CN107293185A - A kind of pilot's simulated training multi-angle rotary device - Google Patents
A kind of pilot's simulated training multi-angle rotary device Download PDFInfo
- Publication number
- CN107293185A CN107293185A CN201710729944.6A CN201710729944A CN107293185A CN 107293185 A CN107293185 A CN 107293185A CN 201710729944 A CN201710729944 A CN 201710729944A CN 107293185 A CN107293185 A CN 107293185A
- Authority
- CN
- China
- Prior art keywords
- angle
- angular adjustment
- pilot
- angle demodulator
- rotary device
- 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.)
- Pending
Links
Classifications
-
- 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
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 discloses a kind of pilot's simulated training multi-angle rotary device, including base, the base upper end is provided with rotating disk, the rotating disk upper end is provided with angle demodulator, the angle demodulator side offers angular adjustment groove, the angle demodulator back side is provided with stepper motor, the angle demodulator and is provided with angular adjustment disk.The present invention is used to drive angle demodulator to rotate in the horizontal plane using electric rotating machine, simultaneously, training seat is driven to rotate adjustment angle in perpendicular around the angle demodulator using stepper motor, so as to realize training seat multi-angle rotary regulation, compared to it is traditional using whole pilot's simulation trainer rotation come drive training seat multi-angle rotary by the way of compare, corresponding speed is fast, flexible movements are changeable, and angle adjustment scope is big, easy to operate, practicality is good.
Description
Technical field
The present invention relates to pilot's simulated training multi-angle rotary device field, more particularly to a kind of pilot's simulation
Multi-angle rotary device is used in training.
Background technology
Flight training simulator is a kind of equipment for training pilot, typically by driving cabin, interface equipment and each quasi-instrument,
Visual system and training computer composition.Computer is the control centre of flight training simulator.Student is sitting in training
Various operations can be carried out in driving cabin：Electric switch, push-and-pull throttle, operation flight bar and rudder are opened, various data can also be obtained,
Such as flying speed, stroke, position, height, wind direction, wind speed.And visual system can provide the object simulation residing for student, student
In operation just as being sitting in aircraft, feel underriding, row and coiling action are faced upward, it can be seen that various scenery above and below aircraft
(cloud, mist, river, building), can also set various flight environment of vehicle, with all round exercise technology, learning and mastering difficulty it is larger and
Dangerous various operations.As long as therefore simulated conditions are true to nature, then at once can after the student's graduation for passing through fly simulation training
Drive an airplane lift-off manoeuvre, therefore applies quite varied in pilot's daily workout, still, traditional flight training simulator
Some problems are still suffered from actual use.Whole flight training is typically used during such as traditional pilot's simulated training
The multi-angle rotary of simulator trains seat multi-angle rotary to help pilot training to drive, because body is simulated in flight training
Product is huge, and therefore, angle of regulation range is small, and dynamic response is slower, and practicality is not strong, for above-mentioned situation, can design one kind
Pilot's simulated training is solved the above problems with multi-angle rotary device.
The content of the invention
The purpose of the present invention is that and provides a kind of pilot's simulated training multi-angle in order to solve the above problems and revolve
Rotary device.
The present invention is achieved through the following technical solutions above-mentioned purpose：
A kind of pilot's simulated training multi-angle rotary device, including base, the base upper end are provided with rotating disk, institute
State rotating disk upper end and be provided with angle demodulator, the angle demodulator side offers angular adjustment groove, the angle demodulator
The back side, which is provided with stepper motor, the angle demodulator, is provided with angular adjustment disk, and the angular adjustment disk upper end is provided with
Angular adjustment bar, the angular adjustment bar upper end is provided with training seat, the base inside bottom surface and is provided with electric rotating machine
And thrust bearing, the electric rotating machine upper end is provided with gear, and the gear includes driving gear and driven gear, the thrust
Bearing upper end is provided with support column, and the support column upper end is fixedly connected with the angle demodulator.
It is preferred that, the rotating disk is fixedly mounted on angle demodulator side lower end；Wherein, the disk lower surface with
The base upper surface is in contact.
It is preferred that, the thrust bearing is fixedly mounted in the middle part of the base inside bottom surface；The support column lower end and institute
State thrust bearing inner ring to be fixedly connected, upper end in the middle part of the angle demodulator lower surface then with being fixedly connected；The driven gear
It is fixedly mounted on support column side upper end；Wherein, the driven gear upper surface is consolidated with the angle demodulator lower surface
Fixed connection.
It is preferred that, the electric rotating machine is fixedly mounted on the base inside bottom surface edge；The driving gear is fixed
On the output shaft of the electric rotating machine；Wherein, the driving gear is connected with driven gear engagement.
It is preferred that, the stepper motor is fixedly mounted in the middle part of the angle demodulator back side, and its output shaft extend into institute
State inside angle demodulator and be fixedly connected with the angular adjustment disk back side.
It is preferred that, the angular adjustment disk is a cylindrical structural；The angular adjustment bar lower end and the angular adjustment
Disk extrados is fixedly connected, and upper end is fixedly connected through the angular adjustment groove with the training seat.
It is preferred that, it is provided with safety belt on the training seat.
The beneficial effects of the present invention are：The present invention is used to drive the angle demodulator in water using the electric rotating machine
Rotated in plane, meanwhile, drive the training seat around the angle demodulator in perpendicular using the stepper motor
Interior rotation adjustment angle, so that the multi-angle rotary regulation of the training seat is realized, compared to traditional whole pilot of use
Simulation trainer rotates to drive the mode of the training seat multi-angle rotary to compare, and corresponding speed is fast, and flexible movements are changeable,
And angle adjustment scope is big, easy to operate, practicality is good.
Brief description of the drawings
Fig. 1 is a kind of front view of pilot's simulated training multi-angle rotary device of the invention；
Fig. 2 is a kind of side view of pilot's simulated training multi-angle rotary device of the invention；
Fig. 3 is a kind of cut-away view of pilot's simulated training multi-angle rotary device of the invention.
Wherein：1st, base；2nd, rotating disk；3rd, angle demodulator；4th, angular adjustment groove；5th, stepper motor；6th, angular adjustment bar；
7th, seat is trained；8th, safety belt；9th, angular adjustment disk；10th, driven gear；11st, support column；12nd, thrust bearing；13rd, electric rotating
Machine；14th, driving gear.
Embodiment
The invention will be further described below in conjunction with the accompanying drawings：
As shown in Figure 1-Figure 3, a kind of pilot's simulated training multi-angle rotary device, including base 1, the upper end of base 1
Rotating disk 2 is provided with, the upper end of rotating disk 2 is provided with angle demodulator 3, and angle demodulator 3 is used for stepper motor 5 and drives angular adjustment disk
9 rotate in angle demodulator 3, and the side of angle demodulator 3 offers angular adjustment groove 4, and angular adjustment groove 4 is used for angular adjustment
Bar 6 rotates the angle orientation of adjusting training seat 7 around angular adjustment disk 9, and the back side of angle demodulator 3 is provided with stepper motor 5, walks
Stepper motor 5 is used to drive angular adjustment disk 9 to rotate, and angular adjustment disk 9 is provided with angle demodulator 3, angular adjustment disk 9 is used for
Fixed angle adjusting rod 6 is installed, the upper end of angular adjustment disk 9 is provided with angular adjustment bar 6, and angular adjustment bar 6 is used to support fixation
Training seat 7 simultaneously drives training seat 7 to be rotated around angular adjustment disk 9, and the upper end of angular adjustment bar 6 is provided with training seat 7, base
Electric rotating machine 13 and thrust bearing 12 are provided with 1 inside bottom surface, electric rotating machine 13 is used to drive angle demodulator 3 in horizontal plane
Interior rotation, meanwhile, stepper motor 5 drives training seat 7 to rotate adjustment angle in perpendicular around angle demodulator 3, so that
The multi-angle rotary regulation of training seat 7 is realized, instruction driven using the rotation of whole pilot's simulation trainer compared to traditional
The mode for practicing the multi-angle rotary of seat 7 is compared, and corresponding speed is fast, and flexible movements are changeable, and angle adjustment scope is big, operation letter
Just, practicality is good, and the upper end of electric rotating machine 13 is provided with gear, and gear includes driving gear 14 and driven gear 10, electric rotating machine
13 drive driving gears 14 rotate, and the rotation of driving gear 14 drives driven gear 10 to rotate, and the rotation of driven gear 10 drives angle
Adjuster 3 is rotated, and the upper end of thrust bearing 12 is provided with support column 11, and the upper end of support column 11 is fixedly connected with angle demodulator 3.
In order to further improve the practicality of pilot's simulated training multi-angle rotary device, rotating disk 2 is fixedly mounted on
The side lower end of angle demodulator 3；Wherein, the lower surface of rotating disk 2 is in contact with the upper surface of base 1, and thrust bearing 12 is fixedly mounted on
In the middle part of the inside bottom surface of base 1；The lower end of support column 11 is fixedly connected with the inner ring of thrust bearing 12, upper end then with angle demodulator 3
Surface middle part is fixedly connected；Driven gear 10 is fixedly mounted on the side upper end of support column 11；Wherein, the upper surface of driven gear 10 with
The lower surface of angle demodulator 3 is fixedly connected, and electric rotating machine 13 is fixedly mounted on the inside bottom surface edge of base 1；Driving gear 14
On the output shaft for being fixedly mounted on electric rotating machine 13；Wherein, driving gear 14 is connected with the engagement of driven gear 10, stepper motor 5
It is fixedly mounted in the middle part of the back side of angle demodulator 3, its output shaft extend into the inside of angle demodulator 3 and carried on the back with angular adjustment disk 9
Face is fixedly connected, and angular adjustment disk 9 is a cylindrical structural；The lower end of angular adjustment bar 6 is fixed with the extrados of angular adjustment disk 9 to be connected
Connect, upper end is fixedly connected through angular adjustment groove 4 with training seat 7, safety belt 8 is provided with training seat 7.
The general principle and basic structure of the present invention has been shown and described above.It should be understood by those skilled in the art that,
The present invention is not limited to the above embodiments, merely illustrating the principles of the invention described in above-described embodiment and specification,
Without departing from the spirit and scope, various changes and modifications of the present invention are possible, and these changes and improvements all fall
Enter in scope of the claimed invention.The claimed scope of the invention is defined by appended claims and its effect thing.
Claims (7)
1. a kind of pilot's simulated training multi-angle rotary device, including base, it is characterised in that：The base upper end is set
There is rotating disk, the rotating disk upper end is provided with angle demodulator, and the angle demodulator side offers angular adjustment groove, the angle
The degree adjuster back side, which is provided with stepper motor, the angle demodulator, is provided with angular adjustment disk, on the angular adjustment disk
End is provided with angular adjustment bar, and the angular adjustment bar upper end is provided with training seat, the base inside bottom surface and is provided with
Electric rotating machine and thrust bearing, the electric rotating machine upper end are provided with gear, and the gear includes driving gear and driven gear,
The thrust bearing upper end is provided with support column, and the support column upper end is fixedly connected with the angle demodulator.
2. a kind of pilot's simulated training multi-angle rotary device according to claim 1, it is characterised in that：Described turn
Disk is fixedly mounted on angle demodulator side lower end；Wherein, the disk lower surface is in contact with the base upper surface.
3. a kind of pilot's simulated training multi-angle rotary device according to claim 1, it is characterised in that：It is described to stop
Thrust bearing is fixedly mounted in the middle part of the base inside bottom surface；The support column lower end is fixed with the thrust bearing inner ring to be connected
Connect, upper end in the middle part of the angle demodulator lower surface then with being fixedly connected；The driven gear is fixedly mounted on the support column
Side upper end；Wherein, the driven gear upper surface is fixedly connected with the angle demodulator lower surface.
4. a kind of pilot's simulated training multi-angle rotary device according to claim 1, it is characterised in that：The rotation
Rotating motor is fixedly mounted on the base inside bottom surface edge；The driving gear is fixedly mounted on the defeated of the electric rotating machine
On shaft；Wherein, the driving gear is connected with driven gear engagement.
5. a kind of pilot's simulated training multi-angle rotary device according to claim 1, it is characterised in that：The step
Stepper motor is fixedly mounted in the middle part of the angle demodulator back side, its output shaft extend into inside the angle demodulator and with institute
The angular adjustment disk back side is stated to be fixedly connected.
6. a kind of pilot's simulated training multi-angle rotary device according to claim 1, it is characterised in that：The angle
Degree adjustment disk is a cylindrical structural；The angular adjustment bar lower end is fixedly connected with the angular adjustment disk extrados, upper end
It is fixedly connected through the angular adjustment groove with the training seat.
7. a kind of pilot's simulated training multi-angle rotary device according to claim 1, it is characterised in that：The instruction
Practice and be provided with safety belt on seat.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710729944.6A CN107293185A (en) | 2017-08-23 | 2017-08-23 | A kind of pilot's simulated training multi-angle rotary device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710729944.6A CN107293185A (en) | 2017-08-23 | 2017-08-23 | A kind of pilot's simulated training multi-angle rotary device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107293185A true CN107293185A (en) | 2017-10-24 |
Family
ID=60106402
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710729944.6A Pending CN107293185A (en) | 2017-08-23 | 2017-08-23 | A kind of pilot's simulated training multi-angle rotary device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107293185A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107862938A (en) * | 2017-12-27 | 2018-03-30 | 北京夏商科技有限公司 | A kind of rotary seat trainer |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2009102286A2 (en) * | 2008-02-11 | 2009-08-20 | Orkun Aktas | The method that gives the feeling of fyling to the users and imaginary studio developed for this method |
| CN105185189A (en) * | 2015-10-16 | 2015-12-23 | 上海电机学院 | Flight simulation platform |
| CN105652684A (en) * | 2014-11-13 | 2016-06-08 | 北京航天计量测试技术研究所 | Novel large-size four-freedom attitude simulation structure |
| CN206039947U (en) * | 2016-05-20 | 2017-03-22 | 钟君城 | Initiative control platform about VR |
| CN206115768U (en) * | 2016-07-07 | 2017-04-19 | 上海源荀电子技术有限公司 | Modularization simulation passenger cabin device |
| CN106774920A (en) * | 2016-12-27 | 2017-05-31 | 李翔 | A kind of controllable coordinated movement of various economic factors for virtual reality perceives seat |
| CN106902514A (en) * | 2017-03-20 | 2017-06-30 | 歌尔科技有限公司 | Dynamic simulating device and its control method and control device |
| CN106943744A (en) * | 2017-03-20 | 2017-07-14 | 歌尔科技有限公司 | Dynamic simulating device and its control method and control device |
-
2017
- 2017-08-23 CN CN201710729944.6A patent/CN107293185A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2009102286A2 (en) * | 2008-02-11 | 2009-08-20 | Orkun Aktas | The method that gives the feeling of fyling to the users and imaginary studio developed for this method |
| CN105652684A (en) * | 2014-11-13 | 2016-06-08 | 北京航天计量测试技术研究所 | Novel large-size four-freedom attitude simulation structure |
| CN105185189A (en) * | 2015-10-16 | 2015-12-23 | 上海电机学院 | Flight simulation platform |
| CN206039947U (en) * | 2016-05-20 | 2017-03-22 | 钟君城 | Initiative control platform about VR |
| CN206115768U (en) * | 2016-07-07 | 2017-04-19 | 上海源荀电子技术有限公司 | Modularization simulation passenger cabin device |
| CN106774920A (en) * | 2016-12-27 | 2017-05-31 | 李翔 | A kind of controllable coordinated movement of various economic factors for virtual reality perceives seat |
| CN106902514A (en) * | 2017-03-20 | 2017-06-30 | 歌尔科技有限公司 | Dynamic simulating device and its control method and control device |
| CN106943744A (en) * | 2017-03-20 | 2017-07-14 | 歌尔科技有限公司 | Dynamic simulating device and its control method and control device |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107862938A (en) * | 2017-12-27 | 2018-03-30 | 北京夏商科技有限公司 | A kind of rotary seat trainer |
| CN107862938B (en) * | 2017-12-27 | 2023-10-13 | 北京夏商科技有限公司 | Rotary seat training device |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN202887507U (en) | Simulative operation device of aircraft | |
| CN101633409B (en) | Bidirectional synchronous automatic turning flapping-wings | |
| CN107150804B (en) | Flapping wing aircraft with three-degree-of-freedom wings | |
| CN202855112U (en) | Motor-human sense simulation control system motor of helicopter | |
| CN106585984A (en) | Rolling and rotating ornithopter | |
| CN105691606B (en) | A kind of the unmanned plane device and control method in high cruise duration | |
| CN205428282U (en) | Autogyro simulator | |
| CN109760834B (en) | Science and education demonstration device for flapping wing aircraft | |
| CN104229138A (en) | Split differential tail wing control mechanism of flapping-wing micro air vehicle | |
| US2357481A (en) | Aircraft training apparatus | |
| CN111086634B (en) | Dragonfly-like double-flapping-wing micro aircraft | |
| CN108423173A (en) | One kind plunderring dynamic formula flapping wing aircraft device | |
| CN107293185A (en) | A kind of pilot's simulated training multi-angle rotary device | |
| CN107380428A (en) | Dish-style rotor craft | |
| CN106428524A (en) | Multi-rotor wing aircraft with free wing | |
| CN103991540A (en) | Conical rotary flapping wing aircraft | |
| CN203220761U (en) | Multi-rotor aircraft | |
| CN104002968A (en) | Small conical rotary flapping wing air vehicle | |
| CN103466064A (en) | Flap wing underwater and water surface propeller, navigator and propelling method | |
| CN203864996U (en) | Tapered rotating flapping wing air vehicle | |
| CN205948363U (en) | 360 degrees all -round high -speed dynamic simulation simulation equipment of triaxial | |
| CN108609176A (en) | A kind of coaxial air-sea aircraft of verting | |
| CN102013188B (en) | Centrifugal machine based flight simulation system and method thereof | |
| CN113539046A (en) | Device for simulating and demonstrating side effect of propeller type airplane | |
| CN107396058A (en) | A kind of special fly simulation training supervising device of space flight |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20171024 |