CN208350339U - A kind of multiple degrees of freedom debugging apparatus - Google Patents
A kind of multiple degrees of freedom debugging apparatus Download PDFInfo
- Publication number
- CN208350339U CN208350339U CN201820592646.7U CN201820592646U CN208350339U CN 208350339 U CN208350339 U CN 208350339U CN 201820592646 U CN201820592646 U CN 201820592646U CN 208350339 U CN208350339 U CN 208350339U
- Authority
- CN
- China
- Prior art keywords
- support
- stabilizer
- platform
- motor
- sun gear
- 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.)
- Expired - Fee Related
Links
Abstract
It includes: the first platform that the utility model, which provides multiple degrees of freedom debugging apparatus,；First stabilizer blade, the first stabilizer blade are fixedly connected with the first platform；Second stabilizer blade, the second stabilizer blade are fixedly connected with the first platform；First telescope support, the first telescope support are detachably connected by the first bolt and the first stabilizer blade；Second telescope support, the second telescope support are detachably connected by the second bolt and the second stabilizer blade；Bearing rod, bearing rod are fixedly connected with the first platform；Second platform, the second platform are connect by third bolt with the first telescope support, are connect by the 4th bolt with the second telescope support and are connect by attachment device with bearing rod；Support of motor, support of motor are fixedly installed on the second platform；Stabilizer support, stabilizer support are fixedly installed on the second platform；Motor, motor are set on support of motor；Stabilizer, stabilizer are set on stabilizer support, and stabilizer is connected by shaft coupling with motor；Speed changer, speed changer are connected with stabilizer.
Description
Technical field
The utility model relates to debug machinery field, in particular to multiple degrees of freedom debugging apparatus.
Background technique
Debugging apparatus is as a kind of large artificial instrument and equipment high-accuracy, application value is high, by mechanical technique, sensing
A variety of subject crossing joint research and developments such as detection technique, hydraulic technique, control instrument technical device and electrical technology form.At present
It is widely used in industry, military and Entertainment facility, as typical electromechanical integration equipment with various technologies
Its application value with development is improved just to be stepped up.Such as debugging apparatus experimental bench can be applied as a spatial movement mechanism
In the stability sighting system experiment of the military issue weapons such as airborne, vehicle-mounted and carrier-borne equipment, simulating vehicle, aviation and ship
Spatial movement state provides the vibration environment under very close real conditions for tested object, is studied with this condition
The performance study and technology of object are evaluated.In recent years, due to the extensive practical value and bright prospects of debugging apparatus, gradually draw
Play the research interest of domestic and international scientific research expert, universities and colleges.During vehicle, ship and other civil equipments develop, it is
Produce security performance components product (automobile gearbox, shipborne radar, mounting, the subsidiary engine equipment high compared with strong, precision
Deng), it requires to carry out model machine under the various environmental aspects of reality detection test repeatedly, the peace of product is verified with this
Full performance and movenent performance.But if a large amount of people can be consumed by carrying out repeated multiple times detection test under actual environment
Power, material resources and time, debugging apparatus is taken advantage of a situation generation with this condition.Debugging apparatus can be greatly lowered verification test at
This.
The information disclosed in the background technology section is intended only to increase the understanding to the general background of the utility model, and
It is not construed as recognizing or implying in any form that information composition is already known to those of ordinary skill in the art existing
Technology.
Utility model content
The purpose of this utility model is to provide multiple degrees of freedom debugging apparatus, thus the shortcomings that overcoming the prior art.
To achieve the above object, the utility model provides a kind of multiple degrees of freedom debugging apparatus, it is characterised in that: debugging dress
Setting includes: the first platform；First stabilizer blade, the first stabilizer blade are fixedly connected with the first platform；Second stabilizer blade, the second stabilizer blade and first flat
Platform is fixedly connected；First telescope support, the first telescope support are detachably connected by the first bolt and the first stabilizer blade；Second is flexible
Bracket, the second telescope support are detachably connected by the second bolt and the second stabilizer blade；Bearing rod, bearing rod are fixed with the first platform
Connection；Second platform, the second platform are connect by third bolt with the first telescope support, and the 4th bolt and the second flexible branch are passed through
Frame is connected and is connect by attachment device with bearing rod；Support of motor, support of motor are fixedly installed on the second platform；
Stabilizer support, stabilizer support are fixedly installed on the second platform；Motor, motor are set on support of motor；Surely
Determine device, stabilizer is set on stabilizer support, and stabilizer is connected by shaft coupling with motor；Speed changer, speed changer and steady
Determine device to be connected.
Preferably, in above-mentioned technical proposal, the first telescope support further includes the first height adjustment device, the first height adjustment
Device is set to the first telescope support bottom.
Preferably, in above-mentioned technical proposal, attachment device includes: the first main shaft, and attachment device passes through the first main shaft and holds
The connection of power bar；Second main shaft, the second main shaft is perpendicularly through the first main shaft, and the second main shaft can be freely rotated；Connecting plate,
Connecting plate is fixedly connected with the second main shaft, and the second platform is connect by connecting plate with bearing rod.
Preferably, in above-mentioned technical proposal, stabilizer includes: power input wheel axis, and power input wheel axis is by motor band
Turn is dynamic；The rotational motion of primary planet frame, power input wheel axis is exported by primary planet frame；Main sun gear, main sun gear is by main row
Carrier drives rotation；The rotational motion of secondary planet carrier, main sun gear is exported by secondary planet carrier；Output wheel, output wheel is by secondary
Grade planet carrier drives rotation；Support component, support component support output wheel by roller bearing.
Preferably, in above-mentioned technical proposal, stabilizer includes: power input wheel axis, and power input wheel axis is by motor band
Turn is dynamic；The rotational motion of primary planet frame, power input wheel axis is exported by primary planet frame；Main sun gear, main sun gear is by main row
Carrier drives rotation；The rotational motion of secondary planet carrier, main sun gear is exported by secondary planet carrier；Secondary sun gear, secondary is too
Sun wheel is driven by secondary planet carrier to be rotated；The rotation of ring gear, secondary sun gear is exported by ring gear；Output wheel, output wheel by
Ring gear drives rotation；Support component, support component support output wheel by roller bearing.
Preferably, in above-mentioned technical proposal, speed changer further include output external member, output external member for output power to
Test piece.
Preferably, in above-mentioned technical proposal, debugging apparatus further include: test device case, test device case is for accommodating the
One telescope support, the second telescope support and bearing rod.
Compared with prior art, the utility model has the following beneficial effects: retarder in the prior art is more heavy,
Structure is longer, and in order not to tie up the confined space on test device platform, test device in the prior art is generally withouyt subtracting
Fast device, generally there are following problems for this test device: the fluctuation of motor speed will be fully transmitted on speed changer, cause to become
Fast device output power fluctuates, this to fluctuate strong influence test result when carrying out precision measurement.The utility model
It is designed first by speed changer structure, the length and construction weight of speed changer is reduced, so the utility model realizes
Retarder is added between debugging apparatus motor and speed changer, solving test device in the prior art not can be carried out precision measurement
The problem of.
Detailed description of the invention
By reading the following detailed description of the preferred embodiment, various other advantages and benefits are common for this field
Technical staff will become clear.The drawings are only for the purpose of illustrating a preferred embodiment, and is not considered as practical to this
Novel limitation.And throughout the drawings, the same reference numbers will be used to refer to the same parts.In the accompanying drawings:
Fig. 1 is the structural schematic diagram of multiple degrees of freedom debugging apparatus according to the present utility model；
Fig. 2 is the structural schematic diagram of one embodiment of stabilizer according to the present utility model.
Specific embodiment
With reference to the accompanying drawing, specific embodiment of the present utility model is described in detail, it is to be understood that this is practical
Novel protection scope is not limited by the specific implementation.
Fig. 1 is the structural schematic diagram of multiple degrees of freedom debugging apparatus according to the present utility model.Debugging apparatus includes: first flat
Platform 101；First stabilizer blade 116, the first stabilizer blade 116 are fixedly connected with the first platform 101；Second stabilizer blade 121, the second stabilizer blade 121 with
First platform 101 is fixedly connected；First telescope support 113, the first telescope support 113 pass through the first bolt and the first stabilizer blade 116
It is detachably connected；Second telescope support 103, the second telescope support 103 are detachably connected by the second bolt with the second stabilizer blade 121
It connects；Bearing rod 118, bearing rod 118 are fixedly connected with the first platform 101；Second platform 104, the second platform 104 pass through third spiral shell
Bolt 112 is connect with the first telescope support 113, is connect by the 4th bolt 107 with the second telescope support 103 and is filled by connection
It sets and is connect with bearing rod 118；Support of motor 106, support of motor 106 are fixedly installed on the second platform 104；Stabilizer branch
Seat 110, stabilizer support 110 is fixedly installed on the second platform 104；Motor 105, motor 105 are set to motor branch
On seat 106；Stabilizer 109, stabilizer 109 are set to 110 on stabilizer support, stabilizer 109 by shaft coupling 108 with it is electronic
Machine 105 is connected；Speed changer 111, speed changer 111 are connected with stabilizer 109.First telescope support 113 further includes that the first height is adjusted
Regulating device 114, the first height adjustment device 114 are set to the first telescope support bottom.Attachment device includes: the first main shaft 117,
Attachment device is connect by the first main shaft 117 with bearing rod 118；Second main shaft 119, the second main shaft 119 is perpendicularly through first
Main shaft 117, and the second main shaft can be freely rotated；Connecting plate 120, connecting plate 120 are fixedly connected with the second main shaft 119, the
Two platforms are connect by connecting plate with bearing rod.
Fig. 2 is the structural schematic diagram of stabilizer according to the present utility model.Stabilizer includes: power input wheel axis 201, is moved
Power inputs wheel shaft 201 and drives rotation by motor；Primary planet frame 203, the rotational motion of power input wheel axis 201 is by primary planet frame
Output 203；Main sun gear 202, main sun gear 202 are driven by primary planet frame 203 and are rotated；Secondary planet carrier 208, main sun gear
202 rotational motion is exported by secondary planet carrier 208；Secondary sun gear 204, secondary sun gear 204 is by secondary 208 band of planet carrier
Turn is dynamic；The rotation of ring gear 211, secondary sun gear 204 is exported by ring gear 211；Output wheel 212, output wheel 212 is by internal tooth
Circle 211 drives rotation；Support component 214, support component 214 support output wheel 212 by roller bearing.The utility model it is steady
Determining device further includes brake assemblies 213 and end cap 206.As shown, the course of work of the stabilizer of the utility model are as follows: power
It inputs wheel shaft 201 and rotation is driven by motor；Power input wheel axis 201 then drives first gear 205 to rotate, first gear
205 are connected with primary planet frame 203, and subsequent main sun gear 202 is driven by primary planet frame 203 to be rotated；Main sun gear 202 drives again
The rotation of two gears 207, second gear 207 are connected with secondary planet carrier 208, and the rotational motion of main sun gear 202 is by secondary planet
Frame 208 exports；Secondary sun gear 204 is driven by secondary planet carrier 208 and is rotated；Secondary sun gear 204 drives third gear 209 again
Rotation, third gear 209 drive ring gear 211 to rotate；Output wheel 212, output wheel 212 are driven by ring gear 211 and are rotated.
Stabilizer structure according to fig. 2, the utility model also proposed a kind of more simple stabilizer structure, this knot
Structure can be simply transformed by the structure of Fig. 2, therefore without separately shown structural schematic diagram.The stabilizer packet of this simplification
Include: power input wheel axis, power input wheel axis are driven by motor and are rotated；Primary planet frame, the rotational motion of power input wheel axis
It is exported by primary planet frame；Main sun gear, main sun gear are driven by primary planet frame and are rotated；Secondary planet carrier, the rotation of main sun gear
Movement is exported by secondary planet carrier；Output wheel, output wheel are driven by secondary planet carrier and are rotated；Support component, support component pass through
Roller bearing supports output wheel.Since the stabilizer structure of the utility model is compact, length is smaller compared with short weight amount, so this is practical
It is novel successfully by stabilizer in conjunction with test device.
The description of the aforementioned specific exemplary embodiment to the utility model is in order to illustrate and illustration purpose.These
Description is not wishing to for the utility model to be limited to disclosed precise forms, and it will be apparent that according to the above instruction, can carry out
It is many to change and change.The purpose of selecting and describing the exemplary embodiment is that explaining the specific principle of the utility model
And its practical application, so that those skilled in the art can be realized and utilize a variety of different examples of the utility model
Property embodiment and various chooses and changes.The scope of the utility model is intended to by claims and its waits similar shapes
Formula is limited.
Claims (7)
1. a kind of multiple degrees of freedom debugging apparatus, it is characterised in that: the debugging apparatus includes:
First platform；
First stabilizer blade, first stabilizer blade are fixedly connected with first platform；
Second stabilizer blade, second stabilizer blade are fixedly connected with first platform；
First telescope support, first telescope support are detachably connected by the first bolt and first stabilizer blade；
Second telescope support, second telescope support are detachably connected by the second bolt and second stabilizer blade；
Bearing rod, the bearing rod are fixedly connected with first platform；
Second platform, second platform are connect by third bolt with first telescope support, and the 4th bolt and institute are passed through
The second telescope support is stated to connect and connect by attachment device with the bearing rod；
Support of motor, the support of motor are fixedly installed on second platform；
Stabilizer support, the stabilizer support are fixedly installed on second platform；
Motor, the motor are set on the support of motor；
Stabilizer, the stabilizer are set on the stabilizer support, and the stabilizer passes through shaft coupling and the motor
It is connected；
Speed changer, the speed changer are connected with the stabilizer.
2. multiple degrees of freedom debugging apparatus as described in claim 1, it is characterised in that: first telescope support further includes first
Height adjustment device, first height adjustment device are set to first telescope support bottom.
3. multiple degrees of freedom debugging apparatus as described in claim 1, it is characterised in that: the attachment device includes:
First main shaft, the attachment device are connect by first main shaft with the bearing rod；
Second main shaft, second main shaft is perpendicularly through first main shaft, and second main shaft can be freely rotated；
Connecting plate, the connecting plate are fixedly connected with second main shaft, second platform by the connecting plate with it is described
Bearing rod connection.
4. multiple degrees of freedom debugging apparatus as described in claim 1, it is characterised in that: the stabilizer includes:
Power input wheel axis, the power input wheel axis are driven by the motor and are rotated；
The rotational motion of primary planet frame, the power input wheel axis is exported by the primary planet frame；
Main sun gear, the main sun gear are driven by the primary planet frame and are rotated；
The rotational motion of secondary planet carrier, the main sun gear is exported by the secondary planet carrier；
Output wheel, the output wheel drive rotation by the secondary planet carrier；
Support component, the support component support the output wheel by roller bearing.
5. multiple degrees of freedom debugging apparatus as described in claim 1, it is characterised in that: the stabilizer includes:
Power input wheel axis, the power input wheel axis are driven by the motor and are rotated；
The rotational motion of primary planet frame, the power input wheel axis is exported by the primary planet frame；
Main sun gear, the main sun gear are driven by the primary planet frame and are rotated；
The rotational motion of secondary planet carrier, the main sun gear is exported by the secondary planet carrier；
Secondary sun gear, the secondary sun gear drive rotation by the secondary planet carrier；
The rotation of ring gear, the secondary sun gear is exported by the ring gear；
Output wheel, the output wheel are driven by the ring gear and are rotated；
Support component, the support component support the output wheel by roller bearing.
6. multiple degrees of freedom debugging apparatus as described in claim 1, it is characterised in that: the speed changer further includes output external member,
The output external member is for outputing power to workpiece to be tested.
7. multiple degrees of freedom debugging apparatus as described in claim 1, it is characterised in that: the debugging apparatus further include:
Test device case, the test device case is for accommodating first telescope support, second telescope support and institute
State bearing rod.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820592646.7U CN208350339U (en) | 2018-04-25 | 2018-04-25 | A kind of multiple degrees of freedom debugging apparatus |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820592646.7U CN208350339U (en) | 2018-04-25 | 2018-04-25 | A kind of multiple degrees of freedom debugging apparatus |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208350339U true CN208350339U (en) | 2019-01-08 |
Family
ID=64887196
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820592646.7U Expired - Fee Related CN208350339U (en) | 2018-04-25 | 2018-04-25 | A kind of multiple degrees of freedom debugging apparatus |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208350339U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108414206A (en) * | 2018-04-25 | 2018-08-17 | 北京光宇之勋科技有限公司 | A kind of multiple degrees of freedom debugging apparatus |
-
2018
- 2018-04-25 CN CN201820592646.7U patent/CN208350339U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108414206A (en) * | 2018-04-25 | 2018-08-17 | 北京光宇之勋科技有限公司 | A kind of multiple degrees of freedom debugging apparatus |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN203858778U (en) | Steering engine load simulation device based on electric loading | |
| CN105652684B (en) | A kind of novel large four-degree-of-freedom attitude-simulating simulation architecture | |
| CN102538598B (en) | A kind of motion simulation analogue system of infrared target | |
| CN104155538B (en) | Comprehensive experiment testing system for small satellite antenna | |
| CN102156047B (en) | Loading simulation device for test bed of wind turbine | |
| CN103308325A (en) | Driving system semi-physical simulation platform of electric automobile | |
| CN205352219U (en) | Three -dimensional test turntable of guided missile | |
| CN108444706B (en) | Multi-parameter mass property testboard based on spherical surface air-bearing | |
| CN105652688A (en) | Steering system real-time hardware in-the-loop simulation platform and test method thereof | |
| CN102998082A (en) | Device for wind tunnel dynamic derivative pitch vibration test | |
| CN208350339U (en) | A kind of multiple degrees of freedom debugging apparatus | |
| CN112525460B (en) | Test method based on multi-axis swinging and vibration composite test platform | |
| CN204256060U (en) | A kind of swing rocks electrostatic testing table | |
| CN110207980A (en) | Multiple-input and multiple-output gear train assembly test of Vibration platform and test method | |
| CN109540452A (en) | A kind of rotating missile arrow Three Degree Of Freedom angular movement simulation test device | |
| CN103335831A (en) | Brake electrical inertia simulating test table and electrical inertia simulation control method thereof | |
| CN114295317A (en) | Unfolding and folding rudder torque loading test system, method and medium | |
| CN103645055A (en) | Test platform for simulating dynamic environments | |
| CN109307610A (en) | Rudder system load simulation test device | |
| CN110132587A (en) | A kind of Electric Motor Wheel testing stand based on real-time simulation tool and load simulation system | |
| CN109823566A (en) | A kind of vertically taking off and landing flyer flight control system test platform | |
| CN103033209A (en) | Three-dimensional motion testing device | |
| CN102141463A (en) | Slewing mechanism of swing test bench | |
| CN104595475A (en) | Electromechanical hybrid type precise transmission system and control method thereof | |
| CN108414206A (en) | A kind of multiple degrees of freedom debugging apparatus |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20190108 Termination date: 20190425 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |