CN105374255A - Emergency forced landing interactive simulation device - Google Patents

Emergency forced landing interactive simulation device Download PDF

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Publication number
CN105374255A
CN105374255A CN201510809479.8A CN201510809479A CN105374255A CN 105374255 A CN105374255 A CN 105374255A CN 201510809479 A CN201510809479 A CN 201510809479A CN 105374255 A CN105374255 A CN 105374255A
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CN
China
Prior art keywords
aircraft
scene
simulation
motion platform
interactive
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Pending
Application number
CN201510809479.8A
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Chinese (zh)
Inventor
田地
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
HEFEI JINNUO DIGITAL TECHNOLOGY Co Ltd
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HEFEI JINNUO DIGITAL TECHNOLOGY Co Ltd
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Application filed by HEFEI JINNUO DIGITAL TECHNOLOGY Co Ltd filed Critical HEFEI JINNUO DIGITAL TECHNOLOGY Co Ltd
Priority to CN201510809479.8A priority Critical patent/CN105374255A/en
Publication of CN105374255A publication Critical patent/CN105374255A/en
Pending legal-status Critical Current

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    • GPHYSICS
    • G09EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
    • G09BEDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
    • G09B9/00Simulators for teaching or training purposes
    • G09B9/02Simulators for teaching or training purposes for teaching control of vehicles or other craft
    • G09B9/08Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of aircraft, e.g. Link trainer
    • G09B9/16Ambient or aircraft conditions simulated or indicated by instrument or alarm
    • GPHYSICS
    • G09EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
    • G09BEDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
    • G09B9/00Simulators for teaching or training purposes
    • G09B9/02Simulators for teaching or training purposes for teaching control of vehicles or other craft
    • G09B9/08Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of aircraft, e.g. Link trainer
    • G09B9/30Simulation of view from aircraft
    • G09B9/32Simulation of view from aircraft by projected image

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  • Engineering & Computer Science (AREA)
  • Theoretical Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Business, Economics & Management (AREA)
  • Physics & Mathematics (AREA)
  • Educational Administration (AREA)
  • Educational Technology (AREA)
  • General Physics & Mathematics (AREA)
  • Projection Apparatus (AREA)
  • Toys (AREA)

Abstract

The invention discloses an emergency forced landing interactive simulation device. The emergency forced landing interactive simulation device comprises a simulation cabin, a six-degree-of-freedom hydraulic motion platform installed at the bottom of the simulation cabin, an operation display mechanism which is arranged in the simulation cabin and is located at a cockpit, a vibration device which is arranged at the bottom of a seat in the simulation cabin, display equipment and audio equipment which are arranged in the simulation cabin, and a main control machine; and the six-degree-of-freedom hydraulic motion platform, the operation display mechanism, the vibration device, the display equipment and the audio equipment are respectively connected with the main control machine. According to the emergency forced landing interactive simulation device of the invention, the six-degree-of-freedom hydraulic motion platform and the vibration device are adopted to simulate the moving state of the flight of an aircraft; the display equipment displays the video of the operating state of the aircraft and a scene corresponding to the flight of the aircraft; the audio equipment emits sound effects under different flight states of the aircraft; and the simulation device, animation scenes and vivid sound effects are integrated, so that interactive personnel can personally experience a complete process from the takeoff of the aircraft to the emergency forced landing of the aircraft, and experience immersion feelings can be enriched.

Description

A kind of emergency landing interactive simulation device
Technical field
The present invention relates to human-computer interaction system field, specifically a kind of emergency landing interactive simulation device.
Background technology
Traditional analog emergency landing interactive experience device only adopts Building environment to simulate in conjunction with shadow casting technique, the airframe models of console mode is set, by arranging LCDs at the window place of cabin pilothouse and passenger accommodation, the picture of simulated altitude flight, sensation during experience emergency landing from high-altitude to ground.The experience sense of this complete equipment is poor, only has visual experience sense, does not possess the Flow experience sense of true forced landing.In addition, conventional emergency forced landing interactive experience device, does not limit experience number, the engine room structure of complete open type, easily be subject to the interference of external environment, and the later maintenance cost of equipment is increased, be only difficult to the feeling of stress making spectators' own experience to emergency landing by simple image technology.
Summary of the invention
The technical problem to be solved in the present invention is to provide a kind of emergency landing interactive simulation device, analogue means, cartoon scene, audio triplicity true to nature, solves the problem that existing simulation emergency landing immersion experience sense is not strong.
Technical scheme of the present invention is:
A kind of emergency landing interactive simulation device, include simulation cabin, be installed on the six-freedom hydraulic motion platform in analog machine bilge portion, be arranged at be positioned at driving cabin position in simulation cabin operation indication mechanism, be arranged at the vibrating device bottom simulation cabin inner seat chair, the display device being arranged at simulation cabin and stereo set, and master controller; Described six-freedom hydraulic motion platform, operation indication mechanism, vibrating device, display device, stereo set are all connected with master controller; Described display device includes hyperchannel ring curtain projection system and is arranged at simulates nacelle interior wall and the display screen being positioned at seat side; Described stereo set be arranged on hyperchannel ring curtain projection system both sides and just to seat position around stereo system; The storer that described master controller includes central processing unit, be connected respectively with central processing unit and driving mechanism, described driving mechanism is connected with six-freedom hydraulic motion platform, vibrating device.
Described six-freedom hydraulic motion platform include upper mounting plate, lower platform, six be installed on upper universal coupling on upper mounting plate lower surface, six be installed on lower universal coupling on lower platform upper surface and six hydraulic jacks be connected between universal coupling and lower universal coupling, described hydraulic jack is connected with driving mechanism.
Projecting video images and display screen video image is stored in described storer, projecting video images include take off, aircraft smooth flight, aircraft encounter thunderbolt, aircraft spirals, airplane nose down, aircraft landing and aircraft come to a complete stop video image, display screen video image includes scene of taking off, aerial scene, thunderbolt scene, black clouds scene, underriding scene, ground fast moving scenes and ground static scene, the aircraft state video image one_to_one corresponding that the scene video image shown in described display screen and hyperchannel ring curtain projection system show.
Described operation indication mechanism includes action button, pilot lamp and instrument, and described action button is connected with central processing unit by 232 interfaces, and described display screen is connected with central processing unit by USB interface.
Described hyperchannel ring curtain projection system, stereo set are connected with central processing unit by WiFi wireless routing.
Advantage of the present invention:
The present invention adopts the motion state of six-freedom hydraulic motion platform and the flight of vibrating device simulated aircraft, the video of display device display aircraft running status and scene corresponding to aircraft flight, stereo set sends the audio under aircraft different flight state, by analogue means, cartoon scene, audio triplicity true to nature, make interactive personnel can own experience to aircraft from fly to the complete procedure of emergency landing, make experience feeling of immersion substantial.Six-freedom hydraulic motion platform of the present invention can simulated aircraft flight time pitching, driftage, rolling, lifting, vertical and horizontal translation various states, make flight experience effect true, interactive interesting strong; The present invention is provided with seat vibration arrangement, coordinates control with six-freedom hydraulic motion platform, further increases the actual experience sense of flight effect; Master controller of the present invention adopts WiFi network to communicate to connect, and ensures that analogue means, cartoon scene, audio three linkage true to nature are unified, there will not be the problem of interlock effect error.
Accompanying drawing explanation
Fig. 1 is theory diagram of the present invention.
Fig. 2 is the structural representation of six-freedom hydraulic motion platform of the present invention.
Embodiment
See Fig. 1, a kind of emergency landing interactive simulation device, include simulation cabin, be installed on the six-freedom hydraulic motion platform 2 in analog machine bilge portion, be arranged at be positioned at driving cabin position in simulation cabin operation indication mechanism 3, be arranged at the vibrating device 3 bottom simulation cabin inner seat chair, the display device 4 being arranged at simulation cabin and stereo set 5, and master controller 1; Six-freedom hydraulic motion platform 2, operation indication mechanism 3, vibrating device 4, display device 5, stereo set 6 are all connected with master controller 1; Operation indication mechanism 3 includes action button 31, pilot lamp 32 and instrument 33; Display device 5 includes hyperchannel ring curtain projection system 51 and is arranged at simulates nacelle interior wall and the display screen 52 being positioned at seat side; Stereo set 6 for be arranged on hyperchannel ring curtain projection system both sides and just to seat position around stereo system; The storer 12 that master controller 1 includes central processing unit 11, be connected respectively with central processing unit 11 and driving mechanism 13, driving mechanism 13 is connected with six-freedom hydraulic motion platform 2, vibrating device 4, action button 31 is connected with central processing unit 11 by 232 interfaces, display screen 52 is connected with central processing unit 11 by USB interface, and hyperchannel ring curtain projection system 51, stereo set 6 are connected with central processing unit 11 by WiFi wireless routing.
Wherein, see Fig. 2, six-freedom hydraulic motion platform 3 includes upper mounting plate 31, lower platform 32, six the upper universal coupling 33, six be installed on upper mounting plate 31 lower surface is installed on lower universal coupling 34 on lower platform 32 upper surface and six hydraulic jacks 35 be connected between universal coupling 33 and lower universal coupling 34, and hydraulic jack 35 is connected with driving mechanism 13; Projecting video images and display screen video image is stored in storer 12, projecting video images include take off, aircraft smooth flight, aircraft encounter thunderbolt, aircraft spirals, airplane nose down, aircraft landing and aircraft come to a complete stop video image, display screen video image includes scene of taking off, aerial scene, thunderbolt scene, black clouds scene, underriding scene, ground fast moving scenes and ground static scene, the aircraft state video image one_to_one corresponding that the scene video image of display in display screen 52 and hyperchannel ring curtain projection system 51 show.
Principle of work of the present invention:
First passenger to enter in simulation cabin also seat on seat, then operating personnel press start key, picture is taken off in the display of hyperchannel ring curtain projection system 51, display screen 52 shows scene of taking off, master controller 1 controls driving mechanism 13, driving mechanism 13 controls six-freedom hydraulic motion platform 2 and vibrating device 4 and combines and realize aircraft layback operation, then hyperchannel ring curtain projection system 51 shows aircraft smooth flight more successively, aircraft encounter is struck by lightning, aircraft spirals, airplane nose down, the video image that aircraft landing and aircraft come to a complete stop, corresponding display screen shows aerial scene, thunderbolt scene, black clouds scene, underriding scene, ground fast moving scenes and ground static scene, corresponding six-freedom hydraulic motion platform 2 and vibrating device 4 are combined and are realized aircraft smooth flight, air craft battery, aircraft continues to jolt, bow before aircraft, aircraft jolts again, the state of aircraft stable landing, thus realize aircraft from fly to the complete procedure of emergency landing.

Claims (5)

1. an emergency landing interactive simulation device, it is characterized in that: include simulation cabin, be installed on the six-freedom hydraulic motion platform in analog machine bilge portion, be arranged at be positioned at driving cabin position in simulation cabin operation indication mechanism, be arranged at the vibrating device bottom simulation cabin inner seat chair, the display device being arranged at simulation cabin and stereo set, and master controller; Described six-freedom hydraulic motion platform, operation indication mechanism, vibrating device, display device, stereo set are all connected with master controller; Described display device includes hyperchannel ring curtain projection system and is arranged at simulates nacelle interior wall and the display screen being positioned at seat side; Described stereo set be arranged on hyperchannel ring curtain projection system both sides and just to seat position around stereo system; The storer that described master controller includes central processing unit, be connected respectively with central processing unit and driving mechanism, described driving mechanism is connected with six-freedom hydraulic motion platform, vibrating device.
2. a kind of emergency landing interactive simulation device according to claim 1, it is characterized in that: described six-freedom hydraulic motion platform include upper mounting plate, lower platform, six be installed on upper universal coupling on upper mounting plate lower surface, six be installed on lower universal coupling on lower platform upper surface and six hydraulic jacks be connected between universal coupling and lower universal coupling, described hydraulic jack is connected with driving mechanism.
3. a kind of emergency landing interactive simulation device according to claim 1, it is characterized in that: in described storer, store projecting video images and display screen video image, projecting video images includes to be taken off, aircraft smooth flight, aircraft encounter is struck by lightning, aircraft spirals, airplane nose down, the video image that aircraft landing and aircraft come to a complete stop, display screen video image includes scene of taking off, aerial scene, thunderbolt scene, black clouds scene, underriding scene, ground fast moving scenes and ground static scene, the aircraft state video image one_to_one corresponding that the scene video image shown in described display screen and hyperchannel ring curtain projection system show.
4. a kind of emergency landing interactive simulation device according to claim 1, it is characterized in that: described operation indication mechanism includes action button, pilot lamp and instrument, described action button is connected with central processing unit by 232 interfaces, and described display screen is connected with central processing unit by USB interface.
5. a kind of emergency landing interactive simulation device according to claim 1, is characterized in that: described hyperchannel ring curtain projection system, stereo set are connected with central processing unit by WiFi wireless routing.
CN201510809479.8A 2015-11-23 2015-11-23 Emergency forced landing interactive simulation device Pending CN105374255A (en)

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Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107038927A (en) * 2017-05-27 2017-08-11 合肥磐石自动化科技有限公司 A kind of aircraft flight attitude apparatus for demonstrating
CN107424466A (en) * 2017-08-29 2017-12-01 深圳威阿科技有限公司 The airborne parachute jumping emergency procedure simulated training system of one kind
WO2018040736A1 (en) * 2016-09-05 2018-03-08 海口未来技术研究院 Near space experience system
CN110570744A (en) * 2018-06-06 2019-12-13 中国石油化工股份有限公司 Interactive hoisting operation simulation safety training teaching system
CN112798307A (en) * 2020-12-29 2021-05-14 中国航空工业集团公司西安飞机设计研究所 Six-degree-of-freedom airplane land crash emergency evacuation test system and method

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CN203260222U (en) * 2013-04-25 2013-10-30 泰州市普源视景仿真科技有限公司 Three-freedom simulated motion platform for navigation device and aircraft
CN103760780A (en) * 2014-02-17 2014-04-30 中国航空无线电电子研究所 Universal simulation platform of cockpit display control system
WO2015168799A1 (en) * 2014-05-08 2015-11-12 UNIVERSITé LAVAL Parallel mechanism with kinematically redundant actuation

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Publication number Priority date Publication date Assignee Title
US5490784A (en) * 1993-10-29 1996-02-13 Carmein; David E. E. Virtual reality system with enhanced sensory apparatus
CN200953191Y (en) * 2006-09-30 2007-09-26 吉林大学 Parallel six freedom driving simulator
CN101034503A (en) * 2007-04-10 2007-09-12 南京航空航天大学 Light flight simulating device
CN201051044Y (en) * 2007-05-24 2008-04-23 孙兆虎 Helicopter flying testing platform with 6 free degree
CN203102651U (en) * 2013-01-09 2013-07-31 湖州电力局 Insulating bucket truck simulation device based on six-degree-of-freedom motion control platform
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Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2018040736A1 (en) * 2016-09-05 2018-03-08 海口未来技术研究院 Near space experience system
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CN107038927A (en) * 2017-05-27 2017-08-11 合肥磐石自动化科技有限公司 A kind of aircraft flight attitude apparatus for demonstrating
CN107424466A (en) * 2017-08-29 2017-12-01 深圳威阿科技有限公司 The airborne parachute jumping emergency procedure simulated training system of one kind
CN110570744A (en) * 2018-06-06 2019-12-13 中国石油化工股份有限公司 Interactive hoisting operation simulation safety training teaching system
CN112798307A (en) * 2020-12-29 2021-05-14 中国航空工业集团公司西安飞机设计研究所 Six-degree-of-freedom airplane land crash emergency evacuation test system and method

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Application publication date: 20160302

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