 5 is a schematic elevational view of the seat assembly of the present invention;

FIG. 6 is an enlarged schematic view at A in FIG. 5;

FIG. 7 is a schematic rear view of the seat assembly of the present invention;

FIG. 8 is a schematic view of a screen assembly of the present invention;

FIG. 9 is an enlarged schematic view at B in FIG. 8;

FIG. 10 is a schematic diagram of a foot rudder analog assembly of the present invention;

FIG. 11 is a schematic diagram of the operational simulation assembly of the present invention;

fig. 12 is a schematic view of the control switch connection structure of the manipulation system of the present invention.

In the figure: 100-chassis frame, 101-first rail, 102-second rail, 103-third rail, 104-fourth rail, 105-fifth rail, 106-first rail, 107-second rail, 108-connecting rod, 109-track slot, 200-ceiling frame, 201-sixth rail, 202-seventh rail, 203-eighth rail, 204-ninth rail, 205-third rail, 206-fourth rail, 207-seventh connecting rod, 208-eighth connecting rod, 300-seat assembly, 301-bottom frame, 302-seat frame, 304-first equipment bay, 305-second equipment bay, 306-seat, 307-seat track, 308-operating system control switch, 309-main power switch, 400-screen assembly, 401-screen frame skeleton, 402-screen longitudinal adjustment slide rail, 403-screen horizontal adjustment slide rail, 404-adjustment slide sleeve, 405-stop bolt, 406-cabin door, 407-main screen, 408-main screen, 500-computer host, 600-foot rudder analog component, 601-foot rudder mounting bar, 602-foot rudder mounting plate, 603-foot rudder body, 604-angle adjustment support bar, 605-angle adjustment clamping groove, 606-magnetic attraction piece, 700-operation analog component, 701-first telescopic sleeve, 702-first telescopic rod, 703-second telescopic sleeve, 704-second telescopic rod, 705-analog machine operating rod, 800-throttle analog component, 801-throttle lever sliding platform, 802-throttle lever, 803-sliding platform sled, 805-second equipment bay.

Detailed Description

In order to make the objects, technical solutions and advantages of the present invention more apparent, the technical solutions of the present invention will be described in detail below. It will be apparent that the described embodiments are only some, but not all, embodiments of the invention. All other embodiments, based on the examples herein, which are within the scope of the invention as defined by the claims, will be within the scope of the invention as defined by the claims.

As shown in fig. 1-11, in particular, according to some embodiments of the present invention, an aspect provides a two-seat teaching flight simulation apparatus, which is characterized by comprising:

the seat assembly 300 is arranged at one end of the simulation equipment, and a computer host 500 and a throttle simulation assembly 800 are further arranged on the seat assembly 300;

as shown in fig. 4-6, in an implementation, the seat assembly 300 includes a base infrastructure and seats, etc., for simulating the cabin environment of an actual flying device;

wherein the seat assembly 300 comprises a bottom frame 301, a seat frame 302 disposed on the bottom frame 301, a first equipment compartment 304, and a second equipment compartment 305; the bottom frame 301 is a frame structure based on which a seat frame 302 is provided at the top, preferably two seats 306 are provided on the seat frame 302 for satisfying the configuration of the double operating environment of the cabin.

The top of the bottom frame 301 is provided with the seat frame 302, a first equipment bay 304, and a second equipment bay 305; the top of the seat frame 302 is provided with a bearing platform, the upper end surface of the bearing platform is provided with a sliding rail, and the seat 306 at the top of the seat frame 302 can slide back and forth;

specifically, the bottom of the seat frame 302 is fixedly connected with the bottom frame 301, the top of the seat frame 302 is slidably provided with a seat 306, the seat frame 302 is slidably connected with the seat 306 through a seat slide rail 307, the seat slide rail 307 extends to the front end and the rear end of the seat 306, the seat 306 can slide along the seat slide rail 307 towards the screen assembly 400, wherein the backrest of the seat 306 is adjustable, and the inclination angle of the backrest can be adjusted according to actual use requirements;

the bottom of the seat frame 302 forms an independent space, one side of the seat frame 302 is provided with the first equipment compartment 304, the first equipment compartment 304 is arranged between two seats 306, as shown in fig. 7, the computer host 500 is arranged in the first equipment compartment 304, as shown in fig. 5-7, the back and the top of the first equipment compartment 304 are respectively hinged with a cabin door and a cabin cover, and the cabin door and the cabin cover can be opened and closed in a rotating manner;

a second equipment cabin 305 is arranged on the other side of the seat frame 302, at least one second equipment cabin 305 is arranged, and a throttle simulation assembly 800 is arranged on the top of the second equipment cabin 305;

preferably, as shown in fig. 5, two second equipment cabins 305 are provided and are located at two sides of two seats 306, the VR equipment is placed in the second equipment cabins 305, the reality of the simulation equipment is further improved through the VR equipment, concave grooves are formed in the tops of the second equipment cabins 305, and sliding rails are arranged at the tops of the grooves, so that the accelerator simulation assembly 800 can slide on the tops of the second equipment cabins 305.

As shown in fig. 5-6, in a specific implementation, the throttle simulation assembly 800 includes a throttle lever sliding platform 801, a throttle lever 802, and a sliding platform sliding rail 803, where the opening direction of the sliding platform sliding rail 803 is the same as that of the seat sliding rail 307, so that the throttle lever sliding platform 801 can slide back and forth, the throttle lever sliding platform 801 is slidably connected with the top of the second equipment compartment 305 through the sliding platform sliding rail 803, the throttle lever sliding platform 801 can slide toward the screen assembly 400, and the top of the throttle lever sliding platform 801 is provided with the throttle lever 802, so that a user can slide the throttle lever sliding platform 801 back and forth toward the screen assembly 400 through pushing and pulling the throttle lever 802, thereby achieving the effect of simulating the throttle in the real flight equipment.

The screen assembly 400 is fixedly arranged at the other end of the simulation device; the screen assembly includes a main screen 407 and a sub-screen 408 connected to the computer host 500;

as shown in fig. 8-11, the screen assembly 400 is used in combination with other assemblies, wherein the main screen 407 is provided with two, at least one sub-screen 408 is provided, and the screen can display the instrument of the computer software simulation place on the screen when being connected with the computer host 500.

As shown in fig. 1-3 and 10, a foot rudder simulation assembly 600 is fixedly disposed between the seat assembly 300 and the screen assembly 400;

according to some embodiments of the present invention, a double-seat teaching flight simulation device is provided, where the simulation assembly 600 includes a foot rudder mounting bar 601, a foot rudder mounting plate 602, a foot rudder body 603, an angle adjustment support bar 604, and an angle adjustment clamping groove 605;

the top of the foot rudder mounting rod 601 is hinged with one end of the foot rudder mounting plate 602 through a hinge, the bottom of the other end of the foot rudder mounting plate 602 is hinged with one end of an angle adjusting support rod 604, the other end of the angle adjusting support rod 604 is clamped in a groove body of the angle adjusting clamping groove 605, and the upper end face of the foot rudder mounting plate 602 is provided with the foot rudder main body 603;

as shown in fig. 10, in the implementation, the angle adjusting support bar 604 may be rotated, and the position of the angle adjusting support bar 604 in the groove body of the angle adjusting slot 605 may be adjusted according to the actual use situation, so as to control the inclination angle of the rudder mounting plate 602, and the user steps on the rudder body 603 when using, so that the simulation device is more realistic by means of the angle adjusting manner.

As shown in fig. 11, in the implementation, an operation simulation module 700 is connected to the screen module 400, the operation simulation module 700 is disposed between the seat module 300 and the screen module 400, and the operation simulation module 700 is disposed corresponding to the rudder simulation module 600.

In a specific implementation, the operation simulation assembly 700 includes a first telescopic assembly, a second telescopic assembly and a simulator joystick 705, one end of the first telescopic assembly is fixedly connected to the screen assembly 400, the telescopic end of the first telescopic assembly is fixedly connected to the second telescopic assembly, and a telescopic section of the second telescopic assembly is provided with the simulator joystick 705.

Specifically, the first telescopic assembly is arranged in a downward inclined manner, the second telescopic assembly is arranged vertically, the first telescopic assembly of the operation simulation assembly 700 comprises a first telescopic sleeve 701 and a first telescopic rod 702, and the second telescopic assembly comprises a second telescopic sleeve 703 and a second telescopic rod 704

As shown in fig. 11, one end of the first telescopic sleeve 701 is fixedly connected with the screen assembly 400, the other end of the first telescopic sleeve 701 extends toward the seat assembly 300, a first telescopic rod 702 is disposed inside the first telescopic sleeve 701, the first telescopic sleeve 701 and the first telescopic rod 702 are coaxially disposed, one end of the first telescopic rod 702 extending out of the first telescopic sleeve 701 is fixedly provided with the second telescopic sleeve 703, the axis of the second telescopic sleeve 703 is perpendicular to the end surface of the chassis frame 100, a fourth telescopic rod 704 is disposed inside the second telescopic sleeve 703, and one end of the second telescopic rod 704 extending out of the second telescopic sleeve 703 is fixedly provided with the simulator operating rod 705;

when the position of the analog machine operation lever 705 needs to be adjusted back and forth, the back and forth position adjustment of the analog machine operation lever 705 is realized by the expansion and contraction of the first telescopic rod 702 in the first telescopic sleeve 701, when the position of the analog machine operation lever 705 needs to be adjusted longitudinally, the adjustment is realized by the longitudinal sliding of the second telescopic rod 704 in the second telescopic sleeve 703,

the first telescopic sleeve 701 and the second telescopic sleeve 703 are provided with stop bolts for fixing the first telescopic rod 702 and the second telescopic rod 704. In the concrete implementation, the part screwed into the sleeve is pressed to form the fixing and anti-loosening functions of the telescopic rod by rotating the stop bolt.

As shown in fig. 8-9, the screen assembly 400 includes a screen frame backbone 401, a screen longitudinal adjustment slide rail 402, a screen horizontal adjustment slide rail 403, an adjustment slide sleeve 404, and a stop bolt 405;

the screen frame framework 401 is a support frame with an integral structure, the screen frame framework 401 is longitudinally provided with the screen longitudinal adjusting slide rails 402, and at least two screen longitudinal adjusting slide rails 402 are symmetrically arranged; the two ends of the screen horizontal adjusting slide rail 403 are respectively and slidably arranged on the two screen longitudinal adjusting slide rails 402, so that the screen horizontal adjusting slide rail 403 can longitudinally slide along the screen longitudinal adjusting slide rail 402, the axial direction of the screen longitudinal adjusting slide rail 402 is perpendicular to the axial direction of the screen horizontal adjusting slide rail 403, the screen horizontal adjusting slide rail 403 is sleeved with the adjusting slide sleeve 404, the adjusting slide sleeve 404 is provided with a stop bolt 405, and the stop bolt 405 can fix the position of the adjusting slide sleeve 404 on the screen horizontal adjusting slide rail 403;

specifically, when the screen position needs to be adjusted, the position in the horizontal direction is adjusted by horizontally sliding the adjusting slide rail 404 along the screen horizontal adjusting slide rail 403, the longitudinal position is adjusted by longitudinally sliding the screen horizontal adjusting slide rail 403 on the screen longitudinal adjusting slide rail 402, and when the position is appropriate, the position of the screen is further fixed by fixing the adjusting slide rail 404 through rotation of the stop bolt 405, preferably, the main screen 407 and the auxiliary screen 408 are both provided with adjusting components capable of slidably adjusting the position.

The main screen 407 and the auxiliary screen 408 are slidably and fixedly arranged on the screen assembly 400 through the adjusting sliding sleeve 404, and the main screen 407 and the auxiliary screen 408 are connected with the computer host 500, so that instruments and other pictures simulated by computer software are displayed on the screen.

The seat assembly 300 is provided with an operating system control switch 308 and a main power switch 309, the operating system control switch 308 is connected with the computer host 500, the foot rudder analog assembly 600, the operation analog assembly 700 and the throttle analog assembly 800, the main power switch 309 is a power control switch of the whole system, as shown in fig. 1-5 and fig. 12, the foot rudder analog assembly 600, the operation analog assembly 700 and the throttle analog assembly 800 are provided with two sets, the two sets of foot rudder analog assembly 600, the operation analog assembly 700 and the throttle analog assembly 800 are connected with the same computer host 500 through a hub and other assemblies, and two operating system control switches 308 are provided, and the two sets of operating systems respectively comprise a left foot rudder, a left seat throttle lever, a right seat rudder, a right seat throttle lever and a right seat throttle lever; as shown in fig. 5 and 12, two control switches 308 of the control system are provided, namely a left control switch of the control system and a right control switch of the control system, the left control switch of the control system can control a left foot rudder, a left seat throttle lever and a left seat control lever, the right control switch of the control system can control a right foot rudder, a right seat throttle lever and a right seat control lever, and the two control switches of the control system respectively control simulation equipment on the left side and the right side, so that the whole simulation machine can be independently controlled in a time-sharing manner, and the control right is switched by switching the switch according to actual needs, therefore, the simulation flight teaching can be conveniently realized, the equipment can realize the demonstration of a learner, and the trainee follows the simulated flight teaching effect. 1-11, according to some embodiments of the present invention, there is provided a two-seat teaching flight simulation pod, including the two-seat teaching simulation apparatus, further including:

a chassis frame 100 disposed at the bottom of the simulation bin;

a ceiling frame 200 provided corresponding to the chassis frame 100;

the top and bottom of the seat assembly 300 and the screen assembly 400 are fixedly connected to the chassis frame 100 and the ceiling frame 200, respectively.

Preferably, as shown in fig. 1-3, the chassis frame 100 and the ceiling frame 200 each include a skeleton and an end surface skin, the top and the bottom of the chassis frame 100 and the ceiling frame 200 are provided with the end surface skin, the end surface skin is disposed outside the skeleton, the bottom of the chassis frame 100 is provided with universal wheels, and a part of the universal wheels are provided with a brake device;

the backbone of the chassis frame 100 includes a first cross bar 101, a second cross bar 102, a third cross bar 103, a fourth cross bar 104, a fifth cross bar 105, a first side rail 106, a second side rail 107, and a connecting bar 108;

the axes of the first cross bar 101, the second cross bar 102, the third cross bar 103, the fourth cross bar 104 and the fifth cross bar 105 are parallel to each other, and the axes of the first longitudinal bar 106 and the second longitudinal bar 107 are parallel to each other;

the first cross rod 101 and the second cross rod 102 are arranged at intervals and in parallel, one end of the first connecting rod 101 is fixedly connected with one end of the connecting rod 108, the other end of the connecting rod 108 is fixedly connected with one end of the second longitudinal rod 107, the other end of the second longitudinal rod 107 is fixedly connected with one end of the second cross rod 102, and the structures of the two ends of the first cross rod 101 and the second cross rod 102 are identical;

two first longitudinal bars 106 are arranged in parallel between the first transverse bar 101 and the second transverse bar 102, the axis of each first longitudinal bar 106 is perpendicular to the first transverse bar 101, one end of each first longitudinal bar 106 is fixedly connected with the side wall of the first transverse bar 101, the other end of each first longitudinal bar 106 is fixedly connected with the side wall of the second transverse bar 102, and a circuit groove 109 is formed between the two first longitudinal bars 106 which are arranged in parallel;

the fourth cross bar 104 is disposed between the first cross bar 101 and the second cross bar 102, and two ends of the fourth cross bar 104 are fixedly connected with two second longitudinal bars 107 respectively;

the third vertical rod 103 is disposed between the first horizontal rod 101 and the fourth horizontal rod 104, one end of the third horizontal rod 103 is fixedly connected with the connecting rod 108, and the other end of the third horizontal rod 103 is fixedly connected with the first vertical rod 106;

the fifth cross bar 105 is disposed between the second cross bar 102 and the fourth cross bar 104, one end of the fifth cross bar 105 is fixedly connected with the first vertical bar 106, and the other end of the fifth cross bar 105 is fixedly connected with the second vertical bar 107.

As shown in fig. 4, the canopy frame 200 includes a sixth cross bar 201, a seventh cross bar 202, an eighth cross bar 203, a ninth cross bar 204, a third vertical bar 205, a fourth vertical bar 206, a seventh connecting bar 207, and an eighth connecting bar 208, where the canopy frame 200 is disposed in axisymmetry with the axis of the third vertical bar 205 as a symmetry axis, the axes of the sixth cross bar 201, the seventh cross bar 202, the eighth cross bar 203, and the ninth cross bar 204 are parallel to each other, and the axes of the third vertical bar 205 and the fourth vertical bar 206 are parallel to each other;

the sixth cross bar 201 is spaced from and parallel to the seventh cross bar 202, one end of the sixth connecting bar 201 is fixedly connected with one end of the seventh connecting bar 207, the other end of the seventh connecting bar 207 is fixedly connected with one end of the fourth vertical bar 206, the other end of the fourth vertical bar 206 is fixedly connected with one end of the eighth connecting bar 208, the other end of the eighth connecting bar 208 is fixedly connected with one end of the seventh cross bar 202, and the structures of both ends of the sixth cross bar 201 and the seventh cross bar 202 are the same;

the eighth cross bar 203 is disposed between the sixth cross bar 201 and the seventh cross bar 202, one end of the eighth cross bar 203 is fixedly connected with the third vertical bar 205, and the other end of the eighth cross bar 203 is fixedly disposed at the connection position of the seventh connecting bar 207 and the fourth vertical bar 206;

the ninth cross bar 204 is disposed between the seventh cross bar 202 and the ninth cross bar 204, one end of the ninth cross bar 204 is fixedly connected with the third vertical bar 205, and the other end of the ninth cross bar 204 is fixedly connected with the fourth vertical bar 206.

According to some embodiments of the present invention, a two-seat teaching flight simulation cabin further includes a support frame 303, the support frame 303 is disposed on the back of the seat frame 302, the bottom of the support frame 303 is fixedly connected with the bottom frame 301, the top of the seat frame 302 is fixedly connected with the ceiling frame 200, and a support is formed between the chassis frame 100 and the ceiling frame 200 through the support frame 303 and the screen frame 401.

Specifically, the foot rudder installation bar 601 is fixedly connected with the upper end surface of the chassis frame 100, the foot rudder simulation assembly 600 is arranged right above the fourth cross bar 104, the axis of the foot rudder simulation assembly 600 is parallel to the axis of the fourth cross bar 104, the angle adjustment clamping groove 605 is fixedly arranged on the chassis frame 100, a plurality of groove bodies are arranged on the angle adjustment clamping groove 605 along the axis direction, the top of the chassis frame 100 is provided with a magnetic attraction piece 606, two sides of the screen assembly 400 are hinged with cabin doors 406, one end of the cabin doors 406 is hinged with the screen assembly 400, the other end of the cabin doors 406 is magnetically attracted with the magnetic attraction piece 606, and preferably, the two ends of the foot rudder installation bar 601 are provided with the magnetic attraction piece 606, so that the cabin doors 406 on two sides can be closed by a magnetic attraction mode.

By providing the seat assembly 300 for simulating the seat of the real flying device, wherein the computer host 500 and the electronic devices such as the main screen 407 and the auxiliary screen 408 in the screen assembly 400 are provided for simulating the flying instrument of the real, the throttle simulation assembly 800 is provided for simulating the throttle of the flying device of the real, and by providing the foot rudder simulation assembly 600 and the operation simulation assembly 700 for simulating the operation device of the flying device of the real;

VR equipment is placed in the second equipment cabin 805, so that the simulation effect of the simulation equipment is further improved, and the simulation environment is more realistic;

the semi-closed flight simulation cabin is formed by arranging the chassis frame 100, the ceiling frame 200 and the supporting structures in the seat assembly 300 and the screen assembly 400, the frame structure adopts a fixed connection mode to enable the whole to have good stability, the left cabin door and the right cabin door only cover the height of the seat, the space above the seat to the ceiling is leaked, the condition inside the simulation cabin can be observed, and the flight driving environment is simulated.

Preferably, as shown in fig. 1-11, the simulation design is double-seat, two sets of operating devices are provided, and the two sets of operating devices can respectively and independently operate the whole simulation machine, so that simulation flight teaching can be realized.

The data parameters of the instrument are called out through software to replace the traditional instrument: altimeter, airspeed meter, throttle revolution meter, lifting speed meter, fuel meter, heading meter and other meters. Or through VR devices into the aircraft cabin simulating flight, using the instrument systems of the aircraft within the aircraft software. These parameter data can be called directly through the setting interface of the existing software. The manufacturing cost is greatly saved. Meanwhile, the VR technology is applied, and the airplane cockpit manufactured directly through software programming is displayed in real and immersive mode by various flight instruments. The effect of the professional high-end flight simulator can be achieved through lower production cost, and the popularization of the flight simulator is possible.

In the description of the present invention, it is to be noted that, unless otherwise indicated, the meaning of "plurality" means two or more; the terms "upper", "lower", "left", "right", "inner", "outer", "front", "rear", "head", "tail", etc., refer to an orientation or positional relationship based on that shown in the drawings, and are merely for convenience in describing the present invention and simplifying the description, and do not indicate or imply that the apparatus or elements referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore should not be construed as limiting the present invention. Furthermore, the terms "first," "second," "third," and the like are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.

In the description of the present invention, it should also be noted that, unless explicitly specified and limited otherwise, the terms "mounted", "connected" and "connected" are to be construed broadly, and may be, for example, fixedly connected, detachably connected or integrally connected; can be mechanically or electrically connected; can be directly connected or indirectly connected through an intermediate medium. The specific meaning of the above terms in the present invention can be understood as appropriate by those of ordinary skill in the art.

The foregoing is merely illustrative of the present invention, and the present invention is not limited thereto, and any person skilled in the art will readily recognize that variations or substitutions are within the scope of the present invention. Therefore, the protection scope of the invention is subject to the protection scope of the claims.

Claims (10)

1. A two-seater teaching flight simulation device, comprising:

the seat assembly (300) is arranged at one end of the simulation equipment, and a computer host (500) and a throttle simulation assembly (800) are further arranged on the seat assembly (300);

the screen assembly (400) is fixedly arranged at the other end of the simulation equipment; the screen assembly comprises a main screen (407) and a secondary screen (408) which are connected with the computer host (500);

the foot rudder simulation assembly (600) is fixedly arranged between the seat assembly (300) and the screen assembly (400);

the operation simulation assembly (700) is connected with the screen assembly (400), the operation simulation assembly (700) is arranged between the seat assembly (300) and the screen assembly (400), and the operation simulation assembly (700) is arranged corresponding to the rudder simulation assembly (600);

the seat assembly (300) is provided with an operating system control switch (308) and a main power switch (309), and the operating system control switch (308) is connected with the computer host (500), the foot rudder simulation assembly (600), the operation simulation assembly (700) and the throttle simulation assembly (800).

2. The two-seat teaching flight simulation apparatus of claim 1 wherein the seat assembly (300) comprises a bottom frame (301) and a seat frame (302), a first equipment pod (304) and a second equipment pod (305) disposed on the bottom frame (301);

the top of the bottom frame (301) is provided with the seat frame (302), a first equipment compartment (304) and a second equipment compartment (305);

the bottom of the seat frame (302) is fixedly connected with the bottom frame (301), a seat (306) is slidably arranged at the top of the seat frame (302), the seat frame (302) is slidably connected with the seat (306) through a seat slide rail (307), and the seat (306) can slide along the seat slide rail (307) towards the screen assembly (400);

one side of the seat frame (302) is provided with the first equipment cabin (304), the computer host (500) is arranged in the first equipment cabin (304), and the back and the top of the first equipment cabin (304) are respectively hinged with a cabin door and a cabin cover;

the other side of the seat frame (302) is provided with a second equipment cabin (305), the second equipment cabin (305) is at least provided with one, and the top of the second equipment cabin (305) is provided with a throttle simulation assembly (800).

3. The double-seat teaching flight simulation device according to claim 2, wherein the accelerator simulation assembly (800) comprises an accelerator lever sliding platform (801), an accelerator lever (802) and a sliding platform sliding rail (803), the accelerator lever sliding platform (801) is slidably connected with the top of the second device cabin (305) through the sliding platform sliding rail (803), the accelerator lever sliding platform (801) can slide towards the screen assembly (400), and the accelerator lever (802) is arranged on the top of the accelerator lever sliding platform (801).

4. A two-seat teaching flight simulation apparatus according to claim 3, characterized in that the screen assembly (400) comprises a screen frame skeleton (401), a screen longitudinal adjustment slide rail (402), a screen horizontal adjustment slide rail (403), an adjustment slide sleeve (404) and a stop bolt (405);

the screen frame framework (401) is longitudinally provided with the screen longitudinal adjustment slide rails (402), two ends of the screen horizontal adjustment slide rails (403) are respectively arranged on the two screen longitudinal adjustment slide rails (402) in a sliding mode, the axial direction of the screen longitudinal adjustment slide rails (402) is perpendicular to the axial direction of the screen horizontal adjustment slide rails (403), the screen horizontal adjustment slide rails (403) are sleeved with the adjustment slide sleeves (404), the adjustment slide sleeves (404) are provided with stop bolts (405), and the stop bolts (405) can fix the positions of the adjustment slide sleeves (404) on the screen horizontal adjustment slide rails (403);

the main screen (407) and the auxiliary screen (408) are fixedly arranged on the screen assembly (400) in a sliding mode through the adjusting sliding sleeve (404), and the main screen (407) and the auxiliary screen (408) are connected with the computer host (500).

5. The double-seat teaching flight simulation device according to claim 4, wherein the simulation assembly (600) comprises a foot rudder mounting rod (601), a foot rudder mounting plate (602), a foot rudder main body (603), an angle adjusting support rod (604) and an angle adjusting clamping groove (605);

the top of foot rudder installation pole (601) pass through the hinge with one of them one end of foot rudder mounting panel (602) articulates, the bottom of foot rudder mounting panel (602) other end is articulated with one end of angle modulation bracing piece (604), the other end joint of angle modulation bracing piece (604) is in the cell body of angle modulation draw-in groove (605), the up end of foot rudder mounting panel (602) is provided with foot rudder main part (603).

6. The double-seat teaching flight simulation device according to claim 5, wherein a magnetic attraction piece (606) is arranged at the top of the chassis frame (100), two sides of the screen assembly (400) are hinged with cabin doors (406), one end of each cabin door (406) is hinged with the screen assembly (400), and the other end of each cabin door (406) is in magnetic attraction connection with the corresponding magnetic attraction piece (606).

7. The two-seater teaching flight simulation device of claim 6, wherein the operation simulation assembly (700) comprises a first telescopic assembly, a second telescopic assembly and a simulation machine control lever (705), one end of the first telescopic assembly is fixedly connected with the screen assembly (400), the telescopic end of the first telescopic assembly is fixedly connected with the second telescopic assembly, and a telescopic section of the second telescopic assembly is provided with the simulation machine control lever (705).

8. A two-seater teaching flight simulation pod comprising the two-seater teaching flight simulation apparatus of claims 1-7, further comprising:

a chassis frame (100) disposed at the bottom of the simulation bin;

a ceiling frame (200) provided in correspondence with the chassis frame (100);

the top and bottom of the seat assembly (300) and the screen assembly (400) are fixedly connected with the chassis frame (100) and the ceiling frame (200), respectively.

9. The two-seater teaching flight simulation pod of claim 8, wherein the chassis frame (100) and the ceiling frame (200) each comprise a skeleton and an end skin, the top and bottom of the chassis frame (100) and the ceiling frame (200) each are provided with an end skin, and the end skins are disposed outside the skeleton.

10. The two-seater teaching flight simulation cabin according to claim 9, further comprising a supporting framework (303), wherein the supporting framework (303) is arranged on the back of the seat frame (302), the bottom of the supporting framework (303) is fixedly connected with the bottom frame (301), and the top of the seat frame (302) is fixedly connected with the ceiling frame (200).

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