CN105243919A - Simulated aircraft with manipulator - Google Patents

Simulated aircraft with manipulator Download PDF

Info

Publication number
CN105243919A
CN105243919A CN201510742854.1A CN201510742854A CN105243919A CN 105243919 A CN105243919 A CN 105243919A CN 201510742854 A CN201510742854 A CN 201510742854A CN 105243919 A CN105243919 A CN 105243919A
Authority
CN
China
Prior art keywords
base
flight
rotary drive
drive mechanism
pull rod
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
CN201510742854.1A
Other languages
Chinese (zh)
Other versions
CN105243919B (en
Inventor
江民中
黄振华
黄飞
曾庆锋
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.)
Shenzhen Playfun Culture & Technology Inc
Original Assignee
Shenzhen Playfun Culture & Technology Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Shenzhen Playfun Culture & Technology Inc filed Critical Shenzhen Playfun Culture & Technology Inc
Priority to CN201510742854.1A priority Critical patent/CN105243919B/en
Publication of CN105243919A publication Critical patent/CN105243919A/en
Application granted granted Critical
Publication of CN105243919B publication Critical patent/CN105243919B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • G09B9/10Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of aircraft, e.g. Link trainer with simulated flight- or engine-generated force being applied to aircraft occupant
    • 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
    • G09B9/12Motion systems for aircraft simulators

Landscapes

  • 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)
  • Toys (AREA)

Abstract

The invention provides a simulated aircraft with a manipulator. The simulated aircraft comprises the manipulator and a flight cabin, wherein the manipulator comprises a base, a lower supporting arm, a lower supporting arm driving unit, an upper supporting arm, a lower pull rod, a lower pull rod driving unit and an upper pull rod; the lower supporting arm is movably connected with the base, the lower supporting arm driving unit drives the lower supporting arm to move, the upper supporting arm is movably connected with the lower supporting arm, the lower pull rod is movably connected with the base, the lower pull rod driving unit drives the lower pull rod to move, one end of the upper pull rod is movably connected with the upper supporting arm, and the other end of the upper pull rod is movably connected with the lower pull rod; and the flight cabin comprises a flight cabin skeleton which is connected with the upper supporting arm. The simulated aircraft is safe and reliable, can simulate a real aircraft, is rich in action, vivid and strong in interaction, and brings great interactive entertainment experience to tourists.

Description

There is the simulated flight device of mechanical arm
Technical field
The present invention relates to amusement equipment field, particularly relate to the simulated flight device with mechanical arm.
Background technology
Along with the carrying out of science and technology, the development of society, 4D film has entered the life of people, the hardware device of current 4D film mostly is Six-freedom dynamic platform, and the shortcoming of Six-freedom dynamic platform is that flexibility ratio is poor, and compartment produces vibration, weak effect, cannot meet the demand of user.
Summary of the invention
In order to solve the problems of the prior art, the invention provides a kind of simulated flight device with mechanical arm.
The invention provides a kind of simulated flight device with mechanical arm, comprise mechanical arm and flight capsule body, described mechanical arm comprises base, lower support arm, lower support arm driver element, upper sway brace, lower link, lower link driver element, upper connecting rod, described lower support arm and described base are for being flexibly connected, lower support arm motion described in described lower support arm drive unit drives, described upper sway brace and described lower support arm are for being flexibly connected, described lower link and described base are for being flexibly connected, lower link motion described in described lower link drive unit drives, described upper connecting rod one end and described upper sway brace are for being flexibly connected, the described upper connecting rod other end and described lower link are for being flexibly connected, this flight capsule body comprises flight capsule skeleton, and described flight capsule skeleton is connected with described upper sway brace.
As a further improvement on the present invention, described mechanical arm also comprises underframe and is arranged on the base rotary drive mechanism on described underframe, described floor installation, on described base rotary drive mechanism, drives described base to rotate by described base rotary drive mechanism.
As a further improvement on the present invention, described mechanical arm also comprises balance base, balance plate and balancing pull rod, and described balance base and described balance plate are installed on described upper sway brace two ends respectively, and described balancing pull rod is connected between described balance base and described balance plate.
As a further improvement on the present invention, described flight capsule body also comprises tilting mechanism, and described tilting mechanism is arranged on described upper sway brace, and described flight capsule skeleton is connected with described tilting mechanism, drives described flight capsule skeleton to vacillate now to the left, now to the right by tilting mechanism.
As a further improvement on the present invention, described flight capsule body also comprises the rotor be arranged on described flight capsule skeleton.
As a further improvement on the present invention, described flight capsule body also comprises rotary drive mechanism, described rotary drive mechanism is arranged on described flight capsule skeleton, and described rotor is connected with described rotary drive mechanism, and described rotary drive mechanism drives described rotor to tilt forward and back.
As a further improvement on the present invention, this simulated flight device also comprises PLC control unit, and described PLC control unit controls the duty of described lower support arm driver element, lower link driver element, base rotary drive mechanism and described rotor respectively.
The invention has the beneficial effects as follows: safe and reliable, that is virtually reality like reality aircraft of simulated flight device of the present invention, its action is enriched, it is lively to show and by force interactive, is that the great interaction entertainment that visitor brings is experienced.
Accompanying drawing explanation
Fig. 1 is structural representation of the present invention.
Fig. 2 is flight capsule body structure schematic diagram of the present invention.
Fig. 3 is robot manipulator structure schematic diagram of the present invention.
Embodiment
As shown in Figures 1 to 3, the invention discloses a kind of simulated flight device with mechanical arm, comprise mechanical arm and flight capsule body, described mechanical arm comprises base 2, lower support arm 3, lower support arm driver element 12, upper sway brace 4, lower link 6, lower link driver element 13, upper connecting rod 7, described lower support arm 3 and described base 2 are for being flexibly connected, described lower support arm driver element 12 drives described lower support arm 3 to move, described upper sway brace 4 and described lower support arm 3 are for being flexibly connected, described lower link 6 and described base 2 are for being flexibly connected, described lower link driver element 13 drives described lower link 6 to move, described upper connecting rod 7 one end and described upper sway brace 4 are for being flexibly connected, described upper connecting rod 7 other end and described lower link 6 are for being flexibly connected, this flight capsule body comprises flight capsule skeleton 15, and described flight capsule skeleton 15 is connected with described upper sway brace 4.
Described mechanical arm also comprises underframe 1 and is arranged on the base rotary drive mechanism 11 on described underframe 1, and described base 2 is arranged on described base rotary drive mechanism 11, drives described base 2 to rotate by described base rotary drive mechanism 11.
Described mechanical arm also comprises balance base 5, balance plate 9 and balancing pull rod 10, and described balance base 5 and described balance plate 9 are installed on described upper sway brace 4 two ends respectively, and described balancing pull rod 10 is connected between described balance base 5 and described balance plate 9.By the cooperation of balance base 5, balance plate 9 and balancing pull rod 10, when can ensure mechanical arm arbitrary motion, its balance base 5 remains original state.
Described flight capsule body also comprises tilting mechanism 14, and described tilting mechanism 14 is arranged on described upper sway brace 4, and described flight capsule skeleton 15 is connected with described tilting mechanism 14, drives described flight capsule skeleton 15 to vacillate now to the left, now to the right by tilting mechanism 14.
Described flight capsule body also comprises the rotor 17 be arranged on described flight capsule skeleton 15.
Described flight capsule body also comprises rotary drive mechanism 16, and described rotary drive mechanism 16 is arranged on described flight capsule skeleton 15, and described rotor 17 is connected with described rotary drive mechanism 16, and described rotary drive mechanism 16 drives described rotor 17 to tilt forward and back.
Flight capsule body of the present invention realizes aircraft flight action simulation by the mechanical arm be attached thereto, and realizes visitor's flying adventure and experiences.Simulated flight device lands and takes up an area long 4000mm, wide 4000mm, and be highly 3000mm, moving radius 5500mm, weight is about 2.5t.
In flight capsule skeleton 15, seat is installed, rotor 17 variable rotation speed of the present invention.
This simulated flight device also comprises PLC control unit, described PLC control unit controls the duty of described lower support arm driver element 12, lower link driver element 13 and base rotary drive mechanism 11 respectively, namely controls its average velocity, acceleration, range of movement, beginning and ending time etc.
PLC control unit also controls the duty of rotor 17, namely controls the average velocity, acceleration, range of movement, beginning and ending time etc. of rotor 17.
Base rotary drive mechanism 11 can self contained function, and the flight capsule body made realizes 360 ° of rotations.By the connecting rod mechanism movement of mechanical arm, thus make lower support arm driver element 12 and lower link driver element 13 combinative movement, flight capsule body can be made to realize movable, oscilaltion; Pull bar contracting mechanism 8 self contained function, can make flight capsule body realize pitch; Tilting mechanism 14 self contained function, can make flight capsule body realize vacillating now to the left, now to the right.
Flexible connection of the present invention can be connected through the hinge or connected by axle, in the present invention, servomotor by electric cylinder, each movable joint connecting rod mechanism movement of reductor push-pull maneuver aircraft, realize the oscilaltion of flight capsule body, anterior-posterior translation, vacillate now to the left, now to the right, pitch, 360 ° of spinning movements.
Above content is in conjunction with concrete preferred implementation further description made for the present invention, can not assert that specific embodiment of the invention is confined to these explanations.For general technical staff of the technical field of the invention, without departing from the inventive concept of the premise, some simple deduction or replace can also be made, all should be considered as belonging to protection scope of the present invention.

Claims (7)

1. one kind has the simulated flight device of mechanical arm, it is characterized in that: comprise mechanical arm and flight capsule body, described mechanical arm comprises base (2), lower support arm (3), lower support arm driver element (12), upper sway brace (4), lower link (6), lower link driver element (13), upper connecting rod (7), described lower support arm (3) and described base (2) are for being flexibly connected, described lower support arm driver element (12) drives described lower support arm (3) to move, described upper sway brace (4) and described lower support arm (3) are for being flexibly connected, described lower link (6) and described base (2) are for being flexibly connected, described lower link driver element (13) drives described lower link (6) to move, described upper connecting rod (7) one end and described upper sway brace (4) are for being flexibly connected, described upper connecting rod (7) other end and described lower link (6) are for being flexibly connected, this flight capsule body comprises flight capsule skeleton (15), and described flight capsule skeleton (15) is connected with described upper sway brace (4).
2. simulated flight device according to claim 1, it is characterized in that: described mechanical arm also comprises underframe (1) and is arranged on the base rotary drive mechanism (11) on described underframe (1), described base (2) is arranged on described base rotary drive mechanism (11), drives described base (2) to rotate by described base rotary drive mechanism (11).
3. simulated flight device according to claim 1, it is characterized in that: described mechanical arm also comprises balance base (5), balance plate (9) and balancing pull rod (10), described balance base (5) and described balance plate (9) are installed on described upper sway brace (4) two ends respectively, and described balancing pull rod (10) is connected between described balance base (5) and described balance plate (9).
4. simulated flight device according to claim 1, it is characterized in that: described flight capsule body also comprises tilting mechanism (14), described tilting mechanism (14) is arranged on described upper sway brace (4), described flight capsule skeleton (15) is connected with described tilting mechanism (14), drives described flight capsule skeleton (15) to vacillate now to the left, now to the right by tilting mechanism (14).
5. simulated flight device according to claim 2, is characterized in that: described flight capsule body also comprises the rotor (17) be arranged on described flight capsule skeleton (15).
6. simulated flight device according to claim 5, it is characterized in that: described flight capsule body also comprises rotary drive mechanism (16), described rotary drive mechanism (16) is arranged on described flight capsule skeleton (15), described rotor (17) is connected with described rotary drive mechanism (16), and described rotary drive mechanism (16) drives described rotor (17) to tilt forward and back.
7. simulated flight device according to claim 5, it is characterized in that: this simulated flight device also comprises PLC control unit, described PLC control unit controls the duty of described lower support arm driver element (12), lower link driver element (13), base rotary drive mechanism (11) and described rotor (17) respectively.
CN201510742854.1A 2015-11-04 2015-11-04 Simulated flight device with manipulator Active CN105243919B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201510742854.1A CN105243919B (en) 2015-11-04 2015-11-04 Simulated flight device with manipulator

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201510742854.1A CN105243919B (en) 2015-11-04 2015-11-04 Simulated flight device with manipulator

Publications (2)

Publication Number Publication Date
CN105243919A true CN105243919A (en) 2016-01-13
CN105243919B CN105243919B (en) 2018-11-06

Family

ID=55041544

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201510742854.1A Active CN105243919B (en) 2015-11-04 2015-11-04 Simulated flight device with manipulator

Country Status (1)

Country Link
CN (1) CN105243919B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107694090A (en) * 2017-09-29 2018-02-16 广州云友网络科技有限公司 A kind of simulated flight system of virtual scene combination manipulator

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2009089561A2 (en) * 2008-01-18 2009-07-23 Wunderwerk Digitale Medien Produktion Gmbh Method for simulating flight statuses of a vertical take-off and/or vertical landing-capable aircraft
EP2363849A2 (en) * 2010-01-22 2011-09-07 Wunderwerk Digitale Medien Produktion Gmbh Training assembly for training flight conditions
DE102010049153A1 (en) * 2010-10-22 2012-04-26 Deutsches Zentrum für Luft- und Raumfahrt e.V. Simulator comprises joint-arm robot and gondola which is mounted on joint-arm, where gondola has base part with seating unit and cover, and gondola is provided with mounting device
CN102971777A (en) * 2010-05-21 2013-03-13 马克思-普朗克科学促进协会 Motion simulator and corresponding method
EP2574384A1 (en) * 2011-09-28 2013-04-03 KUKA Laboratories GmbH Fairground ride and method for operating same
CN103155017A (en) * 2010-08-30 2013-06-12 格伦策巴赫机械制造有限公司 Apparatus and method for operating a flight simulator with a special impression of reality
CN104708618A (en) * 2015-03-16 2015-06-17 广东顺德三合工业自动化设备有限公司 Robot
CN205177206U (en) * 2015-11-04 2016-04-20 深圳市普乐方文化科技股份有限公司 Simulated flight ware with manipulator

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2009089561A2 (en) * 2008-01-18 2009-07-23 Wunderwerk Digitale Medien Produktion Gmbh Method for simulating flight statuses of a vertical take-off and/or vertical landing-capable aircraft
EP2363849A2 (en) * 2010-01-22 2011-09-07 Wunderwerk Digitale Medien Produktion Gmbh Training assembly for training flight conditions
CN102971777A (en) * 2010-05-21 2013-03-13 马克思-普朗克科学促进协会 Motion simulator and corresponding method
CN103155017A (en) * 2010-08-30 2013-06-12 格伦策巴赫机械制造有限公司 Apparatus and method for operating a flight simulator with a special impression of reality
DE102010049153A1 (en) * 2010-10-22 2012-04-26 Deutsches Zentrum für Luft- und Raumfahrt e.V. Simulator comprises joint-arm robot and gondola which is mounted on joint-arm, where gondola has base part with seating unit and cover, and gondola is provided with mounting device
EP2574384A1 (en) * 2011-09-28 2013-04-03 KUKA Laboratories GmbH Fairground ride and method for operating same
CN104708618A (en) * 2015-03-16 2015-06-17 广东顺德三合工业自动化设备有限公司 Robot
CN205177206U (en) * 2015-11-04 2016-04-20 深圳市普乐方文化科技股份有限公司 Simulated flight ware with manipulator

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107694090A (en) * 2017-09-29 2018-02-16 广州云友网络科技有限公司 A kind of simulated flight system of virtual scene combination manipulator

Also Published As

Publication number Publication date
CN105243919B (en) 2018-11-06

Similar Documents

Publication Publication Date Title
US20030219702A1 (en) Flight simulator
CN206672418U (en) A kind of rotary simulation system of Three Degree Of Freedom
CN102779438B (en) Flight simulated mechanical execution system simulating full-motion of airplane
CN202795801U (en) Ball flight simulation device
CN103623583B (en) Flight experience simulator
CN104192324B (en) The synchronous space three-dimensional simulator of swing arm type rotation
CN102208141B (en) Suspended-type research training device for simulating ground weightlessness
KR20150005873A (en) 3d-paragliding experiencing apparatus
CN106139595B (en) Three-dimensional railcar
RU130733U1 (en) AIRCRAFT PILOT SIMULATOR
CN104217622B (en) Simulation aircraft and system thereof
CN205177206U (en) Simulated flight ware with manipulator
CN105243919A (en) Simulated aircraft with manipulator
CN106251736A (en) A kind of paragliding VR simulator
CN207541805U (en) A kind of flight simulator list manipulates central linkage
CN206363575U (en) A kind of paragliding VR simulators
CN201101893Y (en) Telecontrolled model helicopter
CN208400337U (en) Simulator and analog machine
CN203870839U (en) Rotating device for aircraft simulation training
CN205055419U (en) Amusement emulation aircraft
CN102350059B (en) Electromagnetic helm gear
CN107862971B (en) Bird visual angle flight simulator platform based on virtual reality technology
CN208400338U (en) Simulator and simulation system
JP3029206U (en) Flight play equipment
CN112498703B (en) Motion device based on real sense parachuting simulation trainer and use method thereof

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant
CP02 Change in the address of a patent holder
CP02 Change in the address of a patent holder

Address after: 518000 Chegongmiao Tianan Innovation Technology Plaza A1403-28, Shatian Street, Futian District, Shenzhen City, Guangdong Province

Patentee after: SHENZHEN PLAYFUN CULTURE SCIENCE AND TECHNOLOGY Co.,Ltd.

Address before: 518000 Room 501-525B39, Huarong Building, Futian Street Center, Futian District, Shenzhen City, Guangdong Province

Patentee before: SHENZHEN PLAYFUN CULTURE SCIENCE AND TECHNOLOGY Co.,Ltd.

PE01 Entry into force of the registration of the contract for pledge of patent right
PE01 Entry into force of the registration of the contract for pledge of patent right

Denomination of invention: Simulated aircraft with manipulator

Effective date of registration: 20211221

Granted publication date: 20181106

Pledgee: Shenzhen Longgang sub branch of Agricultural Bank of China Ltd.

Pledgor: SHENZHEN PLAYFUN CULTURE SCIENCE AND TECHNOLOGY Co.,Ltd.

Registration number: Y2021980015801

PC01 Cancellation of the registration of the contract for pledge of patent right
PC01 Cancellation of the registration of the contract for pledge of patent right

Date of cancellation: 20230317

Granted publication date: 20181106

Pledgee: Shenzhen Longgang sub branch of Agricultural Bank of China Ltd.

Pledgor: SHENZHEN PLAYFUN CULTURE SCIENCE AND TECHNOLOGY Co.,Ltd.

Registration number: Y2021980015801