CN207903863U - A kind of high-altitude operation vehicle radar collision device - Google Patents
A kind of high-altitude operation vehicle radar collision device Download PDFInfo
- Publication number
- CN207903863U CN207903863U CN201820024244.7U CN201820024244U CN207903863U CN 207903863 U CN207903863 U CN 207903863U CN 201820024244 U CN201820024244 U CN 201820024244U CN 207903863 U CN207903863 U CN 207903863U
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- China
- Prior art keywords
- elevating lever
- controller
- ultrasonic wave
- operation vehicle
- altitude operation
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Abstract
The utility model discloses a kind of high-altitude operation vehicle radar collision devices,Its structure includes protective fence,Job platform,Staircase,Connecting pole,Radar probe,Supporting table,Support column,Telescopic rod,First elevating lever,Second elevating lever,It is mutually welded with the upper surface of job platform the lower surface of protective fence,A kind of high-altitude operation vehicle radar collision device of the utility model,Support column is fixed in place,Control telescopic rod up stretches,The first elevating lever and the second elevating lever is driven to move upwards,Second elevating lever drives job platform to rise to certain altitude,Ultrasonic transmitter emits ultrasonic wave outward,Ultrasonic wave rebounds when encountering object to ultrasonic wave,Ultrasonic receiver receives ultrasonic wave,Controller is transferred to by lead and pin as electronic signals,Controller alarms to staff,The outline border plays detection angle and raises up,It is not susceptible to report by mistake,Ultrasonic wave launch angle raises up,Radar probe detection ground will not be reported by mistake,Practicability is higher.
Description
Technical field
The utility model is a kind of high-altitude operation vehicle radar collision device, belongs to machine control techniques field.
Background technology
With the expansion of urban construction scale, demand of the every profession and trade to aerial work platform is also increasing, it is more next to require
Higher, the demand of customization is also more and more obvious, in some nonplanar construction sites.
Prior art discloses application No. is：201420644449.7 a kind of high-altitude operation vehicle radar collision device described in
Aerial work platform is equipped with control centre, and the radar collision device includes supersonic generator, ultrasonic receiver and place
Device is managed, the supersonic generator sends out ultrasonic wave, and the ultrasonic receiver receives the ultrasonic wave being reflected back, the ultrasonic wave
Receiver is connected with the processor, and the processor is connected with the control centre of the aerial work platform, the processor
The movement of the aerial work platform is controlled by the control centre according to the ultrasonic wave of reception, but the prior art is ultrasonic
Wave launch angle is improper, causes radar probe detection ground to be reported by mistake, practicability is relatively low.
Utility model content
In view of the deficienciess of the prior art, the utility model aim is to provide a kind of high-altitude operation vehicle radar collision dress
It sets, it is improper to solve prior art ultrasonic launch angle, cause radar probe detection plane to be reported by mistake, practicability is lower
Problem.
To achieve the goals above, the utility model is to realize by the following technical solutions：A kind of high-altitude operation vehicle
Radar collision device, structure include protective fence, job platform, staircase, connecting pole, radar probe, supporting table, support column, stretch
Contracting bar, the first elevating lever, the second elevating lever, the lower surface of the protective fence are mutually welded with the upper surface of job platform, the work
The lower surface of industry platform is installed on the upper surface of connecting pole and uses vertical welding, and the upper surface of the staircase is installed on operation
It the lower surface of platform and is mutually perpendicular to, the right surface of the staircase is mutually welded with the left surface of connecting pole, the radar probe
Insertion is installed on the front of the first elevating lever and is gap-matched, and the right surface of the supporting table is installed on a left side for support column
Surface and vertical welding is used, the inner surface of the support column and the outer surface of the first elevating lever fit, the supporting table
Upper surface be connected with the lower surface of telescopic rod, the upper surface of the telescopic rod and the lower surface of the first elevating lever are mutually welded,
The outer surface of second elevating lever and the inner surface of support column fit, and the radar probe includes outline border, ultrasonic wave reception
Device, ultrasonic transmitter, lead, fulcrum, pin, controller, controller head cover, lower surface and the ultrasonic wave of the outline border receive
The upper surface of device is bonding, and the lower surface of the ultrasonic receiver is mutually welded with the upper surface of lead, and the ultrasonic wave receives
The upper surface of device is connected with the lower surface of ultrasonic transmitter, and the lower surface of the lead is mutually welded with the upper surface of pin,
The lower surface of the fulcrum and the upper surface of controller head cover are bonding, and the pin insertion is installed on the upper surface of controller simultaneously
And using electrical connection, the controller head cover insertion is installed on the upper surface of controller and is gap-matched, the pin
Outer surface and the inner surface of controller head cover fit.
Further, the second elevating lever insertion is installed on the right surface of connecting pole and is connected by screw, institute
The front for stating the second elevating lever is equipped with internal thread.
Further, the first elevating lever insertion is installed on the right surface of connecting pole and is connected by screw, institute
The front for stating the first elevating lever is equipped with internal thread.
Further, the controller insertion is installed on the front of the first elevating lever and is gap-matched.
Further, the supporting table is the rectangular parallelepiped structure of long 15CM, width 15CM, high 3CM.
Further, the supporting table uses aluminum alloy material, and hardness is higher, is unlikely to deform.
Further, the protective fence uses iron and steel material quality, and sexual valence is relatively high, and cost is relatively low.
Advantageous effect
A kind of high-altitude operation vehicle radar collision device of the utility model, support column is fixed in place, control
Telescopic rod processed up stretches, and the first elevating lever and the second elevating lever is driven to move upwards, and the second elevating lever drives on job platform
It is raised to certain altitude, ultrasonic transmitter emits ultrasonic wave outward, and ultrasonic wave rebounds when encountering object to ultrasonic wave, and ultrasonic wave connects
Receive device and receive ultrasonic wave, controller is transferred to by lead and pin as electronic signals, controller to staff into
Row alarm, the outline border play detection angle and raise up, be not susceptible to report by mistake, and ultrasonic wave launch angle raises up, radar probe detection
Ground will not be reported by mistake, and practicability is higher.
Description of the drawings
Upon reading the detailed description of non-limiting embodiments with reference to the following drawings, other spies of the utility model
Sign, objects and advantages will become more apparent upon：
Fig. 1 is a kind of structural schematic diagram of high-altitude operation vehicle radar collision device of the utility model；
Fig. 2 is the internal structure schematic diagram of the utility model radar probe；
Fig. 3 is the cross-sectional view of the utility model radar probe.
In figure：Protective fence -1, job platform -2, staircase -3, connecting pole -4, radar probe -5, supporting table -6, support column -
7, telescopic rod -8, the first elevating lever -9, the second elevating lever -10, outline border -501, ultrasonic receiver -502, ultrasonic transmitter -
503, lead -504, fulcrum -505, pin -506, controller -507, controller head cover -508.
Specific implementation mode
To make the technical means, creative features, achievement of purpose, and effectiveness of the utility model be easy to understand, below
In conjunction with specific implementation mode, the utility model is expanded on further.
It please refers to Fig.1, Fig. 2, Fig. 3, the utility model provides a kind of high-altitude operation vehicle radar collision device technique scheme：Its
Structure includes protective fence 1, job platform 2, staircase 3, connecting pole 4, radar probe 5, supporting table 6, support column 7, telescopic rod 8,
One elevating lever 9, the second elevating lever 10, the lower surface of the protective fence 1 are mutually welded with the upper surface of job platform 2, the operation
The lower surface of platform 2 is installed on the upper surface of connecting pole 4 and uses vertical welding, and the upper surface of the staircase 3 is installed on work
It the lower surface of industry platform 2 and is mutually perpendicular to, the right surface of the staircase 3 is mutually welded with the left surface of connecting pole 4, the radar
5 insertion of probe is installed on the front of the first elevating lever 9 and is gap-matched, and the right surface of the supporting table 6 is installed on branch
The left surface of dagger 7 and vertical welding being used, the inner surface of the support column 7 and the outer surface of the first elevating lever 9 fit,
The upper surface of the supporting table 6 is connected with the lower surface of telescopic rod 8, the upper surface of the telescopic rod 8 and the first elevating lever 9
Lower surface is mutually welded, and the outer surface of second elevating lever 10 and the inner surface of support column 7 fit, and the radar probe 5 is wrapped
Include outline border 501, ultrasonic receiver 502, ultrasonic transmitter 503, lead 504, fulcrum 505, pin 506, controller 507,
Controller head cover 508, the lower surface and the upper surface of ultrasonic receiver 502 of the outline border 501 are bonding, and the ultrasonic wave connects
The lower surface and the upper surface of lead 504 for receiving device 502 are mutually welded, and upper surface and the ultrasonic wave of the ultrasonic receiver 502 are sent out
The lower surface of emitter 503 is connected, and the lower surface of the lead 504 is mutually welded with the upper surface of pin 506, the fulcrum 505
Lower surface and the upper surface of controller head cover 508 it is bonding, the pin 506, which is embedded in, is installed on the upper surface of controller 507
And using electrical connection, the controller head cover 508 is embedded in the upper surface for being installed on controller 507 and is gap-matched,
The outer surface of the pin 506 and the inner surface of controller head cover 508 fit, and second elevating lever 10 is embedded in the company of being installed on
It connects the right surface of column 4 and is connected by screw, the front of second elevating lever 10 is equipped with internal thread, first lifting
Bar 9 is embedded in the right surface for being installed on connecting pole 4 and is connected by screw, and the front of first elevating lever 9 is equipped with interior spiral shell
Line, the controller 507 are embedded in the front for being installed on the first elevating lever 9 and are gap-matched, and the supporting table 6 is length
The rectangular parallelepiped structure of 15CM, width 15CM, high 3CM, the supporting table 6 use aluminum alloy material, and hardness is higher, is unlikely to deform, institute
It states protective fence 1 and uses iron and steel material quality, sexual valence is relatively high, and cost is relatively low.
Radar probe 5 described in this patent is in order to study and utilize ultrasonic wave, people to design and be made many super
Sonic generator, ultrasonic probe, with back-up radar probe, generally speaking, ultrasonic wave hair probe can be divided into two major classes：One
Class is with electrically generating ultrasonic wave, and one kind is mechanically to generate ultrasonic wave, and the pin 506 is called pin, is exactly
The wiring with peripheral circuit is drawn from IC chip internal circuit, all pins just constitute the interface of this block chip,
One section of lead terminal makes this section that solder joint be collectively formed with the pad in printed board by solder.
Support column 7 is fixed in place when being used, control telescopic rod 8 up stretches, and drives the
One elevating lever 9 and the second elevating lever 10 move upwards, and the second elevating lever 10 drives job platform 2 to rise to certain altitude, ultrasound
Wave launcher 503 emits ultrasonic wave outward, and ultrasonic wave rebounds when encountering object to ultrasonic wave, and ultrasonic receiver 502 receives
Ultrasonic wave is transferred to controller 507 by lead 504 and pin 506 as electronic signals, and controller 507 is to staff
It alarms, the outline border 501 plays detection angle and raises up, and is not susceptible to report by mistake.
It is improper that the utility model solves prior art ultrasonic launch angle, and radar probe detection plane is caused to be missed
Report, the relatively low problem of practicability, the utility model are combined with each other by above-mentioned component, a kind of high-altitude operation vehicle of the utility model
Support column is fixed radar collision device in place, control telescopic rod up stretch, drive the first elevating lever and
Second elevating lever moves upwards, and the second elevating lever drives job platform to rise to certain altitude, and ultrasonic transmitter emits outward
Ultrasonic wave, ultrasonic wave rebounds when encountering object to ultrasonic wave, and ultrasonic receiver receives ultrasonic wave, leads to as electronic signals
It crosses lead and pin is transferred to controller, controller alarms to staff, and the outline border plays detection angle and raises up, no
It easily reports by mistake, ultrasonic wave launch angle raises up, and radar probe detection ground will not be reported by mistake, and practicability is higher, institute specific as follows
It states:
The radar probe 5 includes outline border 501, ultrasonic receiver 502, ultrasonic transmitter 503, lead 504, fulcrum
505, pin 506, controller 507, controller head cover 508, the lower surface of the outline border 501 are upper with ultrasonic receiver 502
Surface is bonding, and the lower surface of the ultrasonic receiver 502 is mutually welded with the upper surface of lead 504, and the ultrasonic wave receives
The upper surface of device 502 is connected with the lower surface of ultrasonic transmitter 503, and the lower surface of the lead 504 is upper with pin 506
Surface is mutually welded, and the lower surface and the upper surface of controller head cover 508 of the fulcrum 505 are bonding, the insertion peace of the pin 506
Upper surface loaded on controller 507 and use electrical connection, the insertion of controller head cover 508 are installed on the upper of controller 507
It surface and is gap-matched, the outer surface of the pin 506 and the inner surface of controller head cover 508 fit.
The advantages of basic principles and main features and the utility model of the utility model have been shown and described above, for
For those skilled in the art, it is clear that the present invention is not limited to the details of the above exemplary embodiments, and without departing substantially from this
In the case of the spirit or essential attributes of utility model, the utility model can be realized in other specific forms.Therefore, no matter
From the point of view of which point, the present embodiments are to be considered as illustrative and not restrictive, and the scope of the utility model is by institute
Attached claim rather than above description limit, it is intended that will fall within the meaning and scope of the equivalent requirements of the claims
All changes are embraced therein.Any reference numeral in claim should not be considered as to the involved right of limitation
It is required that.
In addition, it should be understood that although this specification is described in terms of embodiments, but not each embodiment is only wrapped
Containing an independent technical solution, this description of the specification is merely for the sake of clarity, and those skilled in the art should
It considers the specification as a whole, the technical solutions in the various embodiments may also be suitably combined, forms those skilled in the art
The other embodiment being appreciated that.
Claims (5)
1. a kind of high-altitude operation vehicle radar collision device, it is characterised in that：Its structure include protective fence (1), job platform (2),
Staircase (3), connecting pole (4), radar probe (5), supporting table (6), support column (7), telescopic rod (8), the first elevating lever (9),
Two elevating levers (10), the lower surface and the upper surface of job platform (2) of the protective fence (1) are mutually welded, the job platform (2)
Lower surface be installed on connecting pole (4) upper surface and use vertical welding, the upper surface of the staircase (3) is installed on operation
It the lower surface of platform (2) and is mutually perpendicular to, the right surface and the left surface of connecting pole (4) of the staircase (3) are mutually welded, described
Radar probe (5) insertion is installed on the front of the first elevating lever (9) and is gap-matched, the right table of the supporting table (6)
Face is installed on the left surface of support column (7) and uses vertical welding, the inner surface and the first elevating lever of the support column (7)
(9) outer surface fits, and the upper surface of the supporting table (6) is connected with the lower surface of telescopic rod (8), the telescopic rod
(8) upper surface and the lower surface of the first elevating lever (9) are mutually welded, the outer surface of second elevating lever (10) and support column
(7) inner surface fits, and the radar probe (5) includes outline border (501), ultrasonic receiver (502), ultrasonic transmitter
(503), lead (504), fulcrum (505), pin (506), controller (507), controller head cover (508), the outline border (501)
Lower surface and the upper surface of ultrasonic receiver (502) it is bonding, the lower surface of the ultrasonic receiver (502) and lead
(504) upper surface is mutually welded, the lower surface of the upper surface and ultrasonic transmitter (503) of the ultrasonic receiver (502)
Be connected, the lower surface and the upper surface of pin (506) of the lead (504) are mutually welded, the lower surface of the fulcrum (505) with
The upper surface of controller head cover (508) is bonding, the embedded upper surface for being installed on controller (507) of the pin (506) and
Using electrical connection, controller head cover (508) insertion is installed on the upper surface of controller (507) and is gap-matched,
The outer surface of the pin (506) and the inner surface of controller head cover (508) fit.
2. a kind of high-altitude operation vehicle radar collision device according to claim 1, it is characterised in that：Second elevating lever
(10) insertion is installed on the right surface of connecting pole (4) and is connected by screw, and the front of second elevating lever (10) is set
There is internal thread.
3. a kind of high-altitude operation vehicle radar collision device according to claim 1, it is characterised in that：First elevating lever
(9) insertion is installed on the right surface of connecting pole (4) and is connected by screw, and the front of first elevating lever (9) is equipped with
Internal thread.
4. a kind of high-altitude operation vehicle radar collision device according to claim 1, it is characterised in that：The controller
(507) insertion is installed on the front of the first elevating lever (9) and is gap-matched.
5. a kind of high-altitude operation vehicle radar collision device according to claim 1, it is characterised in that：The supporting table (6)
For the rectangular parallelepiped structure of long 15CM, width 15CM, high 3CM.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820024244.7U CN207903863U (en) | 2018-01-08 | 2018-01-08 | A kind of high-altitude operation vehicle radar collision device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820024244.7U CN207903863U (en) | 2018-01-08 | 2018-01-08 | A kind of high-altitude operation vehicle radar collision device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207903863U true CN207903863U (en) | 2018-09-25 |
Family
ID=63566954
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820024244.7U Expired - Fee Related CN207903863U (en) | 2018-01-08 | 2018-01-08 | A kind of high-altitude operation vehicle radar collision device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207903863U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109970009A (en) * | 2019-04-24 | 2019-07-05 | 江苏建筑职业技术学院 | High-altitude operation vehicle collision prevention device and method |
-
2018
- 2018-01-08 CN CN201820024244.7U patent/CN207903863U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109970009A (en) * | 2019-04-24 | 2019-07-05 | 江苏建筑职业技术学院 | High-altitude operation vehicle collision prevention device and method |
| CN109970009B (en) * | 2019-04-24 | 2024-02-23 | 江苏建筑职业技术学院 | Anti-collision device and method for overhead working truck |
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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: 20180925 Termination date: 20200108 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |