CN115225868B - Image communication equipment suitable for flight training simulation storehouse - Google Patents
Image communication equipment suitable for flight training simulation storehouse Download PDFInfo
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- CN115225868B CN115225868B CN202211140293.4A CN202211140293A CN115225868B CN 115225868 B CN115225868 B CN 115225868B CN 202211140293 A CN202211140293 A CN 202211140293A CN 115225868 B CN115225868 B CN 115225868B
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- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04N—PICTORIAL COMMUNICATION, e.g. TELEVISION
- H04N7/00—Television systems
- H04N7/18—Closed-circuit television [CCTV] systems, i.e. systems in which the video signal is not broadcast
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- G—PHYSICS
- G09—EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
- G09B—EDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
- G09B9/00—Simulators for teaching or training purposes
- G09B9/02—Simulators for teaching or training purposes for teaching control of vehicles or other craft
- G09B9/08—Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of aircraft, e.g. Link trainer
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- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04N—PICTORIAL COMMUNICATION, e.g. TELEVISION
- H04N9/00—Details of colour television systems
- H04N9/12—Picture reproducers
- H04N9/31—Projection devices for colour picture display, e.g. using electronic spatial light modulators [ESLM]
- H04N9/3141—Constructional details thereof
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Abstract
The application discloses image communication equipment suitable for a flight training simulation cabin, which relates to the technical field of image communication equipment and is arranged inside a cabin shell of the flight training simulation cabin, wherein a display screen, a training computer and a central console are arranged in the flight training simulation cabin, and an external control screen is arranged outside the flight training simulation cabin; a monitoring component and a projection component are fixed on the inner wall of the top of the bin body shell; the monitoring component is in signal connection with the external control screen, and images shot by the monitoring component can be displayed on the external control screen for a training teacher to watch; the projection component is used for projecting the recorded or synthesized image to the upper surface of the center console; the center console is sprayed with projection paint or positioned with a projection curtain; the external control screen is in signal connection with the training computer; the technical effect that the image communication equipment suitable for the flight training simulation cabin can assist the simulation training cabin to simulate the center console of airplanes of various types at low cost so as to meet training requirements is achieved.
Description
Technical Field
The invention relates to the technical field of image communication equipment, in particular to image communication equipment suitable for a flight training simulation cabin.
Background
The flight training simulation cabin is equipment for training pilots, and generally consists of a vision system and a training computer; the computer is a control center of the flight training simulation cabin; when trainees sit in the flight training simulation cabin, the trainees can perform operations such as opening a switch, pushing and pulling an accelerator, operating a flight lever and a rudder and the like, and can obtain data such as flight speed, travel, position, height, wind direction, wind speed and the like; the vision system can provide the scene simulation of the student, and the student feels the motions of diving, pitching and circling when in operation like sitting in an airplane; therefore, as long as the simulation conditions are vivid, the trainees trained through flight simulation can fly the airplane to fly off for exercise immediately after graduation. However, the traditional flight training simulation cabin still has some problems in the actual use process; when the traditional flight training simulation cabin is used, if a pilot acts wrongly or not in place during training, the pilot cannot easily see the place of the mistake unless the pilot points, so that the training efficiency is generally low, a large amount of time is usually spent on training, and time and labor are wasted.
In order to solve the above problems, chinese patent No. CN107396058B discloses a flight simulation training monitoring device dedicated for aerospace, which monitors and records the actions of trainees by arranging a camera inside a training cabin, and assists to find trainee errors, thereby shortening training time.
However, aircraft models are continuously updated along with the progress of technology, and the layout difference of a center console among the models is large; if the training cabin is matched with each airplane model, the cost is too high; however, if the simulated training cabin is not updated with the updating of the airplane, the training requirement is difficult to meet.
Disclosure of Invention
The embodiment of the application solves the technical problem that the flight training simulation bin in the prior art is high in updating cost for adapting to airplane model updating, and achieves the technical effect that the image communication equipment suitable for the flight training simulation bin can assist in simulating the central console of airplanes of various models with low cost in the training bin to further meet training requirements.
The embodiment of the application provides image communication equipment suitable for a flight training simulation cabin, which is arranged in a cabin shell of the flight training simulation cabin, wherein a display screen, a training computer and a central console are arranged in the flight training simulation cabin, and an external control screen is arranged outside the flight training simulation cabin;
a monitoring component and a projection component are fixed on the inner wall of the top of the bin body shell;
the monitoring component is a ball head camera and is in signal connection with the external control screen, and images shot by the monitoring component can be displayed on the external control screen for a training teacher to watch;
the projection assembly is used for projecting the recorded or synthesized image to the upper surface of the center console and displaying the structure of each part on the center console and the state of each indicator light;
the center console is sprayed with projection paint or positioned with a projection curtain;
the projection component is in signal connection with the training computer;
the external control screen is in signal connection with the training computer, in the operation process of a student, a teacher can correct and prompt in real time, and a training teacher can modify images projected by the projection assembly in real time or give prompts by controlling the external control screen according to requirements.
Preferably, the center console comprises a center console frame, a module accommodating bin, a closed diaphragm, a pumping assembly, a diaphragm limiting assembly and a learning module body;
the center console frame is of a frame structure or a box structure;
the module accommodating bin is of a box body structure with an opening at the top and is fixed on the central console frame, and the bottom of the module accommodating bin is a bin body bottom plate;
the closed diaphragm is a soft film and is fixed on the inner wall of the module accommodating bin to close the module accommodating bin to form a closed space;
the gas pumping assembly is controlled by a training computer and plays a role in adjusting the gas amount in the closed space;
the diaphragm limiting component is used for fixing the closed diaphragm on the bin body bottom plate according to requirements so as to limit the expansion shape of the closed diaphragm and further facilitate the installation and fixation of the learning module body;
the diaphragm limiting assembly is structurally a magnet group or a buckle;
the whole learning module body is in a block shape and has various specifications, and different control component models are arranged on the learning module bodies with different specifications;
the upper surface of the learning module body is sprayed with projection paint or provided with a projection curtain;
the learning module body is fixed on the closed diaphragm through a magnet or a buckle and is indirectly fixed on the diaphragm limiting component.
Furthermore, the number of the diaphragm limiting assemblies is multiple, the diaphragm limiting assemblies are densely distributed on the closed diaphragm, and the diaphragm limiting assemblies comprise connecting plates, fixing columns, fixing pipes, sliding limiting blocks, force storage pressure springs and releasing assemblies;
the connecting plate is plate-shaped, is integrally provided with a magnet or is provided with a magnet in a positioning mode, is fixed on the closed diaphragm and plays a role in connecting the closed diaphragm and the fixing column and a role in adsorbing and fixing the learning module body;
a bottom magnet is positioned at the bottom of the learning module body;
the fixing column is fixed on the connecting plate, and an annular positioning groove is formed in the side wall of the fixing column;
the fixing column can be inserted into the fixing tube;
the fixed pipes are fixed on the bin body bottom plate and correspond to the fixed columns one by one, and holes for accommodating the sliding limiting blocks are formed in the inner walls of the fixed pipes;
the sliding limiting block is a wedge-shaped block body and is positioned on the inner wall of the fixed pipe in a sliding mode; the power storage pressure spring is positioned in the hole on the inner wall of the fixed pipe and is abutted against the sliding limiting block;
after the fixed column is inserted into the fixed tube, the sliding limiting block is inserted into the positioning groove under the action of the elasticity of the force storage pressure spring to limit the axial movement of the fixed column;
the release assembly is used for driving the sliding limiting block to be separated from the positioning groove.
Further, the release assembly comprises a pulling rope and a rope body pulling assembly;
one end of the pulling rope is positioned on the sliding limiting block, and the other end of the pulling rope is fixed on the rope body pulling assembly;
the rope body dragging assembly is of a reel structure, and is rotated manually or electrically, and the rope is dragged to shift during rotation.
Preferably, the closed membrane is a double-layer membrane and comprises a first membrane and a second membrane, and the first membrane and the second membrane are fixed on the side wall of the module accommodating bin;
a space formed by the first diaphragm and the module accommodating bin is a gas storage space filled with gas;
the second membrane is located above the first membrane, and the second membrane, together with the first membrane and the module accommodating bin, form a liquid storage space for storing liquid.
Preferably, the closed membrane is a three-layer membrane, which comprises a first membrane, a second membrane and a third membrane, all of which are fixed on the side wall of the module accommodating bin;
the space formed by the first diaphragm and the module accommodating bin is a gas storage space which is filled with gas; the second diaphragm is positioned above the first diaphragm, and the second diaphragm, the first diaphragm and the module accommodating bin form a liquid storage space for storing liquid together;
the third diaphragm is positioned above the second diaphragm, the third diaphragm, the second diaphragm and the module accommodating bin form a powder storage space for storing iron powder together, and the powder storage space is filled with the iron powder;
the side wall of the learning module body is provided with a side wall magnet.
Preferably, the closed diaphragm is a double-layer film, and forms a gas storage space and a powder storage space together with the module accommodating bin;
a side wall magnet is positioned on the side wall of the learning module body; and iron powder is filled in the powder storage space.
Preferably, a bottom plate magnet group is positioned on the bin body bottom plate, and the bottom plate magnet group is matched with iron powder filled in the powder storage space to enable the closed diaphragm to tend to be smooth.
Preferably, the powder storage space is divided into a plurality of powder storage units by welding or sewing.
Further, the control component model is a handle model, a joystick model and/or a key model.
One or more technical solutions provided in the embodiments of the present application have at least the following technical effects or advantages:
the monitoring equipment of a flight training simulation cabin in the prior art is optimized, a projection assembly is additionally arranged on the monitoring equipment, projection paint is sprayed or projection cloth is covered on the upper surface of a central console, teacher-student interaction is realized by using the monitoring equipment, and central console forms of airplanes of different models are projected on the central console by using the projection assembly; the technical problem that the flight training simulation cabin is high in updating cost for adapting to airplane model updating in the prior art is effectively solved, and the technical effect that the image communication equipment suitable for the flight training simulation cabin can assist the simulation training cabin to simulate the center console of airplanes of various models at low cost so as to meet training requirements is achieved.
Drawings
FIG. 1 is a schematic diagram showing the positional relationship between each component of the image communication equipment and the shell of the cabin body, which is suitable for the flight training simulation cabin of the invention;
FIG. 2 is a schematic diagram showing a positional relationship between an external control panel and a cabin body shell of the image communication equipment for the flight training simulation cabin according to the present invention;
FIG. 3 is a schematic structural diagram of a center console of an image communication device suitable for a flight training simulation cabin according to the present invention;
FIG. 4 is a simplified structural diagram of a diaphragm spacing assembly of the image communication device suitable for use in a flight training simulation cabin in accordance with the present invention;
FIG. 5 is a schematic diagram of a modular receiving bay of an image communication device suitable for use in a flight training simulation bay in accordance with the present invention;
FIG. 6 is a schematic view of the positional relationship between the module accommodating chamber and the closed membrane of the image communication device suitable for the flight training simulation chamber according to the present invention;
FIG. 7 is a schematic diagram showing the positional relationship between a closed membrane and a connecting plate of the image communication device suitable for the flight training simulation cabin according to the present invention;
FIG. 8 is a schematic diagram showing the positional relationship between the learning module body and the closed membrane of the image communication device for the flight training simulation cabin according to the present invention;
FIG. 9 is a schematic diagram showing a positional relationship between a gas storage space and a liquid storage space of an image communication device adapted to a flight training simulation cabin according to the present invention;
FIG. 10 is a schematic view of the position relationship of the first diaphragm and the second diaphragm of the image communication device suitable for use in a flight training simulation chamber according to the present invention;
FIG. 11 is a schematic diagram showing the positional relationship among the air storage space, the liquid storage space and the powder storage space of the image communication device suitable for the flight training simulation cabin according to the present invention;
FIG. 12 is a schematic diagram showing the positional relationship of the first diaphragm, the second diaphragm and the third diaphragm of the image communication device suitable for use in a flight training simulation cabin according to the present invention;
fig. 13 is a schematic structural diagram of a powder storage unit of the image communication equipment suitable for the flight training simulation cabin.
In the figure:
the cabin body comprises a cabin body shell 001, a seat 002, a display screen 003 and an external control screen 004;
a monitoring assembly 100; a projection assembly 200; the device comprises a center console 300, a center console frame 310, a module accommodating bin 320, a bin body bottom plate 321, a bottom plate magnet group 322, a sealing diaphragm 330, a first diaphragm 331, a second diaphragm 332, a third diaphragm 333, an air storage space 334, a liquid storage space 335, a powder storage space 336, a powder storage unit 337, an air pumping assembly 340, a diaphragm limiting assembly 350, a connecting plate 351, a fixing column 352, a positioning groove 353, a fixing pipe 354, a sliding limiting block 355, a stored force pressure spring 356, a releasing assembly 357, a pulling rope 358, a rope body 359, a learning module body 360, a bottom magnet 361 and a side wall magnet 362.
Detailed Description
To facilitate an understanding of the invention, the present application will now be described more fully hereinafter with reference to the accompanying drawings; the preferred embodiments of the present invention are illustrated in the accompanying drawings, but the invention may be embodied in many different forms and should not be construed as limited to the embodiments set forth herein; rather, these embodiments are provided so that this disclosure will be thorough and complete.
It is noted that the terms "vertical," "horizontal," "upper," "lower," "left," "right," and the like as used herein are for illustrative purposes only and do not represent the only embodiments.
Unless defined otherwise, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this invention belongs; the terminology used herein in the description of the invention is for the purpose of describing particular embodiments only and is not intended to be limiting of the invention; as used herein, the term "and/or" includes any and all combinations of one or more of the associated listed items.
Fig. 1 is a schematic diagram showing a positional relationship between each component of the image communication device and a cabin body shell of the flight training simulation cabin according to the present invention; the monitoring equipment of the flight training simulation cabin in the prior art is optimized, the projection assembly 200 is additionally arranged on the monitoring equipment, projection paint is sprayed or projection cloth is covered on the upper surface of the central console 300, the monitoring equipment is utilized to realize the interaction between teachers and students, and the projection assembly 200 is utilized to project the central console 300 forms of different types of airplanes on the central console 300; the technical effect that the image communication equipment suitable for the flight training simulation cabin can assist the simulation training cabin to simulate the center console of airplanes of various types at low cost so as to meet training requirements is achieved.
Example one
As shown in fig. 1 and fig. 2, the image communication device suitable for the flight training simulation cabin of the present application is arranged inside a cabin shell 001 of the flight training simulation cabin, a seat 002, a display screen 003, a training computer and a console 300 are arranged in the flight training simulation cabin, and an external control screen 004 is arranged outside the flight training simulation cabin; the display screen 003 is a component of a vision system; a monitoring component 100 and a projection component 200 are fixed on the inner wall of the top of the bin body shell 001; the monitoring component 100 is a ball head camera, plays a role in monitoring the actions of students in the flight training simulation cabin, the monitoring component 100 is in signal connection with the external control screen 004, and images shot by the monitoring component 100 can be displayed on the external control screen 004 for a training teacher to watch; the projection assembly 200 is used for projecting the recorded or synthesized image onto the upper surface of the center console 300, displaying the structure of each component (key) on the center console 300 and the state of each indicator light, and further simulating the center consoles 300 of airplanes of different models; the center console 300 is sprayed with projection paint or positioned with a projection curtain; the projection assembly 200 is preferably a projector, which is in signal connection with the training computer; the external control screen 004 is in signal connection with a training computer, a teacher can correct and prompt in real time in the operation process of a student, and a training teacher can modify images projected by the projection assembly 200 in real time by controlling the external control screen 004 according to requirements (equivalent to switching PPT pages; after the student makes a specific action, the teacher switches different images by clicking) or give a prompt (equivalent to drawing lines on dynamic or static images displayed on a screen by a handheld mouse, which is the prior art and is not repeated herein);
the technical scheme in the embodiment of the application at least has the following technical effects or advantages:
the technical problem that the flight training simulation cabin is high in updating cost for adapting to airplane model updating in the prior art is solved, and the technical effect that the image communication equipment suitable for the flight training simulation cabin can assist the simulation training cabin to simulate the center console of airplanes of various models at low cost so as to meet training requirements is achieved.
Example two
In order to further improve the practicality of this application, optimize the training effect, the formation of supplementary student's custom, this application embodiment has optimized the structure of the display position of projected on the basis of above-mentioned embodiment to add modular brake valve lever, control button and be used for improving the interactivity, specifically do:
as shown in fig. 3 to 8, the center console 300 includes a center console frame 310, a module accommodating chamber 320, a closing diaphragm 330, a pumping assembly 340, a diaphragm restraining assembly 350, and a learning module body 360;
the console frame 310 is a frame structure or a box structure, and is positioned on the bin body shell 001 for carrying the module accommodating bin 320;
the module accommodating bin 320 is a box structure with an open top and is fixed on the console frame 310, and a bin body bottom plate 321 is arranged at the bottom of the module accommodating bin 320;
the sealing diaphragm 330 is a soft film, preferably made of rubber, and is fixed on the inner wall of the module accommodating bin 320 to seal the module accommodating bin 320, so as to form a sealed space;
the pumping assembly 340 is positioned on the console frame 310, preferably a pump, and controlled by a training computer to adjust the amount of gas in the enclosed space and thus control the expansion and contraction of the sealing diaphragm 330;
the diaphragm limiting assembly 350 is used for fixing one part or a plurality of parts of the sealing diaphragm 330 on the bin body bottom plate 321 according to requirements, so as to limit the expansion shape of the sealing diaphragm 330 and facilitate the installation and fixation of the learning module body 360; the diaphragm restraint assembly 350 is preferably configured as a magnet assembly or snap.
As shown in fig. 3, the whole learning module body 360 is a block shape and has various specifications, and different control component models (a handle model, a joystick model, a key model, etc.) are arranged on the learning module bodies 360 with different specifications; the upper surface of the learning module body 360 is coated with projection paint or provided with a projection curtain; the learning module body 360 is fixed on the closed diaphragm 330 through a magnet, a buckle, and the like, and is indirectly fixed on the diaphragm limiting component 350; when the multifunctional learning module is used, the learning module body 360 (similar to a font template printed by type characters) is stacked on the closed diaphragm 330 (can be freely adjusted according to the model of an airplane), then the closed diaphragm 330 below the learning module body 360 is fixed on the cabin body bottom plate 321 by using the diaphragm limiting component 350, finally the air pumping component 340 is controlled to pump air, and the learning module body 360 except the top surface is covered by using the closed diaphragm 330; the upper surfaces of the closing diaphragm 330 and the learning module body 360 serve as projection surfaces.
Further, as shown in fig. 4 and 6, the number of the diaphragm limiting assemblies 350 is multiple, and the diaphragm limiting assemblies 350 are densely distributed on the closed diaphragm 330 and comprise a connecting plate 351, a fixing column 352, a fixing tube 354, a sliding limiting block 355, a power storage compression spring 356 and a release assembly 357; the connecting plate 351 is plate-shaped, is integrally a magnet or is provided with a magnet in a positioning mode, and is fixed on the closed diaphragm 330 to play a role in connecting the closed diaphragm 330 with the fixing column 352 and a role in adsorbing and fixing the learning module body 360; a bottom magnet 361 is positioned at the bottom of the learning module body 360; the fixing column 352 is fixed on the connecting plate 351, and an annular positioning groove 353 is formed in the side wall of the fixing column 352; the fixing post 352 can be inserted into the fixing tube 354; the fixed pipes 354 are fixed on the bin body bottom plate 321 and correspond to the fixed columns 352 one by one, and holes for accommodating the sliding limiting blocks 355 are formed in the inner walls of the fixed pipes 354; the sliding limiting block 355 is a wedge-shaped block and is positioned on the inner wall of the fixed pipe 354 in a sliding manner; the power storage pressure spring 356 is positioned in a hole in the inner wall of the fixed pipe 354 and abuts against the sliding limit block 355; after the fixed column 352 is inserted into the fixed pipe 354, the sliding limiting block 355 is inserted into the positioning groove 353 under the elastic force action of the power storage pressure spring 356 to limit the axial movement of the fixed column 352; the releasing assembly 357 is used for driving the sliding limiting block 355 to be separated from the positioning groove 353, and is of a telescopic rod structure, a winding structure and the like.
Further, the release assembly 357 includes a pulling rope 358 and a rope pulling assembly 359; one end of the pulling rope 358 is positioned on the slide stopper 355, and the other end is fixed to the rope pulling assembly 359; the rope pulling assembly 359 is of a reel structure and is manually or electrically rotated; pulling the pull cord 358 to displace as it rotates.
EXAMPLE III
As shown in fig. 8, in view of the fact that the closed diaphragm 330 may form a large annular arc surface at the contact position of the two after expanding and wrapping the learning module body 360, which affects the projection effect, the embodiment of the present application optimizes the closed diaphragm 330 based on the above embodiments, so as to improve the projection effect; the method specifically comprises the following steps:
preferably, as shown in fig. 9 and 10, the closing diaphragm 330 is a double-layer film, and includes a first diaphragm 331 and a second diaphragm 332, and both the first diaphragm 331 and the second diaphragm 332 are fixed on the side wall of the module accommodating chamber 320; a space formed by the first diaphragm 331 and the module accommodating chamber 320 is a gas storage space 334, and gas is filled in the gas storage space 334; the second membrane 332 is located above the first membrane 331, and the distance between the second membrane 332 and the first membrane 331 is preferably 2 cm, the second membrane 332, the first membrane 331 and the module accommodating chamber 320 form a liquid storage space 335 for storing liquid, and the liquid storage space 335 is filled with liquid; as shown in fig. 10, the liquid gravity can be used to make the sealing diaphragm 330 more fit to the sidewall of the learning module body 360 to improve the projection effect.
Preferably, as shown in fig. 11 and 12, the closing membrane 330 is a three-layer membrane including a first membrane 331, a second membrane 332 and a third membrane 333, all of which are fixed to the side wall of the module accommodating chamber 320; a space formed by the first diaphragm 331 and the module accommodating chamber 320 is a gas storage space 334, and gas is filled in the gas storage space 334; the second membrane 332 is located above the first membrane 331, and the distance between the second membrane 332 and the first membrane 331 is preferably 2 cm, the second membrane 332, the first membrane 331 and the module accommodating chamber 320 form a liquid storage space 335 for storing liquid, and the liquid storage space 335 is filled with liquid; the third membrane 333 is located above the second membrane 332, the distance between the third membrane 333 and the second membrane 332 is preferably 1 cm, the third membrane 333, the second membrane 332 and the module accommodating chamber 320 together form a powder storage space 336 for storing iron powder, and the powder storage space 336 is filled with iron powder; a sidewall magnet 362 is positioned on the sidewall of the learning module body 360; as shown in fig. 12, the side wall magnets 362 magnetically urge the sealing diaphragm 330 to more closely fit the side wall of the learning module body 360 to enhance the projection effect.
Preferably, the sealing membrane 330 is a double-layer membrane, and forms an air storage space 334 and a powder storage space 336 together with the module accommodating chamber 320; a sidewall magnet 362 is positioned on the sidewall of the learning module body 360; the powder storage space 336 is filled with iron powder.
Preferably, as shown in fig. 12, a bottom plate magnet group 322 is positioned on the bottom plate 321 of the storage chamber, and the closed membrane 330 tends to be smooth and gentle by the cooperation of the bottom plate magnet group 322 and the iron powder filled in the powder storage space 336, so as to obtain a better projection effect.
Preferably, as shown in fig. 13, in order to avoid the concentrated influence of the iron powder on the adsorption effect, the powder storage space 336 is divided into a plurality of powder storage units 337 by welding or sewing.
The above description is only a preferred embodiment of the present invention and is not intended to limit the present invention, and various modifications and changes may be made to the present invention by those skilled in the art. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.
Claims (8)
1. An image communication device suitable for a flight training simulation cabin is arranged inside a cabin body shell (001) of the flight training simulation cabin, a display screen (003), a training computer and a central console (300) are arranged in the flight training simulation cabin, and the image communication device is characterized in that an external control screen (004) is arranged outside the flight training simulation cabin;
a monitoring component (100) and a projection component (200) are fixed on the inner wall of the top of the bin body shell (001);
the monitoring component (100) is a ball head camera, the monitoring component (100) is in signal connection with the external control screen (004), and images shot by the monitoring component (100) can be displayed on the external control screen (004) for a training teacher to watch;
the projection assembly (200) is used for projecting the recorded or synthesized image to the upper surface of the center console (300) and displaying the structure of each part on the center console (300) and the state of various indicator lights;
the center console (300) is sprayed with projection paint or positioned with a projection curtain;
the projection assembly (200) is in signal connection with the training computer;
the external control screen (004) is in signal connection with the training computer, a teacher can correct and prompt in real time in the operation process of a student, and a training teacher can modify images projected by the projection assembly (200) in real time or give a prompt by controlling the external control screen (004) according to requirements;
the center console (300) comprises a center console framework (310), a module accommodating bin (320), a sealing diaphragm (330), an air pumping assembly (340), a diaphragm limiting assembly (350) and a learning module body (360);
the center console frame (310) is of a frame structure or a box structure;
the module accommodating bin (320) is of a box body structure with an opening at the top and is fixed on the center console frame (310), and the bottom of the module accommodating bin (320) is a bin body bottom plate (321);
the sealing diaphragm (330) is a soft film and is fixed on the inner wall of the module accommodating bin (320) to seal the module accommodating bin (320) to form a sealed space;
the pumping assembly (340) is controlled by a training computer and plays a role in adjusting the gas amount in the closed space;
the diaphragm limiting assembly (350) is used for fixing one part or a plurality of parts of the closed diaphragm (330) on the bin body bottom plate (321) according to requirements, so that the expansion shape of the closed diaphragm (330) is limited, and the installation and fixation of the learning module body (360) are facilitated;
the diaphragm limiting assembly (350) is in a magnet group or a buckle structure;
the whole learning module body (360) is in a block shape and has various specifications, and different control component models are arranged on the learning module bodies (360) with different specifications;
the upper surface of the learning module body (360) is coated with projection paint or provided with a projection curtain;
the learning module body (360) is fixed on the closed diaphragm (330) through a magnet or a buckle and is indirectly fixed on the diaphragm limiting component (350);
the number of the diaphragm limiting assemblies (350) is multiple, the diaphragm limiting assemblies are densely distributed on the closed diaphragm (330), and each diaphragm limiting assembly comprises a connecting plate (351), a fixed column (352), a fixed pipe (354), a sliding limiting block (355), a force accumulating pressure spring (356) and a releasing assembly (357);
the connecting plate (351) is plate-shaped, is integrally a magnet or is positioned on the magnet, and is fixed on the closed diaphragm (330) to play a role in connecting the closed diaphragm (330) with the fixing column (352) and a role in adsorbing and fixing the learning module body (360);
a bottom magnet (361) is positioned at the bottom of the learning module body (360);
the fixing column (352) is fixed on the connecting plate (351), and an annular positioning groove (353) is formed in the side wall of the fixing column (352);
the fixing post (352) is insertable into the fixing tube (354);
the fixed pipes (354) are fixed on the bin body bottom plate (321) and correspond to the fixed columns (352) one by one, and holes for accommodating the sliding limiting blocks (355) are formed in the inner walls of the fixed pipes (354);
the sliding limiting block (355) is a wedge-shaped block and is positioned on the inner wall of the fixed pipe (354) in a sliding mode; the power storage compression spring (356) is positioned in a hole in the inner wall of the fixed pipe (354) and abuts against the sliding limiting block (355);
after the fixed column (352) is inserted into the fixed pipe (354), the sliding limiting block (355) is inserted into the positioning groove (353) under the action of the elastic force of the power storage pressure spring (356) to limit the axial movement of the fixed column (352);
the release assembly (357) is used for driving the sliding limiting block (355) to be separated from the positioning groove (353).
2. The image communication device adapted for use in a flight training simulation suite of claim 1, wherein: the release assembly (357) comprises a pulling rope (358) and a rope pulling assembly (359);
one end of the pulling rope (358) is positioned on the sliding limiting block (355), and the other end is fixed on the rope body pulling assembly (359);
the rope body dragging assembly (359) is of a reel structure, and the rope body dragging assembly is manually or electrically rotated, and pulls the dragging rope (358) to displace during rotation.
3. The image communication device of claim 1, adapted for use in a flight training simulation suite, wherein: the closed membrane (330) is a double-layer membrane and comprises a first membrane (331) and a second membrane (332), and the first membrane (331) and the second membrane (332) are fixed on the side wall of the module accommodating bin (320);
a space formed by the first diaphragm (331) and the module accommodating bin (320) is a gas storage space (334), and gas is filled in the gas storage space (334);
the second membrane (332) is located above the first membrane (331), and the second membrane (332) forms a reservoir space (335) for storing liquid together with the first membrane (331) and the module accommodating chamber (320).
4. The image communication device of claim 1, adapted for use in a flight training simulation suite, wherein: the closed diaphragm (330) is a three-layer diaphragm, and comprises a first diaphragm (331), a second diaphragm (332) and a third diaphragm (333), which are all fixed on the side wall of the module accommodating bin (320);
a space formed by the first diaphragm (331) and the module accommodating bin (320) is a gas storage space (334), and gas is filled in the gas storage space (334); the second diaphragm (332) is positioned above the first diaphragm (331), and the second diaphragm (332), together with the first diaphragm (331) and the module accommodating bin (320), forms a liquid storage space (335) for storing liquid;
the third membrane (333) is positioned above the second membrane (332), the third membrane (333), the second membrane (332) and the module accommodating bin (320) jointly form a powder storage space (336) for storing iron powder, and the powder storage space (336) is filled with the iron powder;
a sidewall magnet (362) is positioned on a sidewall of the learning module body (360).
5. The image communication device adapted for use in a flight training simulation suite of claim 1, wherein: the closed membrane (330) is a double-layer membrane and forms a gas storage space (334) and a powder storage space (336) together with the module accommodating bin (320);
a sidewall magnet (362) is positioned on the sidewall of the learning module body (360); and iron powder is filled in the powder storage space (336).
6. An image communication device adapted for use in a flight training simulation suite according to claim 4 or claim 5, wherein: a soleplate magnet group (322) is positioned on the bin body soleplate (321), and the soleplate magnet group (322) is matched with iron powder filled in the powder storage space (336) to enable the closed diaphragm (330) to tend to be gentle.
7. An image communication device adapted for use in a flight training simulation suite according to claim 4 or claim 5, wherein: the powder storage space (336) is divided into a plurality of powder storage units (337) by welding or sewing.
8. The image communication device of claim 1, adapted for use in a flight training simulation suite, wherein: the control component model is a handle model, a control lever model and/or a key model.
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| CN202211140293.4A CN115225868B (en) | 2022-09-20 | 2022-09-20 | Image communication equipment suitable for flight training simulation storehouse |
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| CN202211140293.4A CN115225868B (en) | 2022-09-20 | 2022-09-20 | Image communication equipment suitable for flight training simulation storehouse |
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Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN202632580U (en) * | 2012-03-07 | 2012-12-26 | 北京欣远诚业科技有限公司 | Integrated training simulator of flight and ejector of airplane |
| CN107396058A (en) * | 2017-08-23 | 2017-11-24 | 芜湖超源力工业设计有限公司 | A kind of special fly simulation training supervising device of space flight |
| CN210466838U (en) * | 2019-06-30 | 2020-05-05 | 卓尔飞机制造（武汉）有限公司 | Flight simulator |
| CN214796324U (en) * | 2020-12-25 | 2021-11-19 | 西安联高电子***工程有限公司 | Flight simulation storehouse emulation display device |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20150379884A1 (en) * | 2013-02-05 | 2015-12-31 | One-G, Llc | Aircraft simulator |
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Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN202632580U (en) * | 2012-03-07 | 2012-12-26 | 北京欣远诚业科技有限公司 | Integrated training simulator of flight and ejector of airplane |
| CN107396058A (en) * | 2017-08-23 | 2017-11-24 | 芜湖超源力工业设计有限公司 | A kind of special fly simulation training supervising device of space flight |
| CN210466838U (en) * | 2019-06-30 | 2020-05-05 | 卓尔飞机制造（武汉）有限公司 | Flight simulator |
| CN214796324U (en) * | 2020-12-25 | 2021-11-19 | 西安联高电子***工程有限公司 | Flight simulation storehouse emulation display device |
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