CN206782108U - A kind of aircraft rigger makees platform anticollision device, collision-prevention device - Google Patents
A kind of aircraft rigger makees platform anticollision device, collision-prevention device Download PDFInfo
- Publication number
- CN206782108U CN206782108U CN201720687649.4U CN201720687649U CN206782108U CN 206782108 U CN206782108 U CN 206782108U CN 201720687649 U CN201720687649 U CN 201720687649U CN 206782108 U CN206782108 U CN 206782108U
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- China
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- switch
- aircraft
- inductor
- speed reducing
- collision
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Abstract
A kind of aircraft rigger makees platform anticollision device, collision-prevention device, including workbench, support, speed reducing switch, location switch and controller, by being arranged on multiple rollers of frame bottom, displacement is realized in cooperation to described support in orbit, one of roller drives as driving wheel and by motor, described location switch and speed reducing switch include inductor and the induction pieces coordinated with inductor, the inductor of speed reducing switch and the inductor of location switch are successively set on the frame bottom that support moves towards aircraft direction to be assembled, the induction pieces of speed reducing switch and the induction pieces of location switch are successively set on the track sidepiece that support moves towards aircraft direction to be assembled；Described controller includes PLC control system and motor driver, and the inductor of described location switch and speed reducing switch feeds back to signal described PLC control system, and control system passes through the described motor of motor driver control and worked；Described workbench is provided with the safe touch side coordinated with aircraft to be assembled.
Description
Technical field
The utility model belongs to aircraft mounting plate technical field of safety protection, especially makees platform with a kind of aircraft rigger
Anticollision device, collision-prevention device is relevant.
Background technology
Current aircraft workbench does not have CAS or only installs a slat gum bar to buffer, so in platform edges
Setting can not ensure aircraft workbench situation about not colliding when close to aircraft, and also may not necessarily using rubber strip
Ensure that aircraft surfaces do not sustain damage.If aircraft workbench is not contacted with aircraft to be assembled, between platform and aircraft
Space is had again, then assembly work can be caused potential safety hazard to be present and can produce many troubles.
Utility model content
For drawbacks described above existing for above-mentioned background technology, the utility model aims to provide a kind of aircraft rigger and makees platform
Anticollision device, collision-prevention device.
Therefore, the utility model uses following technical scheme：A kind of aircraft rigger makees platform anticollision device, collision-prevention device, including work
The support of platform and support working platform, it is characterized in that, described aircraft workbench CAS also includes speed reducing switch, arrived
Bit switch and controller, by being arranged on multiple rollers of frame bottom, displacement is realized in cooperation to described support in orbit, its
In a roller driven as driving wheel and by motor, described location switch and speed reducing switch include inductor and with sense
The induction pieces for answering device to coordinate, the inductor of speed reducing switch and the inductor of location switch are successively set on support and flown towards to be assembled
The frame bottom of machine direction movement, the induction pieces of speed reducing switch and the induction pieces of location switch are successively set on support towards to be assembled
Aircraft direction movement track sidepiece；Described controller includes PLC control system and motor driver, and described opens in place
Close and the inductor of speed reducing switch feeds back to signal described PLC control system, control system is controlled by motor driver
Described motor work；Described workbench is provided with the safe touch side coordinated with aircraft to be assembled.
As the supplement to above-mentioned technical proposal and perfect, the utility model also includes following technical characteristic.
Described PLC system is Siemens S7-1200, and described motor driver is Siemens's G120 drivers.
Described safe touch side is arranged on expansion plate, and expansion plate is driven flexible by drive mechanism.
It can reach following beneficial effect using the utility model：Utility model works platform is transported towards aircraft to be assembled
When dynamic, control system is fed back to by speed reducing switch triggering first, control system controlled motor driver is automatically into deceleration shape
State reaches low-speed motion, and then location switch triggering feeds back to control system, and control system controlled motor driver is automatically stopped,
Platform is contacted by safe touch side with aircraft, by structure of the present utility model, can be improved aircraft workbench and used
Security performance in journey, ensure to reduce collision or friction when platform contacts with aircraft as far as possible, may caused by damage so as to reduce
Property.
Brief description of the drawings
Fig. 1 is main view direction structure schematic diagram of the present utility model.
Fig. 2 is left view direction structure schematic diagram of the present utility model.
Embodiment
Specific embodiment of the present utility model is described in detail below in conjunction with the accompanying drawings.
As shown in Fig. 1~Fig. 2, the utility model includes workbench, speed reducing switch 2, location switch 3, the and of controller 1
The support of support working platform, by being arranged on multiple rollers of frame bottom, displacement is realized in cooperation to support in orbit, wherein
One roller drives as driving wheel and by motor 5, and location switch 3 and speed reducing switch 2 include inductor and and inductor
The induction pieces of cooperation, the inductor of speed reducing switch 2 and the inductor of location switch 3 are successively set on support towards aircraft to be assembled
The frame bottom of direction movement, the induction pieces of speed reducing switch 2 and the induction pieces of location switch 3 are successively set on support towards to be assembled
Aircraft direction movement track sidepiece；Controller 1 includes PLC control system and motor driver, and location switch 3 and deceleration are opened
Signal is fed back to PLC control system by the inductor for closing 2, and control system is worked by motor driver controlled motor 5, preferably
Ground, PLC system are Siemens S7-1200, and motor driver is Siemens's G120 drivers；Workbench be provided with it is to be assembled
The safe touch side 4 that aircraft coordinates, safe touch side 4 are arranged on expansion plate, and expansion plate is driven flexible by drive mechanism.
The advantages of general principle and principal character of the present utility model and the utility model has been shown and described above.One's own profession
The technical staff of industry is it should be appreciated that the utility model is not restricted to the described embodiments, described in above-described embodiment and specification
Simply illustrate principle of the present utility model, on the premise of the spirit and scope of the utility model is not departed from, the utility model is also
Various changes and modifications are had, these changes and improvements are both fallen within claimed the scope of the utility model.The utility model
Claimed scope is by appended claims and its equivalent thereof.
Claims (3)
1. a kind of aircraft rigger makees platform anticollision device, collision-prevention device, including the support of workbench and support working platform, its feature exists
In：Described aircraft rigger, which makees platform anticollision device, collision-prevention device, also includes speed reducing switch（2）, location switch（3）And controller（1）, institute
Displacement is realized in multiple rollers in orbit cooperation of the support stated by being arranged on frame bottom, and one of roller is as actively
Take turns and pass through motor（5）Driving, described location switch（3）And speed reducing switch（2）Include inductor and coordinate with inductor
Induction pieces, speed reducing switch（2）Inductor and location switch（3）Inductor be successively set on support towards aircraft to be assembled
The frame bottom of direction movement, speed reducing switch（2）Induction pieces and location switch（3）Induction pieces be successively set on support towards treating
The track sidepiece of the aircraft direction movement of assembling；Described controller（1）It is described including PLC control system and motor driver
Location switch（3）And speed reducing switch（2）Inductor signal is fed back to described PLC control system, control system passes through
The described motor of motor driver control（5）Work；Described workbench is provided with the safety coordinated with aircraft to be assembled and touched
Side（4）.
2. a kind of aircraft rigger according to claim 1 makees platform anticollision device, collision-prevention device, it is characterised in that：Described PLC systems
It is Siemens's G120 drivers to unite as Siemens S7-1200, described motor driver.
3. a kind of aircraft rigger according to claim 2 makees platform anticollision device, collision-prevention device, it is characterised in that：Described safety is touched
Side（4）It is arranged on expansion plate, expansion plate is driven flexible by drive mechanism.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720687649.4U CN206782108U (en) | 2017-06-14 | 2017-06-14 | A kind of aircraft rigger makees platform anticollision device, collision-prevention device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720687649.4U CN206782108U (en) | 2017-06-14 | 2017-06-14 | A kind of aircraft rigger makees platform anticollision device, collision-prevention device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206782108U true CN206782108U (en) | 2017-12-22 |
Family
ID=60715784
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720687649.4U Expired - Fee Related CN206782108U (en) | 2017-06-14 | 2017-06-14 | A kind of aircraft rigger makees platform anticollision device, collision-prevention device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206782108U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110170972A (en) * | 2019-06-03 | 2019-08-27 | 西安飞机工业（集团）有限责任公司 | A kind of error protection scaling platform mechanism |
-
2017
- 2017-06-14 CN CN201720687649.4U patent/CN206782108U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110170972A (en) * | 2019-06-03 | 2019-08-27 | 西安飞机工业（集团）有限责任公司 | A kind of error protection scaling platform mechanism |
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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 |
Granted publication date: 20171222 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |