WO2020124642A1 - 一种具有离心配重系统的虚拟现实高空飞行体验装置 - Google Patents

一种具有离心配重系统的虚拟现实高空飞行体验装置 Download PDF

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Publication number
WO2020124642A1
WO2020124642A1 PCT/CN2018/123916 CN2018123916W WO2020124642A1 WO 2020124642 A1 WO2020124642 A1 WO 2020124642A1 CN 2018123916 W CN2018123916 W CN 2018123916W WO 2020124642 A1 WO2020124642 A1 WO 2020124642A1
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Prior art keywords
steering
plate
cylinder
hydraulic cylinder
virtual reality
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PCT/CN2018/123916
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English (en)
French (fr)
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黎凯俊
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黎凯俊
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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
    • G09B9/30—Simulation of view from aircraft
    • G09B9/307—Simulation of view from aircraft by helmet-mounted projector or display
    • 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
    • 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
    • G09B9/16—Ambient or aircraft conditions simulated or indicated by instrument or alarm
    • G09B9/20—Simulation or indication of aircraft attitude

Definitions

  • the invention relates to the field of amusement facilities equipment, in particular to a virtual reality high-altitude flight experience device with a centrifugal weight system.
  • a virtual reality high-altitude flight experience device with a centrifugal weight system which has a reasonable structure, simple structure, simple operation, low cost, safe and reliable , Strong sense of reality, high intelligence, etc., effectively solve the problem of poor experience effect in the existing flight experience mode.
  • a virtual reality high-altitude flight experience device with a centrifugal counterweight system including a base, a balanced steering device, and a safety seat.
  • the base includes a bottom plate, a steering seat, and a ring Cover plate and steering rod;
  • the steering seat is a hollow structure with a bidirectional opening, the opening of the downward end of the steering seat is fixedly connected to the bottom plate, and the opening of the upward end of the steering seat is fixedly connected to the annular cover plate;
  • the steering rod has a hollow structure.
  • the lower end of the steering rod passes through the annular cover plate and is provided with a convex ring extending laterally.
  • the convex ring, the steering seat, and the annular cover plate are respectively provided with semi-circular grooves, semi-circular grooves
  • a steering motor is provided in the inner cavity of the steering rod;
  • the output shaft of the steering motor and the bottom plate are fixedly connected to each other;
  • the upper end of the steering rod is fixedly provided with a connection plate, and the connection plate is hinged with a number of A hydraulic cylinder;
  • the balanced steering device includes a cylinder composed of two arc-shaped plates.
  • the cylinder is connected to the steering rod through a first hydraulic cylinder, and two ends of the cylinder are fixedly connected to each other to provide an end cover;
  • a number of second hydraulic cylinders are provided in the axial direction of the cylinder, and the output end of the second hydraulic cylinder is connected to the counterweight through the end cover;
  • a baffle is fixedly arranged at the other end of the inner cavity of the cylinder, and the baffle and the end cover at this end are provided with bearings that are mutually connected to the rotating shaft, and a number of third hydraulic pressures are arranged radially between the rotating shaft and the baffle
  • the cylinders are connected to each other; a controller is provided in the middle of the inner cavity of the cylinder;
  • the safety seat includes a back plate, a horizontal plate, a bumper, and a VR helmet; the back plate and the rotating shaft are fixedly connected to each other, and the lower end of the back plate is connected to the horizontal plate through a connecting shaft, and the bumper is Set on the backplane.
  • the outer surface of the end of the barrel facing the steering rod is a plane
  • the first hydraulic cylinder is respectively connected to points on the plane along two axial directions and two radial directions of the barrel.
  • both ends of the third hydraulic cylinder are hinged with the rotating shaft and the baffle plate respectively, and restrict the movement of the third hydraulic cylinder along the axial direction of the cylinder.
  • the lower end of the back plate is slidably connected to the horizontal plate through a connecting shaft. After the connecting shaft passes through the horizontal plate, it is sleeved with the pressure sensor and locked and fixed by a nut.
  • the counterweight is provided with a distance sensor for detecting the distance from the end cover, and an infrared proximity sensor is provided on an end surface of the counterweight facing the moving direction of the second hydraulic cylinder.
  • a virtual reality high-altitude flight experience device with a centrifugal weight system including a base, a balanced steering device, and a safety seat.
  • the base provides support and balance for the balanced steering device and the safety seat
  • the steering device and the safety seat can rotate along the horizontal plane driven by the steering motor
  • the first hydraulic cylinder drives the balanced steering device to swing
  • the third hydraulic cylinder drives the safety seat to rotate on the vertical plane
  • the safety seat rotates in the horizontal plane
  • the counterweight set on the balance steering device can be extended and contracted to change its extended length to prevent the centrifugal phenomenon from damaging the base and overturning.
  • the preset program plays the corresponding pictures and sounds; its reasonable structure has the advantages of simple structure, convenient use, simple operation, low cost, safe and reliable, strong sense of reality, high intelligence, etc., which effectively solves the existing flight experience methods.
  • FIG. 1 is a schematic diagram of the overall structure of a virtual reality high-altitude flight experience device with a centrifugal weight system according to the present invention
  • FIG. 2 is a schematic diagram of the internal structure of the base of a virtual reality high-altitude flight experience device with a centrifugal weight system according to the present invention
  • FIG. 3 is a schematic structural view of a balance steering device of a virtual reality high-altitude flight experience device with a centrifugal weight system according to the present invention
  • FIG. 4 is a schematic diagram of a connection structure of a cylinder and a base of a virtual reality high-altitude flight experience device with a centrifugal weight system according to the present invention
  • FIG. 5 is a schematic structural view of a rotating shaft and a third hydraulic cylinder of a virtual reality high-altitude flight experience device with a centrifugal weight system according to the present invention
  • FIG. 6 is a schematic diagram of a connection structure of a back plate and a horizontal plate of a virtual reality high-altitude flight experience device with a centrifugal weight system according to the present invention.
  • Base 11, bottom plate, 12, steering seat, 13, ring cover, 14, steering rod, 141, convex ring, 15, ball, 16, steering motor, 17, connecting plate, 18, first hydraulic cylinder, 2.
  • Balance steering device 20, barrel, 21, curved plate, 22, end cover, 23, counterweight, 231, distance sensor, 232, infrared proximity sensor, 24, second hydraulic cylinder, 25, controller , 26, baffle, 27, bearing, 28, rotating shaft, 29, third hydraulic cylinder, 3, safety seat, 31, back plate, 311, connecting shaft, 312, pressure sensor, 32, cross plate, 33, insurance Bar, 34, VR helmet.
  • a virtual reality high-altitude flight experience device with a centrifugal weight system includes a base 1, a balance steering device 2, and a safety seat 3.
  • the base includes a bottom plate 11, a steering seat 12, an annular cover 13, and a steering rod 14;
  • the steering seat 12 is a hollow with a bidirectional opening in the vertical direction Structure, the opening of the downward end of the steering seat 12 is fixedly connected to the bottom plate 11, and the opening of the upward end of the steering seat 12 is fixedly connected to the annular cover 13;
  • the steering rod 14 has a hollow structure.
  • the lower end of the steering rod 14 passes through a circular hole in the middle of the annular cover 13 and is provided with a convex ring 141 extending laterally.
  • the convex ring 141 and the steering rod 14 are integral Structure, in another embodiment, the convex ring 141 is made of a ring welded with the steering rod 14; the steering rod 14 is in clearance fit with the annular cover 13;
  • the convex ring 141, the steering seat 12, and the annular cover 13 are respectively provided with semicircular grooves (not shown in the figure), and the semicircular grooves are provided with balls 15, that is, the convex ring 141 has two upper and lower sides
  • the end surface and the bottom surface of the inner cavity of the steering seat 12 and the lower end surface of the annular cover 13 facing the two end surfaces in the vertical direction are respectively provided with semicircular grooves, the semicircular groove on the upper end surface of the convex ring 141 and the annular cover
  • the semicircular groove on the lower end surface of the plate 13 is aligned and the balls 15 are arranged between the two.
  • the semicircular groove on the lower end surface of the convex ring 141 is aligned with the semicircular groove on the bottom surface of the inner cavity of the steering seat 12
  • the ball 15 is arranged between the two; the annular side surface of the convex ring 141 and the inner cavity wall surface of the steering seat 12 are in clearance fit with each other;
  • a steering motor 16 is provided in the inner cavity of the steering rod 14.
  • the output shaft of the steering motor 16 and the bottom plate 11 are fixedly connected to each other; the upper end of the steering rod 14 is fixedly provided with a connecting plate 17, and the connecting plate 17 is hingedly provided with Several first hydraulic cylinders 18.
  • the balanced steering device 2 includes a cylinder 20 composed of two arc-shaped plates 21 connected to the steering rod 14 through a first hydraulic cylinder 18 Connected to each other, the two ends of the cylinder 20 are fixedly connected with end caps 22; one end of the inner cavity of the cylinder 20 is fixedly provided with a number of second hydraulic cylinders 24 along the axis of the cylinder 20, and the output end of the second hydraulic cylinder 24 Through the end cover 22 and the weight block 23 are connected to each other, the non-output end of the second hydraulic cylinder 24 is fixedly disposed in the inner cavity of the barrel 20;
  • a baffle 26 is fixedly arranged at the other end of the inner cavity of the barrel 20, and the baffle 26 and the end cover 22 at this end are provided with bearings 27 which are rotationally connected to the rotating shaft 28, that is, one end of the rotating shaft 28 is connected to the bearing 27, The other end of the rotating shaft 28 extends out of the cylinder 20; the rotating shaft 28 and the baffle 26 are connected to each other by a number of third hydraulic cylinders 29 that are radially arranged along the axis of the rotating shaft 28 and centered in the radial direction of the rotating shaft; A controller 25 is provided in the middle of the inner cavity of the cylinder 20.
  • the first hydraulic cylinder 18, the second hydraulic cylinder 24, and the third hydraulic cylinder 29 are connected to the equipment for controlling the output of the hydraulic cylinder, such as the hydraulic pump provided in the barrel 20, and the related equipment is connected to the controller 25 And controlled by it.
  • the safety seat 3 includes a back plate 31, a cross plate 32, a bumper 33, and a VR helmet 34; the back plate 31 and the rotating shaft 28 are fixedly connected to each other, and the back plate 31 The lower end of the is connected to the cross plate 32 through the connecting shaft 311, and the bumper 33 is provided on the back plate 31.
  • the VR helmet 34 should be equipped with a motion sensor for detecting the position of the human body, specifically detecting the motion of the human head, in combination with the safety seat 3 detected by the motion sensor installed on the back plate 31 and integrated on the controller 25 In the position, the VR helmet 34 can obtain and play the screen and sound of the user's viewing position from the controller 25.
  • the outer surface of the barrel 20 facing the end of the steering rod 14 is a plane, and the first hydraulic cylinder 18 and the plane are along the two axial directions of the barrel 20 and The two points in the radial direction are connected to control the rocking motion of the cylinder 20 in the front, back, left, and right directions (that is, in the axial and radial directions of the cylinder 20, respectively).
  • the two ends of the third hydraulic cylinder 29 are hinged with the rotating shaft 28 and the baffle 26 respectively, and restrict the movement of the third hydraulic cylinder 29 along the axial direction of the cylinder 20
  • the telescopic movement of the third hydraulic cylinder 29 drives the rotation of the rotating shaft 28.
  • the central axis of the third hydraulic cylinder 29 should be connected to the rotating shaft 28 Avoid the intersection of the central axis of the axis, and avoid staying at the position where the intersection will occur during the rotation of the rotating shaft 28, and the judgment of this position is a combination of the rotation angle of the safety seat 3 detected by the motion sensor provided on the back plate 31
  • the number of installations, dimensions and other parameters are calculated by the preset program in the controller 25.
  • the center axis of the third hydraulic cylinder 29 shown in FIG. 5 is located above the central axis of the rotating shaft 28.
  • the third hydraulic cylinder 29 is directly extended, and when the rotating shaft 28 needs to rotate counterclockwise, the third hydraulic cylinder is contracted. 29.
  • the third hydraulic cylinder can be extended by using the inertia of the rotation to pass the position point, and then the rotating shaft 28 can be rotated counterclockwise.
  • the lower end of the back plate 31 is slidably connected to the horizontal plate 32 through the connecting shaft 311 (that is, the connecting shaft 311 and the connecting hole on the horizontal plate 32 are clearance fit), the connecting shaft After passing through the cross plate 32, 311 is sleeved with the pressure sensor 312 and fixed by a nut, and the pressure value acting on it is measured by the pressure sensor 312. Since it is not measured directly under the human body, the body weight of the human body needs to be obtained by conversion .
  • the weight block 23 is provided with a distance sensor 231 for detecting the distance from the end cover 22. Since the weight of the weight block 23 is fixed, by measuring the outside The extended distance combined with the human body weight data can balance the weight of the two ends of the balance steering device 2 to prevent overturning. At the same time, the expansion and contraction of the weight 23 can provide a boost for the first hydraulic cylinder 18 to control the balance steering device 2 to swing axially along the barrel 20; An infrared proximity sensor 232 is provided on the end surface of the weight block 23 facing the moving direction of the second hydraulic cylinder 24 to prevent the weight block 23 from colliding when extending.
  • a virtual reality high-altitude flight experience device with a centrifugal weight system includes a base, a balanced steering device, and a safety seat.
  • the base provides support for the balanced steering device and the safety seat, and at the same time, the balanced steering device 1.
  • the safety seat can rotate along the horizontal plane driven by the steering motor, the first hydraulic cylinder drives the balance steering device to swing, the third hydraulic cylinder drives the safety seat to rotate on the vertical plane, and the safety seat combines pressure during the horizontal plane rotation
  • the weight data of the human body detected by the sensor, the counterweight set on the balance steering device can be extended and contracted to change its extended length to prevent the centrifugal phenomenon from causing damage to the base and overturning.
  • the program plays the corresponding pictures and sounds; its structure is reasonable, with the advantages of simple structure, convenient use, simple operation, low cost, safe and reliable, strong sense of reality, high intelligence, etc., and effectively solve the experience effect of existing flight experience methods Bad question.

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Abstract

一种具有离心配重系统的虚拟现实高空飞行体验装置，包括底座(1)、平衡转向装置(2)、安全座椅(3)，底座(1)包括底板(11)、转向座(12)、环形盖板(13)、转向杆(14)；平衡转向装置(2)包括由两块弧形板(21)组成的筒体(20)、端盖(22)、第二液压缸(24)、配重块(23)、挡板(26)、轴承(27)、转轴(28)、第三液压缸(29)、控制器(25)；安全座椅(3)包括背板(31)、横板(32)、保险杠(33)以及VR头盔(34)。本体验装置结构合理，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，有效解决现有飞行体验方式存在的体验效果不佳的问题。

Description

一种具有离心配重系统的虚拟现实高空飞行体验装置 技术领域
本发明涉及游乐设施设备领域，尤其是涉及一种具有离心配重系统的虚拟现实高空飞行体验装置。
背景技术
在已知技术中，驾驶航天器或者航空器是实现人类飞行的两种重要手段，但驾驶航空航天器需要具备良好的生理和心理素质，显然并不是所有人都具备这种要求，此外驾驶航空航天器还需经过艰苦、严格的训练，而在航空航天器驾驶训练以及实际驾驶中危险系数过高极易发生危险，即使满足了以上所有需求，航天器和航空器造价昂贵且国家对其实行管制，大部分人只能通过乘坐飞机或者从游戏中体验飞行，而乘坐飞机和游戏产生的飞行体验显然有很大的局限性，所以有必要设计一种操纵简单、安全可靠、体验真实且大部分人群可以参与的飞行体验装置。
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，提供了一种具有离心配重系统的虚拟现实高空飞行体验装置，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，有效解决现有飞行体验方式存在的体验效果不佳的问题。
本发明解决其技术问题所采用的技术方案是：一种具有离心配重系统的虚拟现实高空飞行体验装置，包括底座、平衡转向装置、安全座椅，所述的底座包括底板、转向座、环形盖板、转向杆；所述的转向座是具有双向开口的中空结构，转向座朝下一端的开口与底板相互固定连接，转向座朝上一端的开口与环形盖板相互固定连接；
所述的转向杆具有中空结构，转向杆的下端穿过环形盖板并横向延伸设置有凸环，凸环、转向座、环形盖板上分别设有半圆形凹槽，半圆形凹槽上设有滚珠；所述的转向杆内腔中设有转向电机，转向电机的输出轴与底板相互固定连接；所述的转向杆的上端固定设置有连接板，连接板上铰接设置有若干第一液压缸；
所述的平衡转向装置包括由两块弧形板组成的筒体，筒体通过第一液压缸与转向杆相互连接，筒体两端分别固定连接设置端盖；所述筒体内腔的一端沿筒体的轴线方向设有若干第二液压缸，第二液压缸的输出端穿过端盖与配重块相互连接；
所述筒体内腔的另一端固定设置有挡板，挡板以及该端的端盖上设有与转轴相互转动连接的轴承，所述的转轴、挡板之间通过若干呈放射状设置的第三液压缸相互连接；所述筒体内腔的中部设有控制器；
所述的安全座椅包括背板、横板、保险杠以及VR头盔；所述的背板与转轴相互固定连接，且背板的下端通过连接轴与横板相互连接，所述的保险杠是设置在背板上。
进一步地，所述筒体朝向转向杆一端的外表面是平面，第一液压缸分别与该平面上沿筒体的两个轴向方向以及两个径向方向上的点连接。
进一步地，所述第三液压缸的两端是分别与转轴、挡板相互铰接，且限制第三液压缸沿筒体轴向的运动。
进一步地，所述背板的下端通过连接轴与横板相互滑动连接，连接轴穿过横板后与压力传感器套接并通过螺母锁紧固定。
进一步地，所述的配重块上设有检测其与端盖距离的距离传感器，并在配重块朝向第二液压缸的运动方向的端面上设有红外接近传感器。
本发明的有益效果是：一种具有离心配重系统的虚拟现实高空飞行体验装置，包括底座、平衡转向装置、安全座椅，所述的底座为平衡转向装置、安全 座椅提供支撑，同时平衡转向装置、安全座椅可在转向电机的带动下沿水平面转动，第一液压缸带动平衡转向装置摆动，第三液压缸带动安全座椅在垂直面上转动，且安全座椅在水平面转动过程中结合压力传感器检测到的人体体重数据，平衡转向装置上设置的配重块可伸缩改变其外伸的长度以防止离心现象对底座造成损害而倾覆，VR头盔通过检测使用者的体位同时配合控制器预设的程序播放相应的画面和声音；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，有效解决现有飞行体验方式存在的体验效果不佳的问题。
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是本发明所述一种具有离心配重系统的虚拟现实高空飞行体验装置的整体结构示意图；
图2是本发明所述一种具有离心配重系统的虚拟现实高空飞行体验装置的底座内部结构示意图；
图3是本发明所述一种具有离心配重系统的虚拟现实高空飞行体验装置的平衡转向装置结构示意图；
图4是本发明所述一种具有离心配重系统的虚拟现实高空飞行体验装置的筒体与底座连接结构示意图；
图5是本发明所述一种具有离心配重系统的虚拟现实高空飞行体验装置的转轴与第三液压缸结构示意图；
图6是本发明所述一种具有离心配重系统的虚拟现实高空飞行体验装置的背板与横板连接结构示意图。
附图中标记分述如下：
1、底座，11、底板，12、转向座，13、环形盖板，14、转向杆，141、凸环，15、滚珠，16、转向电机，17、连接板，18、第一液压缸，2、平衡转向装置，20、筒体，21、弧形板，22、端盖，23、配重块，231、距离传感器，232、红外接近传感器，24、第二液压缸，25、控制器，26、挡板，27、轴承，28、转轴，29、第三液压缸，3、安全座椅，31、背板，311、连接轴，312、压力传感器，32、横板，33、保险杠，34、VR头盔。
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所示的一种具有离心配重系统的虚拟现实高空飞行体验装置，包括底座1、平衡转向装置2、安全座椅3。
如图1、图2、图4所示，所述的底座包括底板11、转向座12、环形盖板13、转向杆14；所述的转向座12是在竖直方向上具有双向开口的中空结构，转向座12朝下一端的开口与底板11相互固定连接，转向座12朝上一端的开口与环形盖板13相互固定连接；
所述的转向杆14具有中空结构，转向杆14的下端穿过环形盖板13中部的圆孔并横向延伸设置有凸环141，在一种实施例中凸环141与转向杆14是一体式结构，在另一种实施例中凸环141由圆环与转向杆14焊接制成；所述的转向杆14与环形盖板13间隙配合；
所述的凸环141、转向座12、环形盖板13上分别设有半圆形凹槽(图中未示出)，半圆形凹槽上设有滚珠15，即凸环141上下两个端面以及两个端面竖直方向上所对的转向座12内腔底面、环形盖板13下端面上分别设有半圆形凹槽，凸环141上端面上的半圆形凹槽与环形盖板13下端面上的半圆形凹槽对正并在 两者之间设置滚珠15，凸环141下端面上的半圆形凹槽与转向座12内腔底面上的半圆形凹槽对正并在两者之间设置滚珠15；所述的凸环141环形侧面与转向座12内腔壁面相互间隙配合；
所述的转向杆14内腔中设有转向电机16，转向电机16的输出轴与底板11相互固定连接；所述的转向杆14的上端固定设置有连接板17，连接板17上铰接设置有若干第一液压缸18。
如图1、图3、图4、图5所示，所述的平衡转向装置2包括由两块弧形板21连接组成的筒体20，筒体20通过第一液压缸18与转向杆14相互连接，筒体20两端分别固定连接设置端盖22；所述筒体20内腔的一端沿筒体20的轴线方向固定设置有若干第二液压缸24，第二液压缸24的输出端穿过端盖22与配重块23相互连接，第二液压缸24的非输出端则固定设置在筒体20的内腔中；
所述筒体20内腔的另一端固定设置有挡板26，挡板26以及该端的端盖22上设有与转轴28相互转动连接的轴承27，即转轴28的一端与轴承27相互连接，转轴28的另一端则伸出筒体20；所述的转轴28、挡板26之间通过若干以转轴28轴线为中心，沿转轴径向呈放射状设置的若干第三液压缸29相互连接；所述筒体20内腔的中部设有控制器25。
所述的第一液压缸18、第二液压缸24和第三液压缸29是分别与设置在筒体20中的液压泵等控制液压缸输出的设备相互连接，且相关设备与控制器25连接并受其控制。
如图1、图6所示，所述的安全座椅3包括背板31、横板32、保险杠33以及VR头盔34；所述的背板31与转轴28相互固定连接，且背板31的下端通过连接轴311与横板32相互连接，所述的保险杠33是设置在背板31上。VR头盔34上应安装有运动传感器用于检测人体体位，具体的是检测人体头部的运动， 结合安装在背板31以及集成在控制器25上的运动传感器所检测到的安全座椅3目前所处的位置，VR头盔34便可从控制器25中得到并播放使用者观看位置的画面以及声音。
在如图4所示的一种实施例中，所述筒体20朝向转向杆14一端的外表面是平面，第一液压缸18分别与该平面上沿筒体20的两个轴向方向以及两个径向方向上的点连接，以此控制筒体20前后左右的摇摆动作(即分别沿筒体20轴向和径向方向上的摆动)。
在如图5所示的一种实施例中，所述第三液压缸29的两端是分别与转轴28、挡板26相互铰接，且限制第三液压缸29沿筒体20轴向的运动，通过第三液压缸29的伸缩运动带动转轴28的转动，为了避免第三液压缸29无法转动转轴28，第三液压缸29与转轴28连接时第三液压缸29的中轴线应与转轴28的中心轴线避免有交点，在转轴28转动过程中也避免在将有交点的位置停留，而这个位置的判断由设置在背板31上的运动传感器所检测到的安全座椅3旋转角度结合部件的安装数量、尺寸等参数由控制器25中的预设程序计算得出。
如图5所示的第三液压缸29的中轴线位于转轴28的中心轴线上方，转轴28需要顺时针转动时直接伸长第三液压缸29，转轴28需要逆时针转动时收缩第三液压缸29，当转动到存在交点的位置时利用转动的惯性通过该位置点后伸长第三液压缸即可继续逆时针转动转轴28。
在如图6所示的一种实施例中，所述背板31的下端通过连接轴311与横板32相互滑动连接(即接轴311与横板32上的连接孔间隙配合)，连接轴311穿过横板32后与压力传感器312套接并通过螺母锁紧固定，通过压力传感器312测量作用于其上的压力值，由于不是直接在人体下方测量获得所以需要通过换算得出人体的体重。
在如图1所示的一种实施例中，所述的配重块23上设有检测其与端盖22距离的距离传感器231，由于配重块23的重量是固定的，通过测量其外伸的距离结合人体体重数据即可平衡平衡转向装置2两端的重量，防止倾覆，同时配重块23的伸缩可以为第一液压缸18控制平衡转向装置2沿筒体20轴向摆动提供助力；在配重块23朝向第二液压缸24的运动方向的端面上设有红外接近传感器232，防止配重块23外伸时发生碰撞。
本发明所述的一种具有离心配重系统的虚拟现实高空飞行体验装置，包括底座、平衡转向装置、安全座椅，所述的底座为平衡转向装置、安全座椅提供支撑，同时平衡转向装置、安全座椅可在转向电机的带动下沿水平面转动，第一液压缸带动平衡转向装置摆动，第三液压缸带动安全座椅在垂直面上转动，且安全座椅在水平面转动过程中结合压力传感器检测到的人体体重数据，平衡转向装置上设置的配重块可伸缩改变其外伸的长度以防止离心现象对底座造成损害而倾覆，VR头盔通过检测使用者的体位同时配合控制器预设的程序播放相应的画面和声音；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，有效解决现有飞行体验方式存在的体验效果不佳的问题。
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 (5)

  1. 一种具有离心配重系统的虚拟现实高空飞行体验装置，其特征是：包括底座(1)、平衡转向装置(2)、安全座椅(3)，所述的底座(1)包括底板(11)、转向座(12)、环形盖板(13)、转向杆(14)；所述的转向座(12)是具有双向开口的中空结构，转向座(12)朝下一端的开口与底板(11)相互固定连接，转向座(12)朝上一端的开口与环形盖板(13)相互固定连接；
    所述的转向杆(14)具有中空结构，转向杆(14)的下端穿过环形盖板(13)并横向延伸设置有凸环(141)，凸环(141)、转向座(12)、环形盖板(13)上分别设有半圆形凹槽，半圆形凹槽上设有滚珠(15)；所述的转向杆(14)内腔中设有转向电机(16)，转向电机(16)的输出轴与底板(11)相互固定连接；所述的转向杆(14)的上端固定设置有连接板(17)，连接板(17)上铰接设置有若干第一液压缸(18)；
    所述的平衡转向装置(2)包括由两块弧形板(21)组成的筒体(20)，筒体(20)通过第一液压缸(18)与转向杆(14)相互连接，筒体(20)两端分别固定连接设置端盖(22)；所述筒体(20)内腔的一端沿筒体(20)的轴线方向设有若干第二液压缸(24)，第二液压缸(24)的输出端穿过端盖(22)与配重块(23)相互连接；
    所述筒体(20)内腔的另一端固定设置有挡板(26)，挡板(26)以及该端的端盖(22)上设有与转轴(28)相互转动连接的轴承(27)，所述的转轴(28)、挡板(26)之间通过若干呈放射状设置的第三液压缸(29)相互连接；所述筒体(20)内腔的中部设有控制器(25)；
    所述的安全座椅(3)包括背板(31)、横板(32)、保险杠(33)以及VR头盔(34)；所述的背板(31)与转轴(28)相互固定连接，且背板(31)的下端通过连接轴(311)与横板(32)相互连接，所述的保险杠(33)是设置在背 板(31)上。
  2. 根据权利要求1所述的一种具有离心配重系统的虚拟现实高空飞行体验装置，其特征是：所述筒体(20)朝向转向杆(14)一端的外表面是平面，第一液压缸(18)分别与该平面上沿筒体(20)的两个轴向方向以及两个径向方向上的点连接。
  3. 根据权利要求1所述的一种具有离心配重系统的虚拟现实高空飞行体验装置，其特征是：所述第三液压缸(29)的两端是分别与转轴(28)、挡板(26)相互铰接，且限制第三液压缸(29)沿筒体(20)轴向的运动。
  4. 根据权利要求1所述的一种具有离心配重系统的虚拟现实高空飞行体验装置，其特征是：所述背板(31)的下端通过连接轴(311)与横板(32)相互滑动连接，连接轴(311)穿过横板(32)后与压力传感器(312)套接并通过螺母锁紧固定。
  5. 根据权利要求1所述的一种具有离心配重系统的虚拟现实高空飞行体验装置，其特征是：所述的配重块(23)上设有检测其与端盖(22)距离的距离传感器(231)，并在配重块(23)朝向第二液压缸(24)的运动方向的端面上设有红外接近传感器(232)。
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