CN108492667A - A kind of multi-angle, multi-pose flight training simulator - Google Patents
A kind of multi-angle, multi-pose flight training simulator Download PDFInfo
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- CN108492667A CN108492667A CN201810505205.3A CN201810505205A CN108492667A CN 108492667 A CN108492667 A CN 108492667A CN 201810505205 A CN201810505205 A CN 201810505205A CN 108492667 A CN108492667 A CN 108492667A
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- annular mounting
- mounting frame
- rotating platform
- motor
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- 238000012549 training Methods 0.000 title claims abstract description 20
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims abstract description 13
- 125000004122 cyclic group Chemical group 0.000 claims abstract description 4
- 230000000694 effects Effects 0.000 claims abstract description 3
- 238000009434 installation Methods 0.000 claims description 3
- 238000004088 simulation Methods 0.000 abstract description 7
- 238000004519 manufacturing process Methods 0.000 abstract description 3
- 230000033001 locomotion Effects 0.000 description 7
- 238000011161 development Methods 0.000 description 4
- 238000000034 method Methods 0.000 description 3
- 230000008901 benefit Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000011160 research Methods 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- 238000007792 addition Methods 0.000 description 1
- 230000000386 athletic effect Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000011982 device technology Methods 0.000 description 1
- 230000009189 diving Effects 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 230000010006 flight Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
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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
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- General Physics & Mathematics (AREA)
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Abstract
The present invention discloses a kind of multi-angle, multi-pose flight training simulator, including pedestal, rotating platform, annular mounting frame and cockpit model, rotating platform is located at the top of pedestal, and the bottom of rotating platform is connected with base rotation, the first motor driving rotating platform rotation being set on the base.The both sides of annular mounting frame are rotatedly connected with the top of rotating platform respectively, and the side of rotating platform is provided with the second motor, and the output end of the second motor is connected with annular mounting frame, can drive its rotation.Sliding slot is provided on the madial wall of annular mounting frame, sliding slot is the cyclic structure being closed.Cockpit model is located at the inside of annular mounting base, is connected with annular mounting frame by multiple adjustable and retractable bars.One end of each adjustable and retractable bar is connect with cockpit model activity, the flexible connection of other end annular mounting frame.The configuration of the present invention is simple, manufacturing cost is low, repair and easy to maintain, and adjustment is easy, can carry out multi-angle, multi-pose fly simulation training.
Description
Technical field
The present invention relates to flight simulation equipment technology fields, and in particular to a kind of multi-angle, multi-pose flight training simulation
Device.
Background technology
Flight training simulator can reappear airflight environment, be mainly used for the design of aircraft, research, experiment, fly
Training and teaching of office staff etc..Strong technical support is provided for development of new aircraft and training pilot, there is peace
Entirely, the advantages that economic, reusable and round-the-clock is one of important support equipment of national development aviation industry.Flight mould
Quasi- device technology synchronized development with the development of emulation technology and aviation industry.
Well-known parallel institution is big with rigidity, mechanism stable, bearing capacity is strong, precision is high, motional inertia is small, anti-
Solution controls simple feature.Currently, the movement simulation that skimulated motion in parallel mechanism is widely used for aircraft, naval vessel and automobile etc. is imitative
Very.But most of emulator has the problems such as shape is big, working space is small, operating angle range is small.It is especially imitative to large size
True device is of high cost and not easy care, so the full posture parallel connection simulated flight of wide-angle is research hotspot.Improve motion simulator
Athletic posture motion range is one of critical issue.
Modern combat aircraft has very high maneuverability requirement, and in order to obtain the initiative of air battle, pilot must flexibly answer
It is acted with various tactical maneuvers, such as roll, pitching, racing, these maneuvering flights all have the characteristics that attitude angle changes greatly,
Some maneuvering flight corners want the flight of comprehensive simulated fighter plane, the posture of flight simulator motion platform close to 360 degree
Variation cannot be restricted, it is necessary to have 360 degree of attitudes vibration ability can be rotated around the arbitrary shaft in space.Conventional simulator without
The mobility simulation that method meets fighter plane requires, and to generate true fighter flight posture and movement, affects
The actual effect of flight training.Therefore it is badly in need of having big corner range, the flight instruction of full attitude motion parameter simulation may be implemented
Practice simulator.
Invention content
In view of the above shortcomings of the prior art, it is an object of the invention to propose that one kind is simple in structure, manufacturing cost is low, adjust
Perfect square just, the flight training simulator of many attitude can be simulated.
In order to solve the above-mentioned technical problem, the technical solution adopted in the present invention is：
A kind of multi-angle, multi-pose flight training simulator, including pedestal, rotating platform, annular mounting frame and cockpit
Model, the rotating platform are located at the top of pedestal, and the bottom of rotating platform is connected with base rotation, be set on the base
One motor drives rotating platform rotation.The both sides of the annular mounting frame are rotatedly connected with the top of rotating platform respectively, rotation
The side of platform is provided with the second motor, and the output end of the second motor is connected with annular mounting frame, can drive its rotation.The ring
Sliding slot is provided on the madial wall of shape mounting bracket, sliding slot is the cyclic structure being closed.Cockpit model is located at the interior of annular mounting base
Side is connected by multiple adjustable and retractable bars with annular mounting frame.It lives with cockpit model one end of each adjustable and retractable bar
Dynamic connection, the flexible connection of other end annular mounting frame.
Preferably, rotating platform includes main platform body and U-bracket, and U-bracket is located above main platform body, and solid with it
Surely it is connected as a body, the bottom of main platform body is connected with base rotation.
Preferably, the opposite both sides of annular mounting frame are respectively equipped with a shaft, and two shaft forward directions are opposite and coaxial,
In a shaft and the output end of the second motor of its homonymy be fixedly linked.
Preferably, the quantity of adjustable and retractable bar is four, one end of each adjustable and retractable bar respectively with cockpit model
Top, bottom, left side and right side it is hinged, the other end is installed with sliding block, and sliding block stretches into the inside of sliding slot and annular is pacified
Sliding is shelved to be connected.
Preferably, the both sides that sliding block is contacted with sliding slot inner wall are respectively set there are one telescopic press head, and the inside of sliding block is fixed
There are one Dual-output shaft motor, two output ends of Dual-output shaft motor to be threadedly coupled respectively with telescopic press head for installation, and driving is stretched
Contracting pressure head is flexible relative to sliding block.
Preferably, the cross section of the sliding slot is T-shaped structure.
By using above-mentioned technical proposal, the method have the benefit that：The configuration of the present invention is simple, manufacturing cost
Low, repair and easy to maintain, adjustment is easy, can carry out multi-angle, multi-pose fly simulation training.
Description of the drawings
Fig. 1 is a kind of multi-angle of the present invention, the principle schematic diagram of multi-pose flight training simulator.
Fig. 2 is the structural schematic diagram of certain part in Fig. 1, thus it is shown that sliding block and associated components.
Specific implementation mode
The present invention is described in detail below in conjunction with the accompanying drawings：
A kind of multi-angle, multi-pose flight training simulator combined with Figure 1 and Figure 2, including pedestal 1, rotating platform 2, annular
Mounting bracket 3 and cockpit model 4, the rotating platform 2 are located at the top of pedestal 1, and the bottom of rotating platform 2 passes through pivoting support
It is rotatedly connected with pedestal 1, is arranged and is installed with first motor 7 in the inside of pedestal 1, first motor 7 drives 2 phase of rotating platform
Pedestal 1 is rotated.Rotating platform 2 includes main platform body 21 and U-bracket 22, and U-bracket 22 is located at 21 top of main platform body,
Its bottom and the upper surface of main platform body 21 are fixedly linked integrally, and bottom and the pedestal 1 of main platform body 21 are rotatedly connected, U-shaped
Holder 22 is rotated together with main platform body 21.
