CN202389271U - Deicing vehicle for airplane - Google Patents
Deicing vehicle for airplane Download PDFInfo
- Publication number
- CN202389271U CN202389271U CN2011205258613U CN201120525861U CN202389271U CN 202389271 U CN202389271 U CN 202389271U CN 2011205258613 U CN2011205258613 U CN 2011205258613U CN 201120525861 U CN201120525861 U CN 201120525861U CN 202389271 U CN202389271 U CN 202389271U
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- CN
- China
- Prior art keywords
- spray gun
- speed spray
- deicing
- high speed
- heating pipe
- 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 discloses a deicing vehicle for an airplane. The deicing vehicle comprises a vehicle body, a nanometre heating tube, and a high-speed spray gun, wherein a water tank is arranged on the vehicle body, the water tank is communicated with the nanometre heating tube, and the nanometre heating tube generates steam and then sprays the steam by the high-speed spray gun. The deicing vehicle for an airplane disclosed by the utility model generates steam by adopting the nanometre heating tube, and then sprays the steam by utilizing the high-speed spray gun, thus performing deicing treatment on the surface of the airplane, so that the deicing efficiency can be greatly increased, and the operation safety of the airplane can be enhanced.
Description
Technical field
The utility model discloses a kind of ice machine that removes, and particularly a kind of aircraft deicing vehicle belongs to civil aviaton's specialized equipment.
Background technology
Along with the scale of China civil aviaton and the continuous growth of transportation volume, aircraft increasing become in people's daily life first-selected transport facility, aircraft is in operational process, safety is primary all the time.Discover that if whenever divide a centimetre frost point of going up one 1 mm dia that distributes on the fuselage equally, the raising force of aircraft will reduce 33%; Very easily cause aircraft stall in take-off process to crash; Therefore, how removing freezing on the airframe, is the maximum demand for security of aircraft safe in operation in winter.The Civil Aviation Airport badly influences the operation of aircraft to the deicing ability of aircraft, and the deicing ability of a lot of Civil Aviation Airport is not enough in the winter time, is the major reason that causes aircraft late.
Summary of the invention
To the not enough shortcoming of the deicing ability of the above-mentioned Civil Aviation Airport of mentioning of the prior art; The utility model provides a kind of aircraft deicing vehicle, and it adopts the nanometer heating pipe to produce steam, is going out through the high speed lance ejection; Aircraft surfaces is carried out deicing handle, increased the deicing ability greatly.
The technical scheme that its technical matters that solves the utility model adopts is: a kind of aircraft deicing vehicle; Remove ice machine and comprise car body, nanometer heating pipe and high speed spray gun; Car body is provided with water tank, and water tank is communicated with the nanometer heating pipe, and the nanometer heating pipe is sprayed by the high speed spray gun after producing steam.
The technical scheme that its technical matters that solves the utility model adopts further comprises:
The described ice machine that removes also includes force (forcing) pump, and the steam that the nanometer heating pipe produces is sprayed by the high speed spray gun after the force (forcing) pump pressurization.
The described ice machine that removes also includes bay-lift or aerial ladder, and bay-lift or aerial ladder are installed on the car body, and the high speed spray gun is installed on bay-lift or the aerial ladder.
The beneficial effect of the utility model is: the utility model adopts the nanometer heating pipe to produce steam, and then utilizes the high speed spray gun to spray, and handles thereby aircraft surfaces is carried out deicing, can increase deicing efficiency greatly, strengthens the safety of aircraft operation.
To combine the accompanying drawing and the specific embodiment that the utility model is further specified below.
Description of drawings
Fig. 1 is the utility model embodiment one structural representation.
Fig. 2 is the utility model embodiment two structural representations.
Among the figure, 1-car body, 2-high speed spray gun, 3-bay-lift, 4-aerial ladder.
The specific embodiment
Present embodiment is the utility model preferred implementation, and other all its principles are identical with present embodiment or approximate with basic structure, all within the utility model protection domain.
Please referring to accompanying drawing 1, the utility model main body is a car body 1, and car body 1 is the supporting body of the utility model; In the present embodiment, be installed with water tank on the car body 1, the water tank the inside is mounted with water or other ice-melt liquid; Water in the water tank is through the heating of nanometer heating pipe; Produce high-temperature steam, through 2 ejections of high speed spray gun, aircraft surfaces is carried out deicing then.In the present embodiment, also be provided with force (forcing) pