CN220357699U - Flight illusion induction simulation training system - Google Patents
Flight illusion induction simulation training system Download PDFInfo
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- CN220357699U CN220357699U CN202321061527.6U CN202321061527U CN220357699U CN 220357699 U CN220357699 U CN 220357699U CN 202321061527 U CN202321061527 U CN 202321061527U CN 220357699 U CN220357699 U CN 220357699U
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- 238000012549 training Methods 0.000 title claims abstract description 69
- 238000004088 simulation Methods 0.000 title claims abstract description 30
- 230000006698 induction Effects 0.000 title claims abstract description 18
- 230000033001 locomotion Effects 0.000 claims abstract description 24
- 238000004513 sizing Methods 0.000 claims abstract description 18
- 238000004891 communication Methods 0.000 description 11
- 238000012545 processing Methods 0.000 description 11
- 239000003638 chemical reducing agent Substances 0.000 description 9
- 230000000007 visual effect Effects 0.000 description 9
- 238000011065 in-situ storage Methods 0.000 description 6
- 208000037265 diseases, disorders, signs and symptoms Diseases 0.000 description 5
- 230000005540 biological transmission Effects 0.000 description 4
- 238000010586 diagram Methods 0.000 description 4
- 230000001939 inductive effect Effects 0.000 description 4
- 238000000034 method Methods 0.000 description 3
- 238000012544 monitoring process Methods 0.000 description 3
- 230000001105 regulatory effect Effects 0.000 description 3
- 208000012886 Vertigo Diseases 0.000 description 2
- 230000019771 cognition Effects 0.000 description 2
- 230000001276 controlling effect Effects 0.000 description 2
- 230000007547 defect Effects 0.000 description 2
- 230000008921 facial expression Effects 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000008447 perception Effects 0.000 description 2
- 231100000889 vertigo Toxicity 0.000 description 2
- 230000001720 vestibular Effects 0.000 description 2
- 230000001174 ascending effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000036449 good health Effects 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 230000003340 mental effect Effects 0.000 description 1
- 230000005195 poor health Effects 0.000 description 1
- 230000000272 proprioceptive effect Effects 0.000 description 1
- 230000003304 psychophysiological effect Effects 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
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Abstract
Disclosed is a flight illusion induction simulation training system capable of achieving adjustment of flatness of the entire apparatus. The base (1) of the illusion-induced motion module comprises a plurality of adjusting sizing blocks (12) arranged on foundation bolts, each adjusting sizing block is two pairs and is respectively arranged on two sides of the foundation bolts, each pair of adjusting sizing blocks comprises two right-angle triangular prisms and adjusting screws, the inclined planes of the right-angle triangular prisms are in contact, and the contact area of the inclined planes of the two right-angle triangular prisms is adjusted through the adjusting screws, so that height adjustment is achieved.
Description
Technical Field
The utility model relates to the technical field of flight simulation, in particular to a flight illusion induction simulation training system.
Background
Flight space disorientation is also known as "illusion of flight", "disorientation". Refers to incorrect perception by pilots of the status, position, direction, movement, and flight environment of themselves and of the aircraft in flight. According to different bases, different divisions can be made: subjective experience of a pilot can be divided into inclination illusion, pitching illusion, direction illusion, back flight illusion, rotation anti-rotation illusion, speed illusion, altitude illusion, time illusion and the like; the main body vessel tube which causes illusion can be divided into vestibular proprioceptive illusion, optical illusion and vestibular optical illusion; according to the consciousness degree of the pilot to illusion, the system can be divided into type I space orientation disorder, type II space orientation disorder and type III space orientation disorder.
The method is characterized by mainly comprising four points:
(1) Popularity of the use of the methods. Almost all pilots have illusions of different procedural and types of flight in flight.
(2) Burstiness. From the weather conditions, the most illusion occurs in the flight under complex weather conditions; from the model, the illusion occurrence rate of a single aircraft pilot is higher than that of a plurality of aircraft pilots; from the individual condition of pilots, the occurrence rate of illusions is higher for pilots with poor psychological quality and poor health than for pilots with good health.
(3) And (5) harmfulness. Is an important cause of the flight accidents of the general aircraft and the military aircraft.
(4) Can be used for preventing. After the pilot recognizes the objective conditions and subjective factors that create the illusion of flight, it can be prevented and overcome by mental training.
The flight space orientation disorder is essentially a space cognition error caused by the fact that a human body space orientation system cannot meet the three-dimensional space movement environment, and the flight space orientation disorder is urgent to develop psychophysiological training from a space cognition level state of a flight person, develop and improve the instrument vision orientation capability of the flight person, the capability of identifying space orientation, the capability of controlling self wrong space perception and the capability of eliminating interference of the flight person to perform correct manipulation.
The base of the existing flight illusion induction simulation training system is designed as an integral I-beam, and the defect is that the integral height of the equipment is increased, and the flatness of the integral equipment cannot be adjusted during installation.
Disclosure of Invention
In order to overcome the defects of the prior art, the technical problem to be solved by the utility model is to provide a flight illusion induction simulation training system which can realize adjustment of the flatness of the whole equipment.
The technical scheme of the utility model is as follows: the flight illusion induction simulation training system is provided with an illusion induction motion module, wherein a base (1) of the illusion induction motion module comprises a plurality of adjusting sizing blocks (12) arranged on anchor bolts, each adjusting sizing block is two pairs and is respectively arranged on two sides of the anchor bolts, each pair of adjusting sizing blocks comprises two right-angle triangular prisms and an adjusting screw, the inclined surfaces of the right-angle triangular prisms are contacted, and the contact area of the inclined surfaces of the two right-angle triangular prisms is adjusted through the adjusting screw, so that the height adjustment is realized.
The utility model comprises a plurality of adjusting sizing blocks arranged on the foundation bolt, wherein each adjusting sizing block is two pairs and is respectively arranged on two sides of the foundation bolt, each adjusting sizing block comprises two right-angle triangular prisms and an adjusting screw, the inclined surfaces of the right-angle triangular prisms are contacted, and the contact area of the inclined surfaces of the two right-angle triangular prisms is adjusted through the adjusting screw, so that the height adjustment is realized, and the flatness of the whole equipment can be adjusted.
Drawings
FIG. 1 is a schematic diagram of a flight illusion-inducing simulated training system according to the present utility model.
FIG. 2 is a schematic diagram of the external configuration of a flight illusion-inducing simulation training system according to the present utility model.
Fig. 3 is a schematic diagram showing the outline structure of the flash line vertigo inducing device according to the present utility model.
Fig. 4 is a schematic diagram of the structure of the illusion-induced motion module according to the present utility model.
Fig. 5 is a schematic structural view of an eccentric rotation platform of an illusion-induced motion module according to the present utility model.
Detailed Description
As shown in fig. 4, the flight illusion induction simulation training system is provided with an illusion induction motion module, wherein a base 1 of the illusion induction motion module comprises a plurality of adjusting sizing blocks 12 arranged on foundation bolts, each adjusting sizing block is two pairs and is respectively arranged on two sides of the foundation bolts, each pair of adjusting sizing blocks comprises two right-angle triangular prisms and an adjusting screw, inclined surfaces of the right-angle triangular prisms are contacted, and the contact area of the inclined surfaces of the two right-angle triangular prisms is adjusted through the adjusting screw, so that the height adjustment is realized.
The utility model comprises a plurality of adjusting sizing blocks arranged on the foundation bolt, wherein each adjusting sizing block is two pairs and is respectively arranged on two sides of the foundation bolt, each adjusting sizing block comprises two right-angle triangular prisms and an adjusting screw, the inclined surfaces of the right-angle triangular prisms are contacted, and the contact area of the inclined surfaces of the two right-angle triangular prisms is adjusted through the adjusting screw, so that the height adjustment is realized, and the flatness of the whole equipment can be adjusted.
As shown in fig. 1, this illusion-induced flight simulation training system includes: the main control center and the helicopter simulate training equipment;
the master control center includes: the device comprises an instruction transmission module, a voice communication module, a display module and a monitoring module, wherein a training instruction is transmitted to helicopter simulation training equipment through the instruction transmission module, the device is communicated with the helicopter simulation training equipment in real time through the voice communication module, a visual training picture of a first visual angle of a pilot person in the helicopter simulation training equipment and an instrument indication picture of cabin equipment are displayed through the display module, and flying driving manipulation actions and real-time facial expressions of flying training personnel are observed through the monitoring module;
the helicopter simulation training apparatus includes: the system comprises a training instruction processing module, an illusion induced motion module, a simulation cabin, a vision module, a sound and conversation module; the training instruction processing module receives a training instruction transmitted to the helicopter simulation training equipment by the instruction transmitting module and outputs driving parameters to the illusion induced motion module, the simulation cabin, the vision module, the sound and conversation module; the illusion induced motion module receives the driving parameters of the training instruction processing module, drives the mechanical structure of the illusion induced motion module and provides the real sense of the corresponding flight training gesture for the flight training personnel in the simulated seat cabin; the simulation cabin is provided with an operating system and instrument indication which are truly consistent with the corresponding aircraft type, and receives driving parameters of the training instruction processing module; the visual module receives driving parameters of the training instruction processing module, provides a first visual angle image of flight for flight training personnel in the simulated cabin, and the main control center sets and adjusts illusion induction training scenes required by simulated training; the sound and communication module receives driving parameters of the training instruction processing module, provides sound environments for flight training personnel in the simulated cockpit, and carries out voice communication with the master control center, and the flight training personnel in the simulated cockpit receive flight training information of the master control center through the sound and communication module.
According to the utility model, a training instruction is transmitted to the helicopter simulation training equipment through the instruction transmission module, the helicopter simulation training equipment is communicated in real time through the voice communication module, a visual training picture of a first visual angle of a pilot in the helicopter simulation training equipment and an instrument indication picture of the simulation cabin equipment are displayed through the display module, the flying driving operation action and the real-time facial expression of a flying training person are observed through the monitoring module, the training instruction processing module receives the training instruction transmitted to the helicopter simulation training equipment by the instruction transmission module, and driving parameters are output to the illusion induced motion module, the simulation cabin, the visual module, the sound and the communication module; the illusion induced motion module receives the driving parameters of the training instruction processing module, drives the mechanical structure of the illusion induced motion module and provides the real sense of the corresponding flight training gesture for the flight training personnel in the simulated seat cabin; the simulation cabin is provided with an operating system and instrument indication which are truly consistent with the corresponding aircraft type, and receives driving parameters of the training instruction processing module; the visual module receives driving parameters of the training instruction processing module, provides a first visual angle image of flight for flight training personnel in the simulated cabin, and the main control center sets and adjusts illusion induction training scenes required by simulated training; the sound and communication module receives driving parameters of the training instruction processing module, provides an acoustic environment for flight training personnel in the simulated cabin, and carries out voice communication with the master control center, and the flight training personnel in the simulated cabin receive flight training information of the master control center through the sound and communication module; therefore, the method can gradually induce corresponding illusions, can be more attached to actual flight training, greatly improves the illusion induction success rate, can adjust the induction scene in real time, enables helicopter flight training personnel to keep fresh feeling and mystery feeling when carrying out lesson training, can greatly improve the interests of the flight training personnel compared with the conventional fixed induction scene, can help the helicopter flight personnel to understand and identify the flight illusions, and can effectively treat and reduce similar flight accidents when encountering the illusions.
Preferably, the master control center is disposed in proximity to the helicopter simulated training apparatus. The working state of the helicopter simulation training equipment is conveniently checked, so that the training posture of the helicopter simulation training equipment can be guided and adjusted.
Preferably, as shown in fig. 2, 4, 5, the illusion-induced motion module includes: the device comprises a base 1, an eccentric rotating platform 2, an eccentric adjusting platform 3, a six-degree-of-freedom moving platform 4 and an in-situ rotating platform 5;
the base is fixed to the ground by anchor bolts 11; the eccentric rotary platform comprises two driving motors 21, two speed reducers 22 and a rotary support 23, wherein each driving motor is arranged on the base and is connected with one speed reducer, the rotary support is arranged at the peripheries of the driving motor and the speed reducers, and the inner ring of the rotary support is provided with a gear matched with the speed reducer; the eccentric adjusting platform is arranged above the rotary support and connected with the rotary support, and a control mechanism and a motor driving mechanism are respectively arranged at two ends of the diameter of the eccentric adjusting platform; one of the six-degree-of-freedom motion platform and the in-situ rotation platform is arranged above the eccentric adjustment platform, and the other is arranged above the one; the in-situ rotating platform is a roller bearing; the simulation cabin 6 is installed at the uppermost part;
the in-situ rotating platform simulates actual flight azimuth adjustment and helicopter fault rotation for flight training personnel; the six-degree-of-freedom motion platform provides the motion sensing gesture of pitching, rolling, tilting, ascending, descending and traversing of the airplane for flight training personnel; the eccentric rotary platform provides a spiral sense when illusion is induced, and the eccentric adjusting platform adjusts the intensity of the spiral sense; the base provides a fixed base and a smooth architecture for the illusion-induced motion module.
The eccentric rotating platform comprises two driving motors and two speed reducers, so that the emergency stop can be ensured to be more stable and accurate; each driving motor is arranged on the base and is connected with a speed reducer, the rotary support is arranged on the periphery of the driving motor and the periphery of the speed reducer, the inner ring of the rotary support is provided with a gear matched with the speed reducer, thus the eccentric rotary platform is fixed on the static base instead of the moving eccentric regulating platform, the carrying capacity of the eccentric regulating platform is reduced, the weight of the moving mechanism of the eccentric regulating platform is reduced, namely the weight of the moving mechanism is reduced, and the driving motor and the speed reducer are arranged in the rotary support, so that the wind resistance of equipment rotation is greatly reduced; the eccentric adjusting platform is provided with a control mechanism and a motor driving mechanism at two ends of the diameter respectively, so that the center of gravity distribution at two sides is balanced, and the rotation is more stable; the six-degree-of-freedom motion platform and the in-situ rotation platform can be exchanged in position, so that the installation is more flexible; the in-situ rotating platform is a roller bearing, and compared with the ball bearing, the overturning force is increased, and the equipment is stable and reliable during high-speed rotation or sudden stop.
Preferably, as shown in fig. 3, the system further comprises a glint vertigo inducing device 7, which simulates the effect of the rotor shadows of an aircraft, inside the cabin and comprises: the device comprises a driving unit 71, a rotating unit 72 and a mounting base 73, wherein the device is mounted on the upper side of the base of the illusion-induced motion module through the mounting base, the driving unit is in remote communication data link with a main control center, and the driving unit is used for controlling the start and stop of the rotating unit and the rotation speed adjustment after receiving an instruction of the main control center.
The present utility model is not limited to the preferred embodiments, but can be modified in any way according to the technical principles of the present utility model, and all such modifications, equivalent variations and modifications are included in the scope of the present utility model.
Claims (1)
1. Flight illusion induction simulation training system, its characterized in that: the base (1) of the illusion-induced motion module comprises a plurality of adjusting sizing blocks (12) arranged on foundation bolts, each adjusting sizing block is two pairs and is respectively arranged on two sides of the foundation bolts, each pair of adjusting sizing blocks comprises two right-angle triangular prisms and adjusting screws, the inclined planes of the right-angle triangular prisms are in contact, and the contact area of the inclined planes of the two right-angle triangular prisms is adjusted through the adjusting screws, so that height adjustment is achieved.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321061527.6U CN220357699U (en) | 2023-05-05 | 2023-05-05 | Flight illusion induction simulation training system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321061527.6U CN220357699U (en) | 2023-05-05 | 2023-05-05 | Flight illusion induction simulation training system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220357699U true CN220357699U (en) | 2024-01-16 |
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ID=89484312
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202321061527.6U Active CN220357699U (en) | 2023-05-05 | 2023-05-05 | Flight illusion induction simulation training system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220357699U (en) |
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2023
- 2023-05-05 CN CN202321061527.6U patent/CN220357699U/en active Active
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