The outside of the opposite left and right sides of annular mounting frame 3, is respectively equipped with the shaft of a lateral arrangement, and the one of each shaft
End and the outer wall of 3 respective side of annular mounting frame are fixedly linked integrally, and two shaft forward directions are opposite and coaxial.The annular installation
Frame is rotatedly connected with the top of rotating platform 2 around the axis of shaft by the shaft of its both sides, and the right side of rotating platform 2 is solid
Dingan County is equipped with the second motor 5, and the output end of the second motor 5 and the end of the shaft on 3 right side of annular mounting frame are fixedly linked, and second
In the operating condition, the power output end of the second motor 5 drives annular mounting frame 3 around the axis of the shaft of its both sides to motor 5
Rotation.
Be provided with sliding slot on the madial wall of the annular mounting frame 3, sliding slot is the cyclic structure being closed, the sliding slot it is transversal
Face is T-shaped structure.Cockpit model 4 is located at the inside of annular mounting base 3, and cockpit model 4 passes through adjustable and retractable bar 6 and ring
Shape mounting bracket 3 is movably connected.The quantity of adjustable and retractable bar 6 is four, one end and the cockpit model of each adjustable and retractable bar 6
4 outer wall flexible connection, the inside flexible connection of other end annular mounting frame 3.Specifically, four adjustable and retractable bars 6
One end is hinged with the top of cockpit model 4, bottom, left side and right side respectively, and the other end is installed with sliding block 61, sliding block
The inside that 61 enter sliding slot is stretched with the sliding of annular mounting frame 3 to be connected.
The both sides of sliding block 61 and sliding slot inner wall sliding contact are respectively set there are one telescopic press head 62, the inside of sliding block 61
It is fixedly mounted there are one Dual-output shaft motor 63, two output ends of Dual-output shaft motor 63 screw in corresponding flexible pressure respectively
First 62, and be threadedly coupled with telescopic press head 62, driving telescopic press head 62 is flexible relative to sliding block 61, and the telescopic press head 62 is inserted into
The inside of sliding block 61 is slidably matched with sliding block 61, output end two telescopic press heads 62 of driving of Dual-output shaft motor 63, while to
Outer stretching inwardly bounces back simultaneously, and two telescopic press heads 62 stretch out outward to be contacted with the inner wall of sliding slot, compresses, and realizes sliding block 61
With the fixation of annular mounting frame 3.
The present invention can simulate a variety of flight attitudes of cockpit model, and following application method is adjusted：
Simulator cockpit model smooth flight posture：Rotating platform 2 remains stationary as, and annular mounting frame 3 is located at perpendicular
Interior and holding vertical state, the length of four adjustable and retractable bars 6 of adjustment and position, make the length of four adjustable and retractable bars 6
Be equal, the adjustable and retractable bar 6 of the left and right sides of cockpit model 4 keeps horizontal, at the top and bottom of adjustable and retractable bar 6
Keep vertical, one end of each adjustable and retractable bar 6 is fixed with annular mounting frame 3 and remains stationary state.
Simulator cockpit model tumbling flight posture：First, it keeps rotating platform 2 stationary, adjusts four and be adjusted
The length of telescopic rod 6 and position, the surrounding for making four 6 equal lengths of adjustable and retractable bar, being evenly distributed on cockpit model 4.
Start the second motor 5 being arranged in 2 side of rotating platform, the second motor 5 drives cockpit model 4 to be rotated with annular mounting frame 3.
Simulator cockpit model laterally kick posture (for the left, to the right otherwise)：First, annular mounting frame 3
Plane keep vertical state.Secondly, it is inclined to be located at 4 top of cockpit model, lower section and three, left side adjustable and retractable bar 6 for adjustment
To the left, three adjustable and retractable bars 6 are made to shrink, the adjustable and retractable bar 6 on 4 right side of the cockpit model extends, and makes driving
Cabin model 4 is partial to the left side of annular mounting frame 3.Finally, starting first motor 7, first motor 7 drives rotating platform 2 to rotate,
Rotating platform 2 drives annular mounting frame 3 to rotate, and vertical state is remained in 3 rotary course of annular mounting frame.
Simulator cockpit model accelerates diving flight posture：The length of four adjustable and retractable bars 6 of adjustment and position, make four
6 equal length of a adjustable and retractable bar, the surrounding for being evenly distributed on cockpit model 4.It keeps rotating platform 2 stationary, leads to
Cross the inclination angle of the plane of 5 annular mounting frame 3 of the second motor so that the top of annular mounting frame 3 turns forward, and its underpart retreats
Tiltedly.
Simulator cockpit model accelerates lifting flight attitude：The length of four adjustable and retractable bars 6 of adjustment and position, make four
6 equal length of a adjustable and retractable bar, the surrounding for being evenly distributed on cockpit model 4.It keeps rotating platform 2 stationary, leads to
Cross the inclination angle of the plane of 5 annular mounting frame 3 of the second motor so that the top of annular mounting frame 3 tilts backwards, and its underpart turns forward
Tiltedly.
Certainly, above description is not limitation of the present invention, and the present invention is also not limited to the example above, this technology neck
The variations, modifications, additions or substitutions that the technical staff in domain is made in the essential scope of the present invention should also belong to the present invention's
Protection domain.
Claims (6)
1. a kind of multi-angle, multi-pose flight training simulator, including pedestal, rotating platform, annular mounting frame and cockpit mould
Type, which is characterized in that the rotating platform is located at the top of pedestal, and the bottom of rotating platform is connected with base rotation, and setting exists
First motor driving rotating platform rotation on pedestal；The both sides of the annular mounting frame are rotated with the top of rotating platform respectively
It is connected, the side of rotating platform is provided with the second motor, and the output end of the second motor is connected with annular mounting frame, can drive its turn
It is dynamic；Sliding slot is provided on the madial wall of the annular mounting frame, sliding slot is the cyclic structure being closed；Cockpit model, which is located at annular, pacifies
The inside for filling seat, is connected by multiple adjustable and retractable bars with annular mounting frame；One end of each adjustable and retractable bar and driving
Cabin model activity connection, the flexible connection of other end annular mounting frame.
2. a kind of multi-angle according to claim 1, multi-pose flight training simulator, which is characterized in that rotating platform
Including main platform body and U-bracket, U-bracket is located above main platform body, and is secured to be connected as a body, main platform body
Bottom is connected with base rotation.
3. a kind of multi-angle according to claim 1, multi-pose flight training simulator, which is characterized in that annular installation
The opposite both sides of frame are respectively equipped with a shaft, and two shaft forward directions are opposite and coaxial, and the of one of shaft and its homonymy
The output end of two motors is fixedly linked.
4. a kind of multi-angle according to claim 1, multi-pose flight training simulator, which is characterized in that adjustable to stretch
The quantity of contracting bar is four, and one end of each adjustable and retractable bar is cut with scissors with the top of cockpit model, bottom, left side and right side respectively
It connects, the other end is installed with sliding block, and the inside that sliding block stretches into sliding slot is connected with annular mounting frame sliding.
5. a kind of multi-angle according to claim 1, multi-pose flight training simulator, which is characterized in that sliding block and cunning
The both sides of slot inner wall contact are respectively set there are one telescopic press head, and the inside of sliding block is fixedly mounted there are one Dual-output shaft motor,
Two output ends of Dual-output shaft motor are threadedly coupled with telescopic press head respectively, and driving telescopic press head is flexible relative to sliding block.
6. a kind of multi-angle according to claim 1, multi-pose flight training simulator, which is characterized in that the sliding slot
Cross section be T-shaped structure.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810505205.3A CN108492667A (en) | 2018-05-24 | 2018-05-24 | A kind of multi-angle, multi-pose flight training simulator |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810505205.3A CN108492667A (en) | 2018-05-24 | 2018-05-24 | A kind of multi-angle, multi-pose flight training simulator |
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| Publication Number | Publication Date |
|---|---|
| CN108492667A true CN108492667A (en) | 2018-09-04 |
Family
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810505205.3A Pending CN108492667A (en) | 2018-05-24 | 2018-05-24 | A kind of multi-angle, multi-pose flight training simulator |
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| CN (1) | CN108492667A (en) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109454472A (en) * | 2018-11-01 | 2019-03-12 | 东南大学 | A kind of space multiple degrees of freedom positioning device and its spatial position calculation method |
| CN111899599A (en) * | 2019-08-22 | 2020-11-06 | 王晨曦 | Flight simulator 3DOF cockpit |
| CN112462161A (en) * | 2020-10-19 | 2021-03-09 | 芜湖赛宝机器人产业技术研究院有限公司 | Detection test device suitable for electromagnetic compatibility of industrial robot |
| CN113192383A (en) * | 2021-05-28 | 2021-07-30 | 江苏无国界航空技术有限公司 | PFCU exercise rack |
| CN113495496A (en) * | 2021-06-07 | 2021-10-12 | 中北大学 | Large-inertia three-degree-of-freedom attitude simulation device |
| CN113498952A (en) * | 2021-06-07 | 2021-10-15 | 西安理工大学 | Model display device with human-computer interaction function |
| CN115457836A (en) * | 2022-09-23 | 2022-12-09 | 燕山大学 | Real-scene control-based helicopter simulation driving platform |
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| CN102789709A (en) * | 2012-08-21 | 2012-11-21 | 徐强 | Mechanical structure for multi-axis wireless movement method of flight simulator |
| CN106297473A (en) * | 2016-10-26 | 2017-01-04 | 覃伟 | Multi-functional VR man-machine interaction and the simulator of external environment condition and analogy method |
| CN106710364A (en) * | 2017-01-24 | 2017-05-24 | 山东科技大学 | Parallel type flight training simulator |
| CN208985425U (en) * | 2018-05-24 | 2019-06-14 | 山东科技大学 | A kind of multi-angle, multi-pose flight training simulator |
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2018
- 2018-05-24 CN CN201810505205.3A patent/CN108492667A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
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| JPH0736160U (en) * | 1993-12-15 | 1995-07-04 | 仲成儀器股▲分▼有限公司 | Six-axis motion simulator |
| CN102789709A (en) * | 2012-08-21 | 2012-11-21 | 徐强 | Mechanical structure for multi-axis wireless movement method of flight simulator |
| CN106297473A (en) * | 2016-10-26 | 2017-01-04 | 覃伟 | Multi-functional VR man-machine interaction and the simulator of external environment condition and analogy method |
| CN106710364A (en) * | 2017-01-24 | 2017-05-24 | 山东科技大学 | Parallel type flight training simulator |
| CN208985425U (en) * | 2018-05-24 | 2019-06-14 | 山东科技大学 | A kind of multi-angle, multi-pose flight training simulator |
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109454472A (en) * | 2018-11-01 | 2019-03-12 | 东南大学 | A kind of space multiple degrees of freedom positioning device and its spatial position calculation method |
| CN109454472B (en) * | 2018-11-01 | 2019-11-05 | 东南大学 | A kind of space multiple degrees of freedom positioning device and its spatial position calculation method |
| CN111899599A (en) * | 2019-08-22 | 2020-11-06 | 王晨曦 | Flight simulator 3DOF cockpit |
| CN111899599B (en) * | 2019-08-22 | 2022-06-07 | 王晨曦 | Flight simulator 3DOF cockpit |
| CN112462161A (en) * | 2020-10-19 | 2021-03-09 | 芜湖赛宝机器人产业技术研究院有限公司 | Detection test device suitable for electromagnetic compatibility of industrial robot |
| CN112462161B (en) * | 2020-10-19 | 2022-05-17 | 芜湖赛宝机器人产业技术研究院有限公司 | Detection test device suitable for electromagnetic compatibility of industrial robot |
| CN113192383A (en) * | 2021-05-28 | 2021-07-30 | 江苏无国界航空技术有限公司 | PFCU exercise rack |
| CN113495496A (en) * | 2021-06-07 | 2021-10-12 | 中北大学 | Large-inertia three-degree-of-freedom attitude simulation device |
| CN113498952A (en) * | 2021-06-07 | 2021-10-15 | 西安理工大学 | Model display device with human-computer interaction function |
| CN113495496B (en) * | 2021-06-07 | 2024-04-09 | 中北大学 | Large-inertia three-degree-of-freedom gesture simulation device |
| CN115457836A (en) * | 2022-09-23 | 2022-12-09 | 燕山大学 | Real-scene control-based helicopter simulation driving platform |
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Application publication date: 20180904 |