CN206068194U - Can Omni-mobile wing mounting platform - Google Patents
Can Omni-mobile wing mounting platform Download PDFInfo
- Publication number
- CN206068194U CN206068194U CN201620962873.5U CN201620962873U CN206068194U CN 206068194 U CN206068194 U CN 206068194U CN 201620962873 U CN201620962873 U CN 201620962873U CN 206068194 U CN206068194 U CN 206068194U
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- China
- Prior art keywords
- omni
- mobile
- wing
- mounting platform
- posture adjustment
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- Expired - Fee Related
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Abstract
This utility model belongs to wing mounting technique field, specifically related to it is a kind of can Omni-mobile wing mounting platform, including mobile device and positioning bracket system, positioning bracket system is set up in mobile device, mobile device includes mobile station and omni-directional wheel, located at the bottom of mobile station so that mobile station Omni-mobile, positioning bracket system is provided with bracket and posture adjustment localizer to omni-directional wheel, and posture adjustment localizer is located at the bottom of bracket to adjust the orientation of bracket.It is of the present utility model can Omni-mobile wing mounting platform, can Omni-mobile, automatic butt wing, high degree of automation.
Description
Technical field
This utility model belongs to wing mounting technique field, and in particular to it is a kind of can Omni-mobile wing mounting platform.
Background technology
Carrier structure is adopted when aircraft wing is installed at present, multiple-person cooperative work is needed, needs to adjust in real time according to installing
Whole wing attitude, finally completes wing installment work.This mounting means has inefficiency, to operator's demand
Greatly, working strength is big, installation quality existing defects the shortcomings of.
Utility model content
The purpose of this utility model be to provide it is a kind of can Omni-mobile wing mounting platform, can Omni-mobile, it is automatically right
Pick the wing, high degree of automation.
For achieving the above object, the technical scheme adopted by this utility model is：Including mobile device and positioning bracket dress
Put, positioning bracket system is set up in mobile device, mobile device includes mobile station and omni-directional wheel, and omni-directional wheel is located at mobile station
So that mobile station Omni-mobile, positioning bracket system is provided with bracket and posture adjustment localizer for bottom, and posture adjustment localizer is located at bracket
Bottom adjusting the orientation of bracket.
Preferably, the positioning bracket system also includes base, and, on base, pony sill is located at movement for posture adjustment localizer
In mobile station on device.
Preferably, the bracket is provided with wing fixation clamp.
Preferably, the quantity of the wing fixation clamp is two, and two wing fixation clamps are clinodiagonal located at support
Clamping to wing on frame.
Preferably, the quantity of the posture adjustment localizer is three, and three posture adjustment localizers are distributed in triangular shape on base,
Each posture adjustment localizer is respectively provided with the degree of freedom in tri- directions of X, Y, Z.
Preferably, the posture adjustment localizer is provided with strain gauge.
Preferably, the bottom of the base is provided with four legs with the stability of adjusting base.
Preferably, the mobile station is provided with laser scanner, and the quantity of laser scanner is two, two laser scannings
Instrument is clinodiagonal in mobile station.
After above-mentioned technical proposal, this utility model has the positive effect that：
(1) all directions of mobile device are capable of achieving by arranging four omni-directional wheels in the mobile device in this utility model
Mobile, radius of turn is 0, so as to the coarse positioning of position is carried out to positioning bracket system；
(2) accurate tune is capable of achieving by arranging 3 posture adjustment localizers on the positioning bracket system in this utility model
The posture adjustment localizer synchronization action of appearance, i.e., 3, can complete the actions such as lifting, the translation of wing, and 3 posture adjustment localizers are asynchronous dynamic
Make, the actions such as rotation, inclination and the rolling of wing can be completed, realize the action adjustment of 6 degree of freedom of wing, finally realize machine
The wing is accurately positioned, docks and installment work；
(3) what the present invention can effectively prevent wing forces assembling, it is ensured that the assembling quality of wing, and operator can be greatly reduced
The labor intensity of member, saves wing docking time, improves automaticity and docking efficiency.
Description of the drawings
Fig. 1 be it is of the present utility model can Omni-mobile wing mounting platform structure chart；
Fig. 2 is the mobile device structure chart in this utility model；
Fig. 3 is the positioning bracket system structure chart in this utility model.
Wherein：1st, mobile device, 11, mobile station, 12, omni-directional wheel, 13, laser scanner, 2, positioning bracket system, 21,
Bracket, 22, posture adjustment localizer, 23, base, 24, wing fixation clamp, 25, leg.
Specific embodiment
With reference to the accompanying drawings and detailed description this utility model is described in further detail.
In this utility model, unless otherwise clearly defined and limited, term " installation ", " being connected ", " connection ", " Gu
It is fixed " etc. term should broadly understood, it is for example, it may be fixedly connected, or be detachably connected or integral；Can be
It is mechanically connected, or electrically connects；Can be joined directly together, it is also possible to be indirectly connected to by intermediary, can be two
The connection of element internal or the interaction relationship of two elements.For the ordinary skill in the art, can basis
Concrete condition understands concrete meaning of the above-mentioned term in this utility model.
As Figure 1-3, be it is of the present utility model can Omni-mobile wing mounting platform, including mobile device 1 and fixed
Position bracket system 2, positioning bracket system 2 are set up in mobile device 1.
Mobile device 1 includes mobile station 11, omni-directional wheel 12 and laser scanner 13, and mobile station 11 is a vehicle frame shape, omnidirectional
Wheel 12 is four, and four omni-directional wheels 12 are located at the bottom of mobile station 11 so that 11 Omni-mobile of mobile station.Mobile station 11 it is oblique right
Angle is provided with two laser scanners 13, and laser scanner 13 can detect the barrier of surrounding, so that it is guaranteed that wing transhipment
During wing safety.
Positioning bracket system 2 includes bracket 21, posture adjustment localizer 22, base 23, wing fixation clamp 24 and leg 25, base
23 is a support body, and during use, base 23 is erected in mobile station 11.The quantity of posture adjustment localizer 22 is three, three posture adjustment positioning
Device 22 is distributed in triangular shape on base 23, and each posture adjustment localizer 22 is respectively provided with the degree of freedom in tri- directions of X, Y, Z, can be with complete
The actions such as rotation, inclination and rolling into wing, realize the action adjustment of 6 degree of freedom of wing, finally realize the accurate of wing
Positioning, docking and installment work.Strain gauge is equipped with each posture adjustment localizer 22, the strain gauge can perceptron
With the presence or absence of the problems such as forcing assembling when the wing is installed, wing installation quality is improved, it is ensured that the reliability that wing is installed.21 frame of bracket
It is located on three posture adjustment localizers 22, the quantity of wing fixation clamp 24 is two, and two wing fixation clamps 24 are in diagonally to be distributed in
On bracket 21, wing fixation clamp 24 and 21 pivot joint of bracket.Can manually by wing pressure by wing fixation clamp 24 after placing wing
Tightly, when preventing docking, wing is moved.The bottom of base 23 is provided with four legs 25, not only can bear the gravity of base 23, also
Can adjusting base 23 as needed level.
By lifter being arranged in mobile station 11, can enable positioning bracket system 2 to positioning 2 liters of acts of bracket system
Enough it is erected in mobile station 11 and can lands.Or telescopic pole can be set in the bottom of positioning bracket system 2, make
Positioning bracket system 2 can land.
It is of the present utility model can Omni-mobile wing mounting platform working condition it is as follows：Support will be positioned by mobile station 11
Rack device 2 is moved to where needing work, puts down positioning bracket system 2, and three posture adjustment localizers 22 are by either synchronously or asynchronously
Action, is completed being accurately positioned for wing, then wing is docked with fuselage.Above-mentioned action, can be grasped by hand-held remote controller
Make, it is also dependent on needing to increase the equipment such as laser tracker, final to realize the work such as transhipment, automatic butt automatically.
It will be apparent to those skilled in the art that technical scheme that can be as described above and design, make other various
It is corresponding to change and deformation, and all these change and deformation should all belong to the protection domain of this utility model requirement
Within.
Claims (8)
1. it is a kind of can Omni-mobile wing mounting platform, it is characterised in that：Including mobile device (1) and positioning bracket system
(2), position bracket system (2) to be set up in mobile device (1), mobile device (1) includes mobile station (11) and omni-directional wheel (12),
Omni-directional wheel (12) is located at the bottom of mobile station (11) so that mobile station (11) Omni-mobile, positions bracket system (2) and be provided with support
Frame (21) and posture adjustment localizer (22), posture adjustment localizer (22) is positioned at the bottom of bracket (21) adjusting the orientation of bracket (21).
2. it is according to claim 1 can Omni-mobile wing mounting platform, it is characterised in that：Positioning bracket system (2)
Also include base (23), on base (23), base (23) is set up in the movement in mobile device (1) to posture adjustment localizer (22)
On platform (11).
3. it is according to claim 1 can Omni-mobile wing mounting platform, it is characterised in that：Bracket (21) is provided with machine
Wing fixation clamp (24).
4. it is according to claim 3 can Omni-mobile wing mounting platform, it is characterised in that：The wing fixation clamp
(24) quantity is two, and two wing fixation clamps (24) it is clinodiagonal on bracket (21) clamping to wing.
5. it is according to claim 1 can Omni-mobile wing mounting platform, it is characterised in that：Posture adjustment localizer (22)
Quantity is three, and three posture adjustment localizers (22) are distributed in triangular shape on base (23), and each posture adjustment localizer (22) has
There is the degree of freedom in tri- directions of X, Y, Z.
6. it is according to claim 1 can Omni-mobile wing mounting platform, it is characterised in that：On posture adjustment localizer (22)
It is provided with strain gauge.
7. it is according to claim 2 can Omni-mobile wing mounting platform, it is characterised in that：The bottom of base (23) sets
There are four legs (25) with the stability of adjusting base (23).
8. it is according to claim 1 can Omni-mobile wing mounting platform, it is characterised in that：Mobile station (11) is provided with
Laser scanner (13), the quantity of laser scanner (13) is two, and two laser scanners (13) are clinodiagonal located at movement
On platform (11).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620962873.5U CN206068194U (en) | 2016-08-28 | 2016-08-28 | Can Omni-mobile wing mounting platform |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620962873.5U CN206068194U (en) | 2016-08-28 | 2016-08-28 | Can Omni-mobile wing mounting platform |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206068194U true CN206068194U (en) | 2017-04-05 |
Family
ID=58432582
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620962873.5U Expired - Fee Related CN206068194U (en) | 2016-08-28 | 2016-08-28 | Can Omni-mobile wing mounting platform |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206068194U (en) |
Cited By (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107283159A (en) * | 2017-08-14 | 2017-10-24 | 上海航天设备制造总厂 | Large-scale section numerical control posture adjustment Butt Assembling system |
| CN107352044A (en) * | 2017-07-07 | 2017-11-17 | 浙江大学 | The layout method of large aircraft trailing edge component posture adjusting system |
| CN108000491A (en) * | 2017-12-07 | 2018-05-08 | 上海航天设备制造总厂有限公司 | For matching the posture adjustment equipment of docking between big component |
| CN108001708A (en) * | 2017-12-20 | 2018-05-08 | 西北工业大学 | A kind of aircraft wing docks posture adjustment reconfigurable device |
| CN108080910A (en) * | 2017-12-12 | 2018-05-29 | 大连四达高技术发展有限公司 | A kind of packaged type digitizes docking system |
| CN108100931A (en) * | 2017-12-12 | 2018-06-01 | 大连四达高技术发展有限公司 | A kind of packaged type digital positioners |
| CN108974390A (en) * | 2018-08-22 | 2018-12-11 | 晨龙飞机（荆门）有限公司 | A kind of aircraft horizontal wings test bracket |
| CN110174082A (en) * | 2019-06-03 | 2019-08-27 | 西安飞机工业（集团）有限责任公司 | A kind of restructural positioning system and localization method |
| CN110963071A (en) * | 2018-09-28 | 2020-04-07 | 空中客车运营简化股份公司 | Transport trolley |
| CN112157659A (en) * | 2020-10-28 | 2021-01-01 | 成都九系机器人科技有限公司 | Airplane component assembling system and method based on robot force and position hybrid control |
| CN112407320A (en) * | 2021-01-25 | 2021-02-26 | 北京天创凯睿科技有限公司 | Aircraft wing maintenance device and method thereof |
| CN112722319A (en) * | 2021-01-26 | 2021-04-30 | 北京天创凯睿科技有限公司 | Aircraft wing maintenance device and method thereof |
| CN116443262A (en) * | 2023-06-14 | 2023-07-18 | 陕西德鑫智能科技有限公司 | Wing bracket, wing transferring and installing method |
-
2016
- 2016-08-28 CN CN201620962873.5U patent/CN206068194U/en not_active Expired - Fee Related
Cited By (17)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107352044A (en) * | 2017-07-07 | 2017-11-17 | 浙江大学 | The layout method of large aircraft trailing edge component posture adjusting system |
| CN107352044B (en) * | 2017-07-07 | 2019-11-19 | 浙江大学 | The layout method of large aircraft trailing edge component posture adjusting system |
| CN107283159A (en) * | 2017-08-14 | 2017-10-24 | 上海航天设备制造总厂 | Large-scale section numerical control posture adjustment Butt Assembling system |
| CN108000491A (en) * | 2017-12-07 | 2018-05-08 | 上海航天设备制造总厂有限公司 | For matching the posture adjustment equipment of docking between big component |
| CN108080910A (en) * | 2017-12-12 | 2018-05-29 | 大连四达高技术发展有限公司 | A kind of packaged type digitizes docking system |
| CN108100931A (en) * | 2017-12-12 | 2018-06-01 | 大连四达高技术发展有限公司 | A kind of packaged type digital positioners |
| CN108001708A (en) * | 2017-12-20 | 2018-05-08 | 西北工业大学 | A kind of aircraft wing docks posture adjustment reconfigurable device |
| CN108974390A (en) * | 2018-08-22 | 2018-12-11 | 晨龙飞机（荆门）有限公司 | A kind of aircraft horizontal wings test bracket |
| CN108974390B (en) * | 2018-08-22 | 2020-04-03 | 晨龙飞机（荆门）有限公司 | Plane horizontal wing test bracket |
| CN110963071A (en) * | 2018-09-28 | 2020-04-07 | 空中客车运营简化股份公司 | Transport trolley |
| CN110174082A (en) * | 2019-06-03 | 2019-08-27 | 西安飞机工业（集团）有限责任公司 | A kind of restructural positioning system and localization method |
| CN112157659A (en) * | 2020-10-28 | 2021-01-01 | 成都九系机器人科技有限公司 | Airplane component assembling system and method based on robot force and position hybrid control |
| CN112407320A (en) * | 2021-01-25 | 2021-02-26 | 北京天创凯睿科技有限公司 | Aircraft wing maintenance device and method thereof |
| CN112407320B (en) * | 2021-01-25 | 2021-04-09 | 北京天创凯睿科技有限公司 | Aircraft wing maintenance device and method thereof |
| CN112722319A (en) * | 2021-01-26 | 2021-04-30 | 北京天创凯睿科技有限公司 | Aircraft wing maintenance device and method thereof |
| CN116443262A (en) * | 2023-06-14 | 2023-07-18 | 陕西德鑫智能科技有限公司 | Wing bracket, wing transferring and installing method |
| CN116443262B (en) * | 2023-06-14 | 2023-09-08 | 陕西德鑫智能科技有限公司 | Wing bracket, wing transferring and installing method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170405 Termination date: 20180828 |