CN204433083U - A kind of aircraft deicing vehicle working bucket anti-collision equipment - Google Patents
A kind of aircraft deicing vehicle working bucket anti-collision equipment Download PDFInfo
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- CN204433083U CN204433083U CN201520053317.1U CN201520053317U CN204433083U CN 204433083 U CN204433083 U CN 204433083U CN 201520053317 U CN201520053317 U CN 201520053317U CN 204433083 U CN204433083 U CN 204433083U
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- working bucket
- ultrasonic transduter
- deicing vehicle
- bucket
- collision equipment
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- 230000033228 biological regulation Effects 0.000 claims abstract description 5
- 230000001105 regulatory effect Effects 0.000 claims description 2
- 235000012469 Cleome gynandra Nutrition 0.000 abstract description 5
- 240000007918 Tacca chantrieri Species 0.000 abstract description 5
- 238000001514 detection method Methods 0.000 abstract description 5
- 239000002775 capsule Substances 0.000 description 4
- 230000007423 decrease Effects 0.000 description 3
- NBIIXXVUZAFLBC-UHFFFAOYSA-N Phosphoric acid Chemical compound OP(O)(O)=O NBIIXXVUZAFLBC-UHFFFAOYSA-N 0.000 description 1
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 238000010009 beating Methods 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000004140 cleaning Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
- 229910001220 stainless steel Inorganic materials 0.000 description 1
- 239000010935 stainless steel Substances 0.000 description 1
- 238000011179 visual inspection Methods 0.000 description 1
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- Measurement Of Velocity Or Position Using Acoustic Or Ultrasonic Waves (AREA)
Abstract
The utility model relates to a kind of aircraft deicing vehicle working bucket anti-collision equipment, comprise the ultrasonic transduter for spacing between real-time testing bucket and airplane skin that deicing vehicle working bucket is arranged, ultrasonic transduter is connected with control circuit, and the running state of the result regulation and control deicing vehicle mechanical arm that control circuit detects according to ultrasonic transduter and adjustment signal assembly show the spacing situation between working bucket and airplane skin in real time.Adopt ultrasonic transduter to detect in real time the spacing between working bucket and airplane skin, the accuracy of detection of ultrasonic transduter far away higher than traditional cat's whisker formula limit switch, thus prevents working bucket and aircraft casing from colliding, and eliminates safe hidden trouble.
Description
Technical field
The utility model relates to aircraft deicing vehicle field, is specifically related to a kind of aircraft deicing vehicle working bucket anti-collision equipment.
Background technology
Aircraft deicing vehicle is a kind of airport ground specialized equipment, and it sprays by certain pressure the deicing liquid being heated to uniform temperature, to carry out deicing to aircraft localized ice build position or aircraft whole body, also can carry out cleaning and the maintenance activity of aircraft as required.The work of deicing is mainly undertaken by the working bucket of mechanical arm front end, working bucket should be configured with anticollision device and close to aerocraft prior-warning device, with anticollision wrap up.At present; most employing is installed cat's whisker formula limit switch and is protected in working bucket; and this mode only has and just carries out reporting to the police and position limitation protection when working bucket is pressed close to after aircraft surfaces touches cat's whisker switch, therefore the accuracy of anticollision is limited, there is very large potential safety hazard.
Summary of the invention
The purpose of this utility model is just to provide a kind of aircraft deicing vehicle working bucket anti-collision equipment, and it can effectively solve the problem, and improves accuracy of detection, prevents aircraft and working bucket from colliding.
For achieving the above object, the utility model adopts following technical scheme to implement:
A kind of aircraft deicing vehicle working bucket anti-collision equipment, it is characterized in that: comprise the ultrasonic transduter for spacing between real-time testing bucket and airplane skin that deicing vehicle working bucket is arranged, ultrasonic transduter is connected with control circuit, and the running state of the result regulation and control deicing vehicle mechanical arm that control circuit detects according to ultrasonic transduter and adjustment signal assembly show the spacing situation between working bucket and airplane skin in real time.
Adopt ultrasonic transduter to detect in real time the spacing between working bucket and airplane skin, the accuracy of detection of ultrasonic transduter far away higher than traditional cat's whisker formula limit switch, thus prevents working bucket and aircraft casing from colliding, and eliminates safe hidden trouble.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model;
Fig. 2 is the structural representation of the utility model electrical connection.
Detailed description of the invention
In order to make the purpose of this utility model and advantage clearly understand, below in conjunction with embodiment, the utility model is specifically described.Should be appreciated that following word only in order to describe one or more concrete embodiments of the present utility model, considered critical is not carried out to the protection domain that the utility model is specifically asked.
The technical scheme that the utility model is taked as shown in Figure 1, a kind of aircraft deicing vehicle working bucket anti-collision equipment, comprise the ultrasonic transduter 11 for spacing between real-time testing bucket 10 and airplane skin that deicing vehicle working bucket 10 is arranged, ultrasonic transduter 11 is connected with control circuit, and the running state of the result regulation and control deicing vehicle mechanical arm that control circuit detects according to ultrasonic transduter 11 and adjustment signal assembly show the spacing situation between working bucket 10 and airplane skin in real time.Ultrasonic transduter 11 can be arranged in the sidewall shell of working bucket 10.The spacing between ultrasonic transduter 11 pairs of working buckets 10 and airplane skin is adopted to detect in real time, the accuracy of detection of ultrasonic transduter 11 is far away higher than traditional cat's whisker formula limit switch, thus prevent working bucket 10 and aircraft casing from colliding, eliminate safe hidden trouble.
More preferred embodiment is, ultrasonic transduter 11 and the mutually concordant setting in working bucket 10 lower end, and ultrasonic transduter 11 is positioned at the middle part of shell.The shell of working bucket 10 is provided with flute profile outer cover 12, the notch of flute profile outer cover 12 to extended flange outside two and with the shell Joint of working bucket 10, the flute length direction of flute profile outer cover 12 is consistent with the short transverse of working bucket 10, the notch of flute profile outer cover 12 points to the side of working bucket 10, be provided with L shaped plate part support 13 in flute profile outer cover 12, ultrasonic transduter 11 is fixed on L shaped plate part support 13.Signal component comprises the yellow indicator lamp and red indicating light that are positioned at the setting of end, working bucket 10 upper end.Anti-collision equipment also comprises the toggle switch regulated for enforcing the position of mechanical arm to working bucket 10.Flute profile outer cover 12, L shaped plate part support 13 are panel beating bending part and form, and be fixedly connected with by stainless steel bolt, electrical harness can be connected with working bucket 10 control capsule by entering bottom working bucket 10.
Be fixed on by ultrasonic transduter 11 on L shaped plate part support 13, then entirety be fixed on flute profile outer cover 12, be finally bolted on the dead ahead line of centers of working bucket 10 by flute profile outer cover 12, lower edge is concordant with the bottom surface of working bucket 10.Yellow indicator lamp 14, red indicating light 15, toggle switch 16 are arranged on working bucket 10 control capsule panel, and intermediate relay 17 is arranged on the guide rail of control capsule inside.The assemblies such as ultrasonic transduter 11, yellow indicator lamp 14, red indicating light 15 are connected according to Fig. 2.
Effective detecting distance of sonac is 10 meters, wherein blind area scope is 80 ~ 100mm, namely cannot detect at this wide-ultra sonic transducer, utilize the characteristic of ultrasonic transduter 11, when detecting distance is when being greater than 1200mm, yellow indicator lamp 14, red indicating light 15 does not all work, as detecting distance 100mm≤L≤1200mm, yellow indicator lamp 14 is bright, when detecting distance L is more close to 400mm, yellow indicator lamp 14 can constantly glimmer, as detecting distance 100mm≤L≤400mm, yellow indicator lamp 14 is long bright, red indicating light 15 is long bright simultaneously, now export by relay the mechanical arm controlled cannot decline, thus play the potential safety hazard avoiding working bucket 10 to contact with aircraft surfaces.The toggle switch be arranged on working bucket 10 control capsule can play the function of forcing contact, when yellow indicator lamp 14 and red indicating light 15 bright with duration time, operator according to the actual requirements and visual inspection can continue operating robotic arm regulation and control working bucket 10 by toggle switch 16 (force switch in Fig. 2) declines, thus can reach necessary job requirements.
Control circuit comprises large arm lowering valve, jib control relay, yellow indicator lamp 14, red indicating light 15, toggle switch, electrical connection between ultrasonic transduter and each components and parts of control circuit is concrete with reference to accompanying drawing 2, in Fig. 2 anticollision control principle (in dotted line frame), module is as detecting distance 100mm≤L≤1200mm, yellow indicator lamp 14 is interrupted flicker, as detecting distance 100mm≤L≤400mm, the 1# end of KA1 jib control relay is+12V high level, coil is connected, 3# end leads to 5# termination, 4# and 6# termination is led to, control large arm lowering valve B end, jib decline disabler, red indicating light 15 is long bright simultaneously, realize anti-collision.
Utilize that ultrasonic transduter 11 safety distance is adjustable, the characteristic such as non-contact detection, highly sensitive, fast response time, realize when mechanical arm decline operation, actv. prevents from contacting with aircraft surfaces bottom working bucket 10 thus reducing the potential safety hazard of colliding aircraft to greatest extent.The utility model both carried out limiting to safety distance when operation, can operate toggle switch again simultaneously and lift restrictions voluntarily, control flexibly the scope of work of mechanical arm by operator, improved operating efficiency.
The above is only preferred implementation of the present utility model; should be understood that; for those skilled in the art; to know in the utility model after contents; under the prerequisite not departing from the utility model principle; can also make some equal conversion to it and substitute, these convert on an equal basis and substitute and also should be considered as belonging to protection domain of the present utility model.
Claims (6)
1. an aircraft deicing vehicle working bucket anti-collision equipment, it is characterized in that: comprise the ultrasonic transduter for spacing between real-time testing bucket and airplane skin that deicing vehicle working bucket is arranged, ultrasonic transduter is connected with control circuit, and the running state of the result regulation and control deicing vehicle mechanical arm that control circuit detects according to ultrasonic transduter and adjustment signal assembly show the spacing situation between working bucket and airplane skin in real time.
2. aircraft deicing vehicle working bucket anti-collision equipment according to claim 1, is characterized in that: ultrasonic transduter is arranged in the sidewall shell of working bucket.
3. aircraft deicing vehicle working bucket anti-collision equipment according to claim 1 and 2, is characterized in that: ultrasonic transduter setting mutually concordant with working bucket lower end, and ultrasonic transduter is positioned at the middle part of shell.
4. aircraft deicing vehicle working bucket anti-collision equipment according to claim 3, it is characterized in that: the shell of working bucket is provided with flute profile outer cover, the notch of flute profile outer cover to extended flange outside two and with the shell Joint of working bucket, the flute length direction of flute profile outer cover is consistent with the short transverse of working bucket, the notch of flute profile outer cover points to the side of working bucket, be provided with L shaped plate part support in flute profile outer cover, ultrasonic transduter is fixed on L shaped plate part support.
5. aircraft deicing vehicle working bucket anti-collision equipment according to claim 1 and 2, is characterized in that: signal component comprises the yellow indicator lamp and red indicating light that are positioned at the setting of end, working bucket upper end.
6. aircraft deicing vehicle working bucket anti-collision equipment according to claim 1 and 2, is characterized in that: anti-collision equipment also comprises the toggle switch regulated for enforcing the position of mechanical arm to working bucket.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520053317.1U CN204433083U (en) | 2015-01-26 | 2015-01-26 | A kind of aircraft deicing vehicle working bucket anti-collision equipment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520053317.1U CN204433083U (en) | 2015-01-26 | 2015-01-26 | A kind of aircraft deicing vehicle working bucket anti-collision equipment |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204433083U true CN204433083U (en) | 2015-07-01 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520053317.1U Expired - Fee Related CN204433083U (en) | 2015-01-26 | 2015-01-26 | A kind of aircraft deicing vehicle working bucket anti-collision equipment |
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| CN (1) | CN204433083U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105774542A (en) * | 2016-05-25 | 2016-07-20 | 北京路特思达机电设备有限公司 | Scramming device and method for deicing vehicle |
| CN106825942A (en) * | 2017-01-09 | 2017-06-13 | 宁波市阳光汽车配件有限公司 | The laser cutting device of thermoplasticity abnormal shape body-finishing plate |
| CN106990407A (en) * | 2017-02-24 | 2017-07-28 | 联创汽车电子有限公司 | Anti-collision alarm system ultrasonic blind zone processing method and anti-collision alarm system |
-
2015
- 2015-01-26 CN CN201520053317.1U patent/CN204433083U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105774542A (en) * | 2016-05-25 | 2016-07-20 | 北京路特思达机电设备有限公司 | Scramming device and method for deicing vehicle |
| CN105774542B (en) * | 2016-05-25 | 2018-07-10 | 北京路特思达机电设备有限公司 | A kind of deicing vehicle emergency stop device and method |
| CN106825942A (en) * | 2017-01-09 | 2017-06-13 | 宁波市阳光汽车配件有限公司 | The laser cutting device of thermoplasticity abnormal shape body-finishing plate |
| CN106990407A (en) * | 2017-02-24 | 2017-07-28 | 联创汽车电子有限公司 | Anti-collision alarm system ultrasonic blind zone processing method and anti-collision alarm system |
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| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150701 |
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| CF01 | Termination of patent right due to non-payment of annual fee |