CN205745900U - Five revolving stages - Google Patents
Five revolving stages Download PDFInfo
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- CN205745900U CN205745900U CN201620563038.4U CN201620563038U CN205745900U CN 205745900 U CN205745900 U CN 205745900U CN 201620563038 U CN201620563038 U CN 201620563038U CN 205745900 U CN205745900 U CN 205745900U
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- rotating disk
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- 238000005096 rolling process Methods 0.000 claims abstract description 51
- 230000001960 triggered effect Effects 0.000 claims description 5
- 238000005553 drilling Methods 0.000 claims description 3
- 238000010276 construction Methods 0.000 claims 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims 1
- 238000005259 measurement Methods 0.000 description 8
- 238000011161 development Methods 0.000 description 5
- 230000018109 developmental process Effects 0.000 description 5
- 238000013461 design Methods 0.000 description 4
- 230000033001 locomotion Effects 0.000 description 4
- 238000010586 diagram Methods 0.000 description 3
- 238000006073 displacement reaction Methods 0.000 description 3
- 230000005611 electricity Effects 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 3
- 238000012360 testing method Methods 0.000 description 3
- 238000000034 method Methods 0.000 description 2
- 238000011160 research Methods 0.000 description 2
- 230000002547 anomalous effect Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 230000008595 infiltration Effects 0.000 description 1
- 238000001764 infiltration Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 230000002035 prolonged effect Effects 0.000 description 1
- 238000012827 research and development Methods 0.000 description 1
- 230000033772 system development Effects 0.000 description 1
- 238000005303 weighing Methods 0.000 description 1
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Abstract
The utility model discloses a five revolving stages, lower position base including the bottom, lower position base top is equipped with takes radian rolling guide, the top of taking radian rolling guide is equipped with azimuth axis carousel, azimuth axis carousel slides along taking radian rolling guide, azimuth axis carousel top is equipped with the pitch-axis, the pitch-axis rotates in vertical plane along its central axis, the pitch-axis carries out the horizontal rotation along with azimuth axis carousel, the pitch-axis top is equipped with horizontally Y axle rolling guide, Y axle rolling guide top is equipped with the periscope axis body of vertical direction, the periscope axis body slides along Y axle rolling guide. The utility model discloses a revolving stage is at survey angle shaft, azimuth axis, every single move axle, horizontal Y axle and periscope epaxial removal or rotation to each axle can be according to setting for the removal of speed constant speed or rotation.
Description
Technical field
This utility model relates to a kind of turntable, specifically, relates to a kind of to realize multi-shaft interlocked compound five axles
Turntable.
Background technology
Turntable is a kind of important ground checkout equipment, identifies for inertial navigation system and inertia original paper, demarcates, and
Simulated flight device attitude motion.Artificial rotary table and inertia test table can be divided into according to purposes.Between mesh the first two classification, infiltration is more
Sending out notable, boundary is increasingly upper moves.
In the world, due to inertial guidance techniques generally weighing by the country of advanced technology in the world and developing country
Depending on, so countries in the world state has all put into substantial amounts of fund and manpower is engaged in the development of turntable.
The turntable development of China in these years achieves certain achievement, and the most in recent years, the development of turntable obtains
The biggest development.At present, domestic also have a lot of research institution and colleges and universities being engaged in the research and development of turntable.China is in 20 generation
Record the independent research sixties and manufactured First hydraulic pressure High Precision Flight Simulator, for China's early stage flying vehicles control and guidance system
Development be made that huge contribution.After entering the eighties, China has been incorporated into digital control in turning table control, real with software
Having showed complex control rule, parameter adjustment is also convenient than analog controller, is researched and developed by the turntable of China and has brought one into newly
Epoch.Nineteen ninety, Air China 303 has been succeeded in developing SGT 1 type three axle inertial navigation test table, and this is China's First meter
The high accuracy three axes inertial navigation test table that calculation machine controls.Since entering the nineties, the development of turntable enters numeral and wanting of simulating
Asking more and more higher, the design of turntable and adjusting just is had higher requirement by this.Domestic also have developed many variety classeses
Turntable, and three-axle table can not meet our demand in the actual application of turntable, it would be desirable to one realizes multiaxis
The turntable controlled.
Summary of the invention
In order to overcome the deficiency of existing technology, this utility model provides a kind of five-axis flight table.
Technical solutions of the utility model are as described below:
A kind of five-axis flight table, it is characterised in that include the lower azimuth base of bottom,
Described lower azimuth base is arranged over the band radian rolling guide of horizontal direction, and described band radian rolling guide drives
Described five-axis flight table rotates along angle measurement axle, the azimuth axis rotating disk being arranged over horizontally rotating of described band radian rolling guide,
Five-axis flight table described in described azimuth axis driven by rotary disc rotates along azimuth axis, and described azimuth axis rotating disk rolls along described band radian and leads
Rail slides, and described azimuth axis rotating disk is arranged over pitch axis, and described pitch axis rotates in perpendicular along its central shaft,
Described pitch axis horizontally rotates along with described azimuth axis rotating disk, and described pitch axis is arranged over the Y-axis rolling guide of level,
Described Y-axis rolling guide rotates in perpendicular along with described pitch axis, and described Y-axis rolling guide guides described five-axis flight table
Moving in the Y-axis of level, described Y-axis rolling guide is arranged over the latent prestige axis body of vertical direction, described latent prestige axis body along
Described Y-axis rolling guide slides.
Further, described lower azimuth base is extendible base.
Further, described band radian rolling guide is the globoidal structure of middle concave downward.
Further, the two ends of described band radian rolling guide, the two ends of described Y-axis rolling guide and described latent prestige axle
The base plate of body is equipped with exception-triggered switch.
Further, described pitch axis includes Circumflex branch support structure body and is located at described Circumflex branch this body side surface of support structure
Circumflex branch support structure rotating disk, described Circumflex branch support structure body be arranged over platform.
Further, described Y-axis rolling guide is fixed on above described platform.
Further, described lower azimuth base is provided with angulation motors, azimuth-drive motor and latent prestige motor, described angle measurement
Motor, described azimuth-drive motor and described latent prestige motor respectively with described band radian rolling guide, described azimuth axis rotating disk and
Described latent prestige axis body connects, and the inside of described Circumflex branch support structure body is provided with horizontal Y-motor and pitching motor, described horizontal Y
Motor and described pitching motor are connected with described Y-axis rolling guide and described Circumflex branch support structure rotating disk respectively.
Further, described angulation motors, described azimuth-drive motor, described latent prestige motor, described horizontal Y-motor and described in bow
Face upward the output shaft of motor and connect the reductor corresponding with each motor respectively, and described angulation motors, described azimuth-drive motor, described
The latent inside hoping motor, described horizontal Y-motor and described pitching motor is respectively equipped with and the coding of electric drilling match each described
Device.Described encoder is integrated in the described motor internal of correspondence, and it includes encoder feedback system and measurement, control equipment.
According to this utility model of such scheme, it has the beneficial effects that, this utility model can drive contained object surveying
Angle axle, azimuth axis, pitch axis, horizontal Y-axis and the latent movement hoped on axle or rotation, and each axle can move by setting speed constant speed
Move or rotate, automatically interrupt during with exception-triggered switch in order to realize anomalous rotation rotating, it is to avoid system failure.
Accompanying drawing explanation
Fig. 1 is the schematic diagram that this utility model five axle rotates；
Fig. 2 is structural representation of the present utility model；
Fig. 3 is the schematic diagram of this utility model single shaft control system；
Fig. 4 is the schematic diagram of this utility model overall system control.
In the drawings, 11, angle measurement axle；12, azimuth axis；13, pitch axis；14, horizontal Y-axis；15, latent prestige axle；21, at the bottom of lower orientation
Seat；22, band radian rolling guide；23, azimuth axis rotating disk；24, Circumflex branch support structure rotating disk；25, Y-axis rolling guide；26, latent prestige
Axis body.
Detailed description of the invention
Below in conjunction with the accompanying drawings and this utility model is conducted further description by embodiment:
As shown in Figure 1-2, a kind of five-axis flight table, including the extendible lower azimuth base 21 of bottom.
Lower azimuth base 21 is arranged over the band radian rolling guide 22 of horizontal direction, and band radian rolling guide 22 is middle
The globoidal structure of concave downward.Band radian rolling guide 22 drives five-axis flight table to rotate along angle measurement axle 11, band radian rolling guide
21 are connected with angulation motors.
With the azimuth axis rotating disk 23 being arranged over horizontally rotating of radian rolling guide 22, azimuth axis rotating disk 23 drives five
Axle turntable rotates along azimuth axis 12, and azimuth axis rotating disk 23 slides along band radian rolling guide 22, azimuth axis rotating disk 23 connection side
Position motor.
Azimuth axis rotating disk 23 is arranged over pitch axis 13, and pitch axis 13 rotates in perpendicular along its central shaft,
Pitch axis 13 horizontally rotates along with azimuth axis 12 rotating disk, and pitch axis 13 includes Circumflex branch support structure body and is located at Circumflex branch
The Circumflex branch support structure rotating disk 24 of this body side surface of support structure, Circumflex branch support structure body be arranged over platform.Convolution supports knot
Structure rotating disk 24 is connected with pitching motor.
Platform is arranged over the Y-axis rolling guide 25 of level, and Y-axis rolling guide 25 guides five-axis flight table in horizontal Y-axis 14
Upper movement, Y-axis rolling guide 25 rotates in perpendicular with pitch axis 13, and Y-axis rolling guide 25 connects y-axis motor.
Y-axis rolling guide 25 is arranged over the latent prestige axis body 26 of vertical direction, latent hope axis body 26 make five-axis flight table along
The latent movement hoping axle 15 carry out vertical direction, latent prestige axis body 26 slides along Y-axis rolling guide 25.Latent prestige axis body 26 hopes electricity with latent
Machine connects.
In the present embodiment, angulation motors, azimuth-drive motor and latent prestige motor are located in lower azimuth base 21, horizontal Y electricity
Machine and pitching motor are located at the inside of Circumflex branch support structure body.Angulation motors, azimuth-drive motor, latent hope motor, horizontal Y-motor with
And the output shaft of pitching motor connects the reductor corresponding with each motor, and angulation motors, azimuth-drive motor, latent prestige electricity respectively
The inside of machine, horizontal Y-motor and pitching motor is respectively equipped with the encoder with each electric drilling match.Encoder is integrated in correspondence
Motor internal, it includes encoder feedback system and measurement, control equipment.
Two ends, the two ends of Y-axis rolling guide 25 and the latent base plate hoping axis body 26 with radian rolling guide 22 are equipped with
Exception-triggered switchs.
As it is shown on figure 3, multiple axles of rotating platform control system are high accuracy servo system, rotating platform control system is to multiple axles
Control be separate, control principle is essentially identical.Principle of the present utility model is:
Computer sends I/O control signal to positioning control module, and alternating current torque motor drives under locating module control,
Via driving stage body displacement after reductor governing speed, encoder (position feedback elements) is the angular displacement of stage body or straight-line displacement
Being converted into the signal of telecommunication, be sent to positioning control module, positioning control module accepts signal monitoring stage body turned position, when turntable turns
When moving beyond bound position, positioning control module sends signal, connects protection and the warning circuit of turntable, and turntable proceeds to protection
Action, system break rotates.
Concrete, as shown in Figure 4, computer control system controls motor and drives, and drives motor to use AC servo motor,
And coordinating a high accuracy worm decelerating machine, position feedback elements uses photoelectric encoder.Photoelectric encoder can feed back respective shaft
Positional information, in order to realize triggering when turned position exceedes bound limit switch, position feedback elements selection photoelectric encoder
By the position control that suitable design is countershaft.
At angle measurement axle 11(X axle), horizontal Y-axis 14, latent hope axle 15(Z axle) to there being exception-triggered to switch, in order to realize exception
Automatically interrupt during rotation rotating, it is to avoid system failure.
In the present embodiment, arranging azimuth axis 12 upper limit position is 180 °, and lower position is-180 °, i.e. in level orientation
On can carry out 0-360 ° of rotation, the corresponding reductor speed reducing ratio of azimuth axis 12 is set to 789.33, and the azimuth-drive motor speed of service regulates
It is 15000.When azimuth axis 12 corner exceedes bound position, azimuth encoder sends a signal to locating module, and limit switch closes
Closing, connect protection and the warning circuit of turntable, turntable proceeds to protection act, and system break rotates, it is to avoid system failure.
Same, in the present embodiment, the anglec of rotation of pitch axis 13 is 0-90 ° of scope.
The motor of multi-axis turntable drives each axle to be Y at horizontal plane with certain speed after reductor slows down, Z-direction is moved
Dynamic, horizontal plane rotates and pitching rotates, and angle measurement axle 11 moves in the guide track of level orientation band radian rolling guide 21, turns
Platform azimuth axis 12 is azimuth base place horizontal plane 360 ° rotation under turntable, and turntable drives pitch axis 13 0-90 ° of direction pitching
Mobile, horizontal Y-axis 14 is prolonged horizontal Y-direction rolling guide and is moved forward and backward, and latent prestige axle 15 is lower mobile in the Z-axis direction.
It should be appreciated that for those of ordinary skills, can be improved according to the above description or be converted,
And all these modifications and variations all should belong to the protection domain of this utility model claims.
Above in conjunction with accompanying drawing, this utility model patent is carried out exemplary description, it is clear that the reality of this utility model patent
Now it is not subject to the restrictions described above, as long as the method design that have employed this utility model patent is various with what technical scheme was carried out
Improve, or the most improved design by this utility model patent and technical scheme directly apply to other occasion, all in this reality
With in novel protection domain.
Claims (8)
1. a five-axis flight table, it is characterised in that include the lower azimuth base of bottom,
Described lower azimuth base is arranged over the band radian rolling guide of horizontal direction, and the top of described band radian rolling guide sets
Having the azimuth axis rotating disk that can horizontally rotate, described azimuth axis rotating disk slides along described band radian rolling guide, described azimuth axis
Rotating disk is arranged over pitch axis, and described pitch axis rotates in perpendicular along its central shaft, and described pitch axis is along with institute
Stating azimuth axis rotating disk to horizontally rotate, described pitch axis is arranged over the Y-axis rolling guide of level, described Y-axis rolling guide
Along with described pitch axis rotates in perpendicular, described Y-axis rolling guide is arranged over the latent prestige axis body of vertical direction, described
Latent prestige axis body slides along described Y-axis rolling guide.
Five-axis flight table the most according to claim 1, it is characterised in that described lower azimuth base is extendible base.
Five-axis flight table the most according to claim 1, it is characterised in that described band radian rolling guide is middle concave downward
Globoidal structure.
Five-axis flight table the most according to claim 1, it is characterised in that the two ends of described band radian rolling guide, described Y-axis
The two ends of rolling guide and the base plate of described latent prestige axis body are equipped with exception-triggered switch.
Five-axis flight table the most according to claim 1, it is characterised in that described pitch axis include Circumflex branch support structure body and
It is located at the Circumflex branch support structure rotating disk of described Circumflex branch this body side surface of support structure, being arranged over of described Circumflex branch support structure body
Platform.
Five-axis flight table the most according to claim 5, it is characterised in that described Y-axis rolling guide is fixing on the platform
Side.
Five-axis flight table the most according to claim 5, it is characterised in that be provided with angulation motors, side in described lower azimuth base
Position motor and latent hope motor, described angulation motors, described azimuth-drive motor and described latent prestige motor respectively with described band radian
Rolling guide, described azimuth axis rotating disk and described latent prestige axis body connect, and the inside of described Circumflex branch support structure body is provided with water
Flat Y-motor and pitching motor, described horizontal Y-motor and described pitching motor respectively with described Y-axis rolling guide and described convolution
Supporting construction rotating disk connects.
Five-axis flight table the most according to claim 1, it is characterised in that described angulation motors, described azimuth-drive motor, described latent
The output shaft hoping motor, described horizontal Y-motor and described pitching motor connects the reductor corresponding with each motor respectively, and
And described angulation motors, described azimuth-drive motor, described latent prestige motor, described horizontal Y-motor and the inside of described pitching motor
It is respectively equipped with and the encoder of electric drilling match each described.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620563038.4U CN205745900U (en) | 2016-06-12 | 2016-06-12 | Five revolving stages |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620563038.4U CN205745900U (en) | 2016-06-12 | 2016-06-12 | Five revolving stages |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205745900U true CN205745900U (en) | 2016-11-30 |
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ID=57360444
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620563038.4U Active CN205745900U (en) | 2016-06-12 | 2016-06-12 | Five revolving stages |
Country Status (1)
| Country | Link |
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| CN (1) | CN205745900U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111664749A (en) * | 2020-06-04 | 2020-09-15 | 九江精密测试技术研究所 | High-dynamic vertical five-axis electric turntable |
| CN112577523A (en) * | 2020-12-12 | 2021-03-30 | 江西洪都航空工业股份有限公司 | Adjustable inertial navigation test switching tool and adjusting and mounting method |
-
2016
- 2016-06-12 CN CN201620563038.4U patent/CN205745900U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111664749A (en) * | 2020-06-04 | 2020-09-15 | 九江精密测试技术研究所 | High-dynamic vertical five-axis electric turntable |
| CN112577523A (en) * | 2020-12-12 | 2021-03-30 | 江西洪都航空工业股份有限公司 | Adjustable inertial navigation test switching tool and adjusting and mounting method |
| CN112577523B (en) * | 2020-12-12 | 2023-10-03 | 江西洪都航空工业股份有限公司 | Adjustable inertial navigation test switching tool and adjusting and installing method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CP03 | Change of name, title or address | ||
| CP03 | Change of name, title or address |
Address after: 518000 a1709, No.17, North District, Fuquan new village, Sanlian community, Longhua street, Longhua District, Shenzhen City, Guangdong Province Patentee after: Xinyi Technology (Shenzhen) Co., Ltd Address before: 518000, Guangdong, Nanshan District, Shenzhen Nanhai Avenue, West Temple, northbound sunshine Huayi Building 1, 6B, 6C-27 Patentee before: SHENZHEN CITY FUXIN INFORMATION TECHNOLOGY Co.,Ltd. |