CN205131684U - Deicing vehicle for airplane - Google Patents
Deicing vehicle for airplane Download PDFInfo
- Publication number
- CN205131684U CN205131684U CN201520960188.4U CN201520960188U CN205131684U CN 205131684 U CN205131684 U CN 205131684U CN 201520960188 U CN201520960188 U CN 201520960188U CN 205131684 U CN205131684 U CN 205131684U
- Authority
- CN
- China
- Prior art keywords
- heating pipe
- spray gun
- nanometer heating
- utility
- speed spray
- 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
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Abstract
The utility model provides a deicing vehicle for airplane, which comprises a carriage body, nanometer heating pipe and high -speed spray gun, be equipped with the water tank on the automobile body, water tank and nanometer heating pipe intercommunication, spout by high -speed spray gun behind the nanometer heating pipe steam raising, set up the aerial ladder on the automobile body, mounting platform board on the aerial ladder, the pull groove is seted up on the upper portion of landing slab, set up the cardboard on the pull groove, the cooperation of pull inslot sets up elongated panel, elongated panel is located the cardboard lower part, elongated panel's one end is located the outside of landing slab, the last supporting seat that sets up of elongated panel, articulated high -speed spray gun on the supporting seat. The utility model discloses a nanometer heating pipe steam raising, and then utilize high -speed spray gun to spray to carry out the deicing to the aircraft surface and handle, but greatly increased deicing efficiency, the security of reinforcing aircraft operation. When the platform has the certain distance apart from the operation target, through the gathering range on elongated panel extension platform upper portion to reach suitable position. The utility model discloses avoid the moving as a whole, keep good stability, reduce the occurence of failure.
Description
Technical field
The utility model belongs to aircraft mechanical engineering field, specifically a kind of aircraft deicing vehicle.
Background technology
Along with the scale of civil aviaton of China and the continuous growth of transportation volume, aircraft is more and more becoming transport facility first-selected in people's daily life, and aircraft is in operational process, and safety is primary all the time.Research finds, if fuselage is often divided a centimetre frost point for upper distribution 1 mm dia equally, the raising force of aircraft will reduce 33%, aircraft stall in take-off process is very easily caused to crash, therefore, how removing freezing on airframe, is the maximum demand for security of aircraft safe in operation in winter.Civil Aviation Airport, to the deicing capability of aircraft, badly influences the operation of aircraft, and the deicing capability of a lot of Civil Aviation Airport is inadequate in the winter time, is the major reason causing aircraft late.
Utility model content
The utility model provides a kind of aircraft deicing vehicle, in order to solve defect of the prior art.
The utility model is achieved by the following technical programs:
A kind of aircraft deicing vehicle, comprise car body, nanometer heating pipe and high-speed spray gun, car body is provided with water tank, water tank is communicated with nanometer heating pipe, nanometer heating pipe is sprayed by high-speed spray gun after producing steam, car body arranges aerial ladder, erecting stage plate on aerial ladder, pull groove is offered on the top of landing slab, and pull groove arranges clamp, is equipped with lengthened plate in pull groove, lengthened plate is positioned at clamp bottom, one end of lengthened plate is positioned at the outside of landing slab, and lengthened plate arranges supporting seat, hinged high-speed spray gun on supporting seat.
A kind of aircraft deicing vehicle as above, the both sides, other end top of described lengthened plate arrange cooperation ring, and the both sides of pull groove arrange several set collar, and one of them set collar is worn even by a fixed link with coordinating ring.
A kind of aircraft deicing vehicle as above, safe chair is installed on the top, one end that described lengthened plate stretches out landing slab.
A kind of aircraft deicing vehicle as above, the periphery of described landing slab arranges guardrail.
The utility model has the advantages that: the utility model adopts nanometer heating pipe to produce steam, and then utilizes high-speed spray gun to spray, thus carries out deicing process to aircraft surfaces, greatly can increase deicing efficiency, strengthens the safety that aircraft runs.When platform distance operative goals has certain distance, extended the scope of work of platform upper by lengthened plate, to arrive correct position.The utility model is avoided moving integrally, and keeps good stability, and minimizing accident occurs.
Accompanying drawing explanation
In order to be illustrated more clearly in the utility model embodiment or technical scheme of the prior art, be briefly described to the accompanying drawing used required in embodiment or description of the prior art below, apparently, accompanying drawing in the following describes is embodiments more of the present utility model, for those of ordinary skill in the art, under the prerequisite not paying creative work, other accompanying drawing can also be obtained according to these accompanying drawings.
Fig. 1 is structural representation of the present utility model; Fig. 2 is the A direction view of Fig. 1.
Figure number marks: 1 Trolley, 2 aerial ladders, 3 landing slabs, 4 guardrails, 5 set collars, 6 safe chairs, 7 lengthened plates, and 8 coordinate ring, 9 fixed links, 10 pull grooves, 11 clamps, 12 water tanks, 13 nanometer heating pipes, 14 supporting seats, 15 high-speed spray guns.
Detailed description of the invention
For making the object of the utility model embodiment, technical scheme and advantage clearly, below in conjunction with the accompanying drawing in the utility model embodiment, technical scheme in the utility model embodiment is clearly and completely described, obviously, described embodiment is the utility model part embodiment, instead of whole embodiments.Based on the embodiment in the utility model, those of ordinary skill in the art are not making the every other embodiment obtained under creative work prerequisite, all belong to the scope of the utility model protection.
A kind of aircraft deicing vehicle, as shown in the figure, comprise car body 1, nanometer heating pipe and high-speed spray gun 15, car body 1 is provided with water tank 12, water tank 12 is communicated with nanometer heating pipe 13, sprayed by high-speed spray gun 15 after nanometer heating pipe 13 produces steam, car body 1 is arranged aerial ladder 2, erecting stage plate 3 on aerial ladder 2, pull groove 10 is offered on the top of landing slab 3, pull groove 10 is arranged clamp 11, lengthened plate 7 is equipped with in pull groove 10, lengthened plate 7 is positioned at clamp 11 bottom, one end of lengthened plate 7 is positioned at the outside of landing slab 3, lengthened plate 7 is arranged supporting seat 14, hinged high-speed spray gun 15 on supporting seat 14.The utility model adopts nanometer heating pipe to produce steam, and then utilizes high-speed spray gun to spray, thus carries out deicing process to aircraft surfaces, greatly can increase deicing efficiency, strengthens the safety that aircraft runs.When platform distance operative goals has certain distance, extended the scope of work of platform upper by lengthened plate, to arrive correct position.The utility model is avoided moving integrally, and keeps good stability, and minimizing accident occurs.
Specifically, in order to improve stability, the both sides, other end top of the lengthened plate 7 described in the present embodiment arrange and coordinate ring 8, and the both sides of pull groove 10 arrange several set collar 5, one of them set collar 5 with coordinate ring 8 by fixed link 9 company of wearing.In order to keep lengthened plate 7 to stretch out the stable of state, steady lock can be had in the end of lengthened plate 7 by fixed link 9.
Concrete, in order to improve the safety of aloft work, safe chair 6 is installed on the top, one end that the lengthened plate 7 described in the present embodiment stretches out landing slab 3.Workman in use, can be sitting on safe chair 6, by safety clothes---with reflecting parts on clothes with safe chair 6 lock fit.
Further, in order to improve safety further, the periphery of the landing slab 3 described in the present embodiment arranges guardrail 4.
Last it is noted that above embodiment is only in order to illustrate the technical solution of the utility model, be not intended to limit; Although be described in detail the utility model with reference to previous embodiment, those of ordinary skill in the art is to be understood that: it still can be modified to the technical scheme described in foregoing embodiments, or carries out equivalent replacement to wherein portion of techniques feature; And these amendments or replacement, do not make the essence of appropriate technical solution depart from the spirit and scope of each embodiment technical scheme of the utility model.
Claims (4)
1. an aircraft deicing vehicle, it is characterized in that: comprise car body (1), nanometer heating pipe and high-speed spray gun (15), car body (1) is provided with water tank (12), water tank (12) is communicated with nanometer heating pipe (13), nanometer heating pipe (13) is sprayed by high-speed spray gun (15) after producing steam, car body (1) is arranged aerial ladder (2), the upper erecting stage plate (3) of aerial ladder (2), pull groove (10) is offered on the top of landing slab (3), pull groove (10) is arranged clamp (11), lengthened plate (7) is equipped with in pull groove (10), lengthened plate (7) is positioned at clamp (11) bottom, one end of lengthened plate (7) is positioned at the outside of landing slab (3), lengthened plate (7) is arranged supporting seat (14), the upper hinged high-speed spray gun (15) of supporting seat (14).
2. a kind of aircraft deicing vehicle according to claim 1, it is characterized in that: the both sides, other end top of described lengthened plate (7) arrange and coordinate ring (8), the both sides of pull groove (10) arrange several set collar (5), one of them set collar (5) with coordinate ring (8) by fixed link (9) company of wearing.
3. a kind of aircraft deicing vehicle according to claim 1, is characterized in that: safe chair (6) is installed on the top, one end that described lengthened plate (7) stretches out landing slab (3).
4. a kind of aircraft deicing vehicle according to claim 1, is characterized in that: the periphery of described landing slab (3) arranges guardrail (4).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520960188.4U CN205131684U (en) | 2015-11-27 | 2015-11-27 | Deicing vehicle for airplane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520960188.4U CN205131684U (en) | 2015-11-27 | 2015-11-27 | Deicing vehicle for airplane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205131684U true CN205131684U (en) | 2016-04-06 |
Family
ID=55617501
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520960188.4U Expired - Fee Related CN205131684U (en) | 2015-11-27 | 2015-11-27 | Deicing vehicle for airplane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205131684U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105882998A (en) * | 2016-04-26 | 2016-08-24 | 郭玉 | Hot-air quick defrosting vehicle |
| CN109018374A (en) * | 2018-08-19 | 2018-12-18 | 晨龙飞机（荆门）有限公司 | A kind of continuous deicer of wing |
| CN109987236A (en) * | 2017-12-29 | 2019-07-09 | 湖北省专用汽车研究院 | A kind of self-adapting deicing executive device of steam jet deicing vehicle |
-
2015
- 2015-11-27 CN CN201520960188.4U patent/CN205131684U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105882998A (en) * | 2016-04-26 | 2016-08-24 | 郭玉 | Hot-air quick defrosting vehicle |
| CN109987236A (en) * | 2017-12-29 | 2019-07-09 | 湖北省专用汽车研究院 | A kind of self-adapting deicing executive device of steam jet deicing vehicle |
| CN109018374A (en) * | 2018-08-19 | 2018-12-18 | 晨龙飞机（荆门）有限公司 | A kind of continuous deicer of wing |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| 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: 20160406 Termination date: 20161127 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |