WO2019184041A1 - 一种用于体验载人飞行器逃生的牵引伞型弹射座椅模拟器 - Google Patents

一种用于体验载人飞行器逃生的牵引伞型弹射座椅模拟器 Download PDF

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Publication number
WO2019184041A1
WO2019184041A1 PCT/CN2018/084683 CN2018084683W WO2019184041A1 WO 2019184041 A1 WO2019184041 A1 WO 2019184041A1 CN 2018084683 W CN2018084683 W CN 2018084683W WO 2019184041 A1 WO2019184041 A1 WO 2019184041A1
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experiencing
manned aircraft
support plate
simulator
seat
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PCT/CN2018/084683
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English (en)
French (fr)
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谢文丽
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谢文丽
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Publication of WO2019184041A1 publication Critical patent/WO2019184041A1/zh

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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
    • 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
    • G09B9/085—Special purpose teaching, e.g. alighting on water, aerial photography
    • 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
    • G09B9/12—Motion systems for aircraft simulators
    • G09B9/14—Motion systems for aircraft simulators controlled by fluid actuated piston or cylinder ram

Definitions

  • the present invention relates to the field of virtual reality devices, and more particularly to a traction umbrella type ejection seat simulator for experiencing the escape of a manned aircraft.
  • the manned aircraft is mostly equipped with an ejection seat Ejection seat, which is a seat for the manned aircraft driver.
  • Ejection seat which is a seat for the manned aircraft driver.
  • the driver is ejected out of the cabin by the power device under the seat.
  • the seat-type life-saving device that opens the parachute to make the driver safely land.
  • the technical problem to be solved by the present invention is: in order to overcome the above problems, a traction umbrella type ejection seat simulator for experiencing the escape of a manned aircraft is provided, which has a reasonable structure, simple structure, simple operation and cost. Low, safe and reliable, strong sense of reality, high degree of intelligence, etc., effectively solve the problem of not being able to eject the seat escape training and experience on a real manned aircraft.
  • a traction type ejection device simulator for experiencing the escape of a manned aircraft, comprising a base, a guide rail, a power device, a somatosensory seat, a head mounted display and a
  • the base is provided with a box body, a controller and an air pump
  • the upper cover of the box body is provided with a plurality of ventilation holes
  • the inner body cavity of the box body is connected with the air pump, and the air pump is controlled Electrically connected to each other;
  • the guide rail is an I-shaped structure with chutes on both sides, and the guide rail is vertically fixedly disposed on the base along the traveling direction of the chute;
  • the power device includes a first support plate, a hydraulic rod, a guide wheel set, a first rotating shaft, a connecting plate, a motor and a gear set; the two ends of the hydraulic rod are fixedly connected to the base and the first supporting plate respectively;
  • the guide wheel sets are respectively rotatably connected to the second rotating shaft fixedly disposed on the first supporting plate, and the guiding wheel sets abut against the sliding grooves on the guide rail;
  • the motor is fixed on the first support plate, and the motor main shaft is drivingly connected with the gear set; one end of the first rotating shaft is drivingly connected with the gear set, and the other end of the first rotating shaft is disposed through the supporting plate.
  • the guide rail is provided with a plurality of first magnetic proximity switches
  • the guide wheel set is provided with a first magnet
  • the first support plate is provided with a second magnetic proximity switch, correspondingly on the first rotating shaft Providing a plurality of second magnets
  • the top of the rail is provided with a third support plate, and the third support plate is provided with a plurality of illumination lamps and a nozzle, wherein the nozzles are connected to the air pump;
  • the control pull ring includes a pull ring body and a pull cord; the upper end of the pull cord is fixedly disposed on the third support board; the pull ring body is inlaid with a control button, a wireless transmitting module, a tension sensor, and a buffer spring, one end of the tension sensor is fixedly disposed in the body cavity of the pull ring, and the other end of the tension sensor is connected with the lower end of the pull cord, and a buffer spring is disposed between the tension sensor and the body of the pull ring.
  • the somatosensory seat includes a second support plate fixedly coupled to the connecting plate, a cushion disposed on the second support plate, and a safety pressing bar; the cushion is provided with a speaker; the safety pressure is One end of the bar is hinged to the second support plate, and the other end of the safety press bar is connected to the second support plate by a seat belt.
  • a plurality of airbags connected to the air pump are disposed between the second support plate and the cushion, and the second support plate is further provided with a restraining strap for binding the foot.
  • an electric cylinder is fixedly disposed on the second support plate, and a pedal provided with a footrest is fixed on the main shaft of the electric cylinder.
  • the pedal is provided with a first pressure sensor.
  • the safety pressure bar is provided with a cushion rubber pad, and a second pressure sensor is disposed between the buffer rubber pad and the safety pressure bar.
  • the second pressure sensor is a sheet type pressure sensor.
  • the bottom of the somatosensory seat is provided with a vibration motor.
  • the motor, the illumination lamp, the second magnetic proximity switch, the electric cylinder, the first pressure sensor, the second pressure sensor, the vibration motor, the first magnetic proximity switch, and the head mounted display are respectively mutually connected with the controller Electrical connection.
  • the first rotating shaft is provided with a connecting member and a plurality of steering cylinders circumferentially disposed along a central axis of the first rotating shaft, and both ends of the steering cylinder are respectively hinged with the connecting member and the connecting plate.
  • a traction type ejection mount simulator for experiencing the escape of a manned aircraft, comprising a base, a guide rail, a power unit, a somatosensory seat, a head mounted display and a pair of control pull rings, wherein
  • the air pump installed on the base simulates the change of the airflow when the ejection is carried out through the box body and the nozzle.
  • the guide rail is vertically arranged on the base, and the power device pushes the up, down, flipping and tilting movements of the somatosensory seat to simulate the change of the position of the ejection and the landing, and the sense of body.
  • the seat is fixed to the human body while using the airbag to simulate the impact of weight loss and overweight on the body, while the control pull ring is used to simulate the operation of the parachute during landing. All operations are processed and transmitted to the head-mounted display; the structure is reasonable
  • the utility model has the advantages of simple structure, convenient use, simple operation, low cost, safety and reliability, strong realism and high intelligence, and effectively solves the problem that the ejection seat escape training and experience cannot be performed on a real manned aircraft.
  • FIG. 1 is a schematic view showing the overall structure of a traction type ejection type seat simulator for experiencing the escape of a manned aircraft according to the present invention
  • FIG. 2 is a top plan view showing a traction type ejection type seat simulator for experiencing the escape of a manned aircraft according to the present invention
  • FIG. 3 is a schematic view showing a connection structure of a body-sensing seat and a power device of a traction type-type ejection seat simulator for experiencing manned aircraft escape according to the present invention
  • FIG. 4 is an enlarged schematic view showing a partial structure of a somatosensory seat of a traction type ejection type seat simulator for experiencing manned aircraft escape according to the present invention
  • FIG. 5 is a schematic view showing the structure of a control pull ring of a traction type ejection type seat simulator for experiencing the escape of a manned aircraft according to the present invention.
  • a traction type ejection mount simulator for experiencing manned aircraft escape comprising a base 1, a guide rail 2, a power unit 3, a somatosensory seat 4, an accelerometer and a gyroscope a head mounted display 5 and a pair of control pull rings 6, wherein the base 1 is provided with a box 11, a controller 12 and an air pump 13, and the upper cover 111 of the box 11 is provided with a plurality of ventilation holes.
  • the inner cavity of the casing 11 is in communication with the air pump 13, and the air pump 13 is electrically connected to the controller 12.
  • the controller 12 controls the air pump 13 to supply air into the casing 11, and the gas is ejected through the vent hole to simulate ejection. Airflow during seat landing;
  • the guide rail 2 is an I-shaped structure with chutes on both sides, and the guide rail 2 is vertically fixedly disposed on the base 1 along the traveling direction of the chute;
  • the power device 3 includes a first support plate 31, a hydraulic rod 32, a guide wheel set 33, a first rotating shaft 34, a connecting plate 35, a motor 36 and a gear set 37; the two ends of the hydraulic rod 32 and the base 1 respectively
  • the first support plates 31 are fixedly connected to each other;
  • the guide wheel sets 33 are respectively rotatably connected to the second rotating shaft 313 fixedly disposed on the first support plate 31, and the guide wheel sets 33 are sliding with the guide rails 2
  • the slots abut each other;
  • the motor 36 is fixed on the first support plate 31, and the main shaft of the motor 36 is drivingly connected with the gear set 37; one end of the first rotating shaft 34 is drivingly connected with the gear set 37, and the other end of the first rotating shaft 34 is Passing through the bearing 311 disposed on the support plate and connecting to the connecting plate 35 through the universal joint 342;
  • the first rotating shaft 34 is provided with a connecting member 38 and a plurality of steering cylinders 39 circumferentially disposed along a central axis of the first rotating shaft 34.
  • the two ends of the steering cylinder 39 are respectively hinged to the connecting member 38 and the connecting plate 35.
  • the first support plate 31, the hydraulic rod 32, the first rotating shaft 34, the connecting plate 35, the motor 36 and the gear set 37 can move up and down along the guide rail 2 under the action of the hydraulic rod 32 and the guide wheel set 33, the first rotating shaft 34, under the action of the motor 36, the connecting plate 35 is rotated, and the steering cylinder 39 disposed on the first rotating shaft 34 is used to adjust the orientation of the connecting plate 35. Since the connecting plate 35 is directly connected to the somatosensory seat 4, the hydraulic rod 32, the first The rotating shaft 34 and the steering cylinder 39 indirectly control the up and down movement and the tilting movement of the somatosensory seat 4.
  • the guide rail 2 is provided with a plurality of first magnetic proximity switches 21, a first magnet 331 is disposed on the guide wheel set 33, and a second magnetic proximity switch 312 is disposed on the first support plate 31.
  • a plurality of second magnets 341 are circumferentially disposed on the first rotating shaft 34; the first magnetic proximity switch 21 and the first magnet 331 cooperate with each other to determine the height of the guiding wheel set 33 from the ground, and indirectly derive other components of the power unit 3 from the ground.
  • the distance and the data is sent to the controller 12; similarly, the second magnetic proximity switch 312 and the second magnet 341 cooperate to measure the angle at which the first shaft 34 rotates, and send the data to the controller 12 for data. deal with.
  • the top of the guide rail 2 is provided with a third support plate 22, and a plurality of illumination lamps 221 and a shower head 222 are disposed on the third support plate 22, wherein the spray head 222 is connected to the air pump 13; and the spray head 222 is used for simulating the ejection seat.
  • the control pull ring 6 includes a pull ring body 60 and a pull cord 65; the upper end of the pull cord 65 is fixedly disposed on the third support plate 22; the pull ring body 60 is inlaid with a control button 61, a wireless transmitting module 62, a tension sensor 63, and a buffer spring 64.
  • One end of the tension sensor 63 is fixedly disposed in the inner cavity of the pull ring body 60, and the other end of the tension sensor 63 is connected to the lower end of the pull cord 65, and A buffer spring 64 is disposed between the tension sensor 63 and the tab body 60.
  • the function of the control pull ring 6 is to simulate the operation of the parachute during the landing of the ejection seat, such as pulling the pull ring to control the opening time of the parachute, pulling the pull ring to control the direction of the parachute, pressing the control button 61 to block the parachute rope, etc., and controlling the pull ring
  • the data generated by the inner control button 61 and the tension sensor 63 is passed through the controller 12 by the wireless transmitting module 62 for data processing.
  • the somatosensory seat 4 includes a second support plate 41 fixedly coupled to the connecting plate 35, a cushion 42 disposed on the second support plate 41, and a safety pressing bar 45; the cushion 42 is provided with a speaker 421; One end of the safety pressing bar 45 is hinged to the second supporting plate 41, and the other end of the safety pressing bar 45 is connected to the second supporting plate 41 through the seat belt 451.
  • a plurality of airbags 43 connected to the air pump 13 are disposed between the second support plate 41 and the cushion 42.
  • the second support plate 41 is further provided with a restraining strap 452 for binding the foot;
  • An electric cylinder 44 is fixedly disposed on the two supporting plates 41.
  • a pedal 442 is disposed on the main shaft of the electric cylinder 44.
  • the pedal 442 is provided with a first pressure sensor 441.
  • the safety pressure bar 45 is disposed on the pedal
  • a cushioning pad 47 is disposed, and a second pressure sensor 471 for detecting the pressure of the upper limb of the human body relative to the safety pressing bar 45 is disposed between the cushioning pad 47 and the safety pressing bar 45, and the data is transmitted to the controller 12 for data.
  • the second pressure sensor 471 is a sheet type pressure sensor.
  • a vibration motor 46 is disposed at the bottom of the somatosensory seat 4.
  • the airbag 43 is mainly used for the pressure of the seat on the upper limb of the human body in the weightless and overweight environment.
  • the airbag 43 should accommodate a certain air before use.
  • the power device 3 When the simulated ejection seat is ejected upward, the power device 3 first follows the guide rail 2 Acceleration upwards produces a true sense of overweight, while the airbag 43 is vented outwardly, and the drop of the upper limb of the human body results in a significant reduction in the sense of compression relative to the safety strut 45, resulting in a sustained overweight feeling after the power unit 3 notifies the movement;
  • the power device 3 first accelerates downward along the guide rail 2 to generate a true sense of weight loss, and simultaneously inflates the airbag 43.
  • the airbag 43 When the power device 3 rises to a certain height and the airbag 43 is filled with a certain amount of gas, the airbag 43 is soft in texture. The pressure on the upper limbs of the human body is much greater than that of other parts, resulting in a continuous sense of weight loss.
  • the electric cylinder 44 drives the pedal 442 to move up and down to generate or not support the lower limbs of the human body to enhance the feeling of weightlessness or overweight.
  • the pedal 442 moves upward to support the lower limbs of the human body, and when the weight is lost, the downward movement of the pedal 442 causes the lower limbs of the human body to lose support;
  • the vibration motor 46 is used to simulate vibration.
  • the tension sensor 63 is respectively connected to the controller 12 by wire or wirelessly, and is sent to the controller 12 for analysis and processing, and then the controller 12 issues an instruction to the hydraulic lever 32, the motor 36, the illumination lamp 221, the electric cylinder 44, and the vibration motor. 46.
  • the head mounted display 5 performs control.
  • a traction umbrella type ejection seat simulator for experiencing manned aircraft escape comprising a base, a guide rail, a power unit, a somatosensory seat, a head mounted display and a pair of control pull rings, wherein the base is mounted on the base
  • the set air pump simulates the change of the airflow when the ejection is carried out through the box body and the nozzle.
  • the guide rail is vertically arranged on the base, and the power device pushes the up, down, flipping and tilting movements of the somatosensory seat to simulate the position change of the ejection and landing, and the somatosensory seat While fixing the human body, the airbag is used to simulate the impact of weight loss and overweight on the body, and the control pull ring is used to simulate the operation of the parachute during landing. All operations are processed and transmitted to the head-mounted display; the structure is reasonable, with The utility model has the advantages of simple structure, convenient use, simple operation, low cost, safety and reliability, strong realism and high intelligence, and effectively solves the problem that the ejection seat escape training and experience cannot be performed on a real manned aircraft.

Abstract

一种用于体验载人飞行器逃生的牵引伞型弹射座椅模拟器，包括底座（1）、导轨（2）、动力装置（3）、体感座椅（4）、头戴式显示器（5）以及一对控制拉环（6），底座上设置有箱体（11）、控制器（12）以及气泵（13）；动力装置（3）包括第一支撑板（31）、液压杆（32）、导向轮组（33）、第一转轴（34）、连接板（35）、电机（36）以及齿轮组（37）；控制拉环（6）包括拉环本体（60）以及拉绳（65）；拉环本体（60）上镶嵌设置有控制按钮（61）、无线发射模块（62）、拉力传感器（63）以及缓冲弹簧（64）。该模拟器结构合理，具有结构简单、使用方便、操纵简单、造价低、安全可靠、真实感强、智能化程度高等优点，有效解决不能在真实载人飞行器上进行弹射座椅逃生训练和体验的问题。

Description

一种用于体验载人飞行器逃生的牵引伞型弹射座椅模拟器 技术领域
本发明涉及虚拟现实设备领域，尤其是涉及一种用于体验载人飞行器逃生的牵引伞型弹射座椅模拟器。
背景技术
在已知技术中，载人飞行器大都装备弹射座椅Ejection seat，弹射座椅是载人飞行器驾驶人员用的座椅，在载人飞行器遇难时依靠座椅下的动力装置将驾驶人员弹射出机舱，然后张开降落伞使驾驶人员安全降落的座椅型救生装置。
由于世界各国对载人飞行器进行严格管制，且弹射座椅使用后由于无人驾驶载人飞行器，载人飞行器随即坠毁，无论是普通人想体验弹射座椅还是对载人飞行器驾驶人员的训练都，都不可能使用真实的载人飞行器进行，而在地面单单使用弹射座椅体验从载人飞行器上弹射继而降落与从真实的载人航天器上使用弹射座椅弹射的体验是完全不同的，所以有必要发明一种在地面就能模拟弹射座椅从真实的飞行器上弹射降落的模拟装置。
发明内容
本发明要解决的技术问题是：为了克服上述中存在的问题，提供了一种用于体验载人飞行器逃生的牵引伞型弹射座椅模拟器，其结构合理，具有结构简单、操纵简单、造价低、安全可靠、真实感强、智能化程度高等优点，有效解决不能在真实载人飞行器上进行弹射座椅逃生训练和体验的问题。
本发明解决其技术问题所采用的技术方案是：一种用于体验载人飞行器逃生的牵引伞型弹射座椅模拟器，包括底座、导轨、动力装置、体感座椅、头戴式显示器以及一对控制拉环，所述的底座上设置有箱体、控制器以及气泵，所 述箱体的上盖板上设置有若干通风孔，且箱体内腔是与气泵相互连通，而气泵是与控制器相互电连接；
所述的导轨是两侧带有滑槽的工字型结构，且导轨沿滑槽行进方向竖直固定设置在底座上；
所述的动力装置包括第一支撑板、液压杆、导向轮组、第一转轴、连接板、电机以及齿轮组；所述的液压杆两端分别与底座、第一支撑板相互固定连接；所述的导向轮组是分别与固定设置在第一支撑板上的第二转轴相互转动连接，且导向轮组是与导轨上的滑槽相互抵接；
所述的电机是固定在第一支撑板上，电机主轴与齿轮组传动连接；所述第一转轴的一端是与齿轮组相互传动连接，第一转轴的另一端是穿过设置在支撑板上的轴承，并通过万向轴节与连接板相互连接；
所述的导轨上设置有若干第一磁性接近开关，所述导向轮组上设置有第一磁铁，所述的第一支撑板上设置有第二磁性接近开关，相应的在第一转轴上周向设置有若干第二磁铁；
所述的导轨顶部设置有第三支撑板，且在第三支撑板上设置有若干照明灯以及喷头，其中喷头是与气泵相互连接；
所述的控制拉环包括拉环本体以及拉绳；所述的拉绳上端是固定设置在第三支撑板上；所述的拉环本体上镶嵌设置有控制按钮、无线发射模块、拉力传感器以及缓冲弹簧，所述拉力传感器的一端是固定设置在拉环本体内腔中，拉力传感器的另一端是与拉绳的下端相互连接，并在拉力传感器与拉环本体之间设置有缓冲弹簧。
进一步地，所述的体感座椅包括与连接板相互固定连接的第二支撑板、设置在第二支撑板上的靠垫以及安全压杠；所述的靠垫上设置有扬声器；所述的安全压杠一端是与第二支撑板相互铰接，安全压杠的另一端是通过安全带与第二支撑板相互连接。
进一步地，所述的第二支撑板与靠垫之间设置有与气泵相互连接的若干气囊，所述的第二支撑板上还设置有用于束缚脚部的束缚带。
进一步地，所述的第二支撑板上固定设置有电动缸，电动缸的主轴上固定设置有搁脚的踏板。
进一步地，所述的踏板上设置有第一压力感应器。
进一步地，所述的安全压杠上设置有缓冲胶垫，且在缓冲胶垫与安全压杠之间设置有第二压力传感器。
进一步地，所述的第二压力传感器是薄片型压力传感器。
进一步地，所述的体感座椅底部设置有振动马达。
进一步地，所述的电机、照明灯、第二磁性接近开关、电动缸、第一压力感应器、第二压力传感器、振动马达、第一磁性接近开关、头戴式显示器是分别与控制器相互电连接。
进一步地，所述的第一转轴上设置有连接件以及沿第一转轴中心轴线周向设置的若干转向气缸，转向气缸的两端是分别与连接件、连接板相互铰接。
本发明的有益效果是：一种用于体验载人飞行器逃生的牵引伞型弹射座椅模拟器，包括底座、导轨、动力装置、体感座椅、头戴式显示器以及一对控制拉环，其中底座上设置的气泵通过箱体、喷头模拟弹射时的气流的变化，导轨竖直设置在底座上，动力装置推动体感座椅的上、下、翻转、倾斜运动模仿弹射和降落的体位变化，体感座椅在固定人体的同时利用气囊模拟弹射时失重和超重对身体的压迫，而控制拉环用于模拟降落时降落伞的操作，所有的操作经过处理后传送至头戴式显示器上；其结构合理，具有结构简单、使用方便、操纵简单、造价低、安全可靠、真实感强、智能化程度高等优点，有效解决不能在真实载人飞行器上进行弹射座椅逃生训练和体验的问题。
附图说明
下面结合附图和实施例对本发明进一步说明。
图1是本发明所述一种用于体验载人飞行器逃生的牵引伞型弹射座椅模拟器的整体结构示意图；
图2是本发明所述一种用于体验载人飞行器逃生的牵引伞型弹射座椅模拟器的俯视结构示意图；
图3是本发明所述一种用于体验载人飞行器逃生的牵引伞型弹射座椅模拟器的体感座椅与动力装置的连接结构示意图；
图4是本发明所述一种用于体验载人飞行器逃生的牵引伞型弹射座椅模拟器的体感座椅局部结构放大示意图；
图5是本发明所述一种用于体验载人飞行器逃生的牵引伞型弹射座椅模拟器的控制拉环结构示意图。
附图中标记分述如下：1、底座，11、箱体，111、上盖板，12、控制器，13、气泵，2、导轨，21、第一磁性接近开关，22、第三支撑板，221、照明灯，222、喷头，3、动力装置，31、第一支撑板，311、轴承，312、第二磁性接近开关，313、第二转轴，32、液压杆，33、导向轮组，331、第一磁铁，34、第一转轴，341、第二磁铁，342、万向轴节，35、连接板，36、电机，37、齿轮组，38、连接件，39、转向气缸，4、体感座椅，41、第二支撑板，42、靠垫，421、扬声器，43、气囊，44、电动缸，441、第一压力感应器，442、踏板，45、安全压杠，451、安全带，452、束缚带，46、振动马达，47、缓冲胶垫，471、第二压力传感器，5、头戴式显示器，6、控制拉环，60、拉环本体，61、控制按钮，62、无线发射模块，63、拉力传感器，64、缓冲弹簧，65、拉绳。
具体实施方式
现在结合附图对本发明作进一步详细的说明。这些附图均为简化的示意图， 仅以示意方式说明本发明的基本结构，因此其仅显示与本发明有关的构成。
如图1至5所示的一种用于体验载人飞行器逃生的牵引伞型弹射座椅模拟器，包括底座1、导轨2、动力装置3、体感座椅4、带有加速度计和陀螺仪的头戴式显示器5以及一对控制拉环6，所述的底座1上设置有箱体11、控制器12以及气泵13，所述箱体11的上盖板111上设置有若干通风孔，且箱体11内腔是与气泵13相互连通，而气泵13是与控制器12相互电连接，控制器12控制气泵13向箱体11内供气，气体经由通风孔喷出，用以模拟弹射座椅降落过程中的气流；
所述的导轨2是两侧带有滑槽的工字型结构，且导轨2沿滑槽行进方向竖直固定设置在底座1上；
所述的动力装置3包括第一支撑板31、液压杆32、导向轮组33、第一转轴34、连接板35、电机36以及齿轮组37；所述的液压杆32两端分别与底座1、第一支撑板31相互固定连接；所述的导向轮组33是分别与固定设置在第一支撑板31上的第二转轴313相互转动连接，且导向轮组33是与导轨2上的滑槽相互抵接；
所述的电机36是固定在第一支撑板31上，电机36主轴与齿轮组37传动连接；所述第一转轴34的一端是与齿轮组37相互传动连接，第一转轴34的另一端是穿过设置在支撑板上的轴承311，并通过万向轴节342与连接板35相互连接；
所述的第一转轴34上设置有连接件38以及沿第一转轴34中心轴线周向设置的若干转向气缸39，转向气缸39的两端是分别与连接件38、连接板35相互铰接。
在液压杆32与导向轮组33的共同作用下第一支撑板31、液压杆32、第一转轴34、连接板35、电机36以及齿轮组37可以沿着导轨2作上下运动，第一 转轴34在电机36的作用下带动连接板35转动，第一转轴34上设置的转向气缸39用以调整连接板35的朝向，因为连接板35直接连接体感座椅4，所以液压杆32、第一转轴34、转向气缸39间接控制体感座椅4上下运动以及倾斜运动。
所述的导轨2上设置有若干第一磁性接近开关21，所述导向轮组33上设置有第一磁铁331，所述的第一支撑板31上设置有第二磁性接近开关312，相应的在第一转轴34上周向设置有若干第二磁铁341；第一磁性接近开关21与第一磁铁331相互配合以确定导向轮组33距离地面的高度，间接得出动力装置3其他部件距离地面的距离，并将数据发送给控制器12；相似的原理，第二磁性接近开关312与第二磁铁341相互配合用以测量第一转轴34转动的角度，并将数据发送给控制器12进行数据处理。
所述的导轨2顶部设置有第三支撑板22，且在第三支撑板22上设置有若干照明灯221以及喷头222，其中喷头222是与气泵13相互连接；喷头222用于模拟弹射座椅在向上弹射时产生的向下气流。
所述的控制拉环6包括拉环本体60以及拉绳65；所述的拉绳65上端是固定设置在第三支撑板22上；所述的拉环本体60上镶嵌设置有控制按钮61、无线发射模块62、拉力传感器63以及缓冲弹簧64，所述拉力传感器63的一端是固定设置在拉环本体60内腔中，拉力传感器63的另一端是与拉绳65的下端相互连接，并在拉力传感器63与拉环本体60之间设置有缓冲弹簧64。控制拉环6的作用是模拟弹射座椅在降落过程中对降落伞操作，如拉动拉环控制降落伞的开启时间、拉动拉环控制降落伞的方向、按下控制按钮61隔断降落伞绳索等，控制拉环6内控制按钮61、拉力传感器63所产生的数据由无线发射模块62穿入控制器12进行数据处理。
所述的体感座椅4包括与连接板35相互固定连接的第二支撑板41、设置在第二支撑板41上的靠垫42以及安全压杠45；所述的靠垫42上设置有扬声器421；所述的安全压杠45一端是与第二支撑板41相互铰接，安全压杠45的另 一端是通过安全带451与第二支撑板41相互连接。
所述的第二支撑板41与靠垫42之间设置有与气泵13相互连接的若干气囊43，所述的第二支撑板41上还设置有用于束缚脚部的束缚带452；所述的第二支撑板41上固定设置有电动缸44，电动缸44的主轴上固定设置有搁脚的踏板442；所述的踏板442上设置有第一压力感应器441；所述的安全压杠45上设置有缓冲胶垫47，且在缓冲胶垫47与安全压杠45之间设置有用于检测人体上肢相对于安全压杠45的压力的第二压力传感器471，其数据传入控制器12进行数据分析；所述的第二压力传感器471是薄片型压力传感器。所述的体感座椅4底部设置有振动马达46。
所述的气囊43主要用于对失重和超重环境下座椅对人体上肢的压迫感，气囊43使用前应容纳有一定空气，当模拟弹射座椅向上弹射过程时，动力装置3先沿导轨2向上加速产生真实的超重感，同时气囊43向外排气，人体上肢下落导致相对于安全压杠45的压迫感明显减小，在动力装置3通知运动后产生持续的超重感；当模拟弹射座椅降落时动力装置3先沿导轨2向下加速产生真实的失重感，同时向气囊43内充气，当动力装置3上升到一定高度，气囊43内充有一定量气体时，由于气囊43质地较软，人体上肢所受安全压杠45的压迫感远大于其他部位，进而产生持续的失重感。电动缸44带动踏板442上下运动以对人体下肢产生或不产生支撑力来增强失重或者超重的感觉，超重时踏板442向上运动支撑人体下肢，失重时踏板442向下运动使得人体下肢失去支撑；而振动马达46用于模拟振动。
所述的头戴式显示器5上带有的传感器、第二磁性接近开关312、第一压力感应器441、第二压力传感器471、第一磁性接近开关21、控制拉环6内控制按钮61、拉力传感器63是分别与控制器12通过有线或者无线连接，传入控制器12的数据进行分析处理后由控制器12发出指令对液压杆32、电机36、照明灯221、电动缸44、振动马达46、头戴式显示器5进行控制。
本发明所述的一种用于体验载人飞行器逃生的牵引伞型弹射座椅模拟器， 包括底座、导轨、动力装置、体感座椅、头戴式显示器以及一对控制拉环，其中底座上设置的气泵通过箱体、喷头模拟弹射时的气流的变化，导轨竖直设置在底座上，动力装置推动体感座椅的上、下、翻转、倾斜运动模仿弹射和降落的体位变化，体感座椅在固定人体的同时利用气囊模拟弹射时失重和超重对身体的压迫，而控制拉环用于模拟降落时降落伞的操作，所有的操作经过处理后传送至头戴式显示器上；其结构合理，具有结构简单、使用方便、操纵简单、造价低、安全可靠、真实感强、智能化程度高等优点，有效解决不能在真实载人飞行器上进行弹射座椅逃生训练和体验的问题。
以上述依据本发明的理想实施例为启示，通过上述的说明内容，相关工作人员完全可以在不偏离本项发明技术思想的范围内，进行多样的变更以及修改。本项发明的技术性范围并不局限于说明书上的内容，必须要根据权利要求范围来确定其技术性范围。

Claims (10)

  1. 一种用于体验载人飞行器逃生的牵引伞型弹射座椅模拟器，其特征是：包括底座(1)、导轨(2)、动力装置(3)、体感座椅(4)、头戴式显示器(5)以及一对控制拉环(6)，所述的底座(1)上设置有箱体(11)、控制器(12)以及气泵(13)，所述箱体(11)的上盖板(111)上设置有若干通风孔，且箱体(11)内腔是与气泵(13)相互连通，而气泵(13)是与控制器(12)相互电连接；
    所述的导轨(2)是两侧带有滑槽的工字型结构，且导轨(2)沿滑槽行进方向竖直固定设置在底座(1)上；
    所述的动力装置(3)包括第一支撑板(31)、液压杆(32)、导向轮组(33)、第一转轴(34)、连接板(35)、电机(36)以及齿轮组(37)；所述的液压杆(32)两端分别与底座(1)、第一支撑板(31)相互固定连接；所述的导向轮组(33)是分别与固定设置在第一支撑板(31)上的第二转轴(313)相互转动连接，且导向轮组(33)是与导轨(2)上的滑槽相互抵接；
    所述的电机(36)是固定在第一支撑板(31)上，电机(36)主轴与齿轮组(37)传动连接；所述第一转轴(34)的一端是与齿轮组(37)相互传动连接，第一转轴(34)的另一端是穿过设置在支撑板上的轴承(311)，并通过万向轴节(342)与连接板(35)相互连接；
    所述的导轨(2)上设置有若干第一磁性接近开关(21)，所述导向轮组(33)上设置有第一磁铁(331)，所述的第一支撑板(31)上设置有第二磁性接近开关(312)，相应的在第一转轴(34)上周向设置有若干第二磁铁(341)；
    所述的导轨(2)顶部设置有第三支撑板(22)，且在第三支撑板(22)上设置有若干照明灯(221)以及喷头(222)，其中喷头(222)是与气泵(13)相互连接；
    所述的控制拉环(6)包括拉环本体(60)以及拉绳(65)；所述的拉绳(65)上端是固定设置在第三支撑板(22)上；所述的拉环本体(60)上镶嵌设置有控制按钮(61)、无线发射模块(62)、拉力传感器(63)以及缓冲弹簧(64)， 所述拉力传感器(63)的一端是固定设置在拉环本体(60)内腔中，拉力传感器(63)的另一端是与拉绳(65)的下端相互连接，并在拉力传感器(63)与拉环本体(60)之间设置有缓冲弹簧(64)。
  2. 根据权利要求1所述的一种用于体验载人飞行器逃生的牵引伞型弹射座椅模拟器，其特征是：所述的体感座椅(4)包括与连接板(35)相互固定连接的第二支撑板(41)、设置在第二支撑板(41)上的靠垫(42)以及安全压杠(45)；所述的靠垫(42)上设置有扬声器(421)；所述的安全压杠(45)一端是与第二支撑板(41)相互铰接，安全压杠(45)的另一端是通过安全带(451)与第二支撑板(41)相互连接。
  3. 根据权利要求2所述的一种用于体验载人飞行器逃生的牵引伞型弹射座椅模拟器，其特征是：所述的第二支撑板(41)与靠垫(42)之间设置有与气泵(13)相互连接的若干气囊(43)，所述的第二支撑板(41)上还设置有用于束缚脚部的束缚带(452)。
  4. 根据权利要求2或3所述的一种用于体验载人飞行器逃生的牵引伞型弹射座椅模拟器，其特征是：所述的第二支撑板(41)上固定设置有电动缸(44)，电动缸(44)的主轴上固定设置有搁脚的踏板(442)。
  5. 根据权利要求4所述的一种用于体验载人飞行器逃生的牵引伞型弹射座椅模拟器，其特征是：所述的踏板(442)上设置有第一压力感应器(441)。
  6. 根据权利要求2所述的一种用于体验载人飞行器逃生的牵引伞型弹射座椅模拟器，其特征是：所述的安全压杠(45)上设置有缓冲胶垫(47)，且在缓冲胶垫(47)与安全压杠(45)之间设置有第二压力传感器(471)。
  7. 根据权利要求6所述的一种用于体验载人飞行器逃生的牵引伞型弹射座椅模拟器，其特征是：所述的第二压力传感器(471)是薄片型压力传感器。
  8. 根据权利要求2所述的一种用于体验载人飞行器逃生的牵引伞型弹射座椅模拟器，其特征是：所述的体感座椅(4)底部设置有振动马达(46)。
  9. 根据权利要求7所述的一种用于体验载人飞行器逃生的牵引伞型弹射座 椅模拟器，其特征是：所述的电机(36)、照明灯(221)、第二磁性接近开关(312)、电动缸(44)、第一压力感应器(441)、第二压力传感器(471)、振动马达(46)、第一磁性接近开关(21)、头戴式显示器(5)是分别与控制器(12)相互电连接。
  10. 根据权利要求1所述的一种用于体验载人飞行器逃生的牵引伞型弹射座椅模拟器，其特征是：所述的第一转轴(34)上设置有连接件(38)以及沿第一转轴(34)中心轴线周向设置的若干转向气缸(39)，转向气缸(39)的两端是分别与连接件(38)、连接板(35)相互铰接。
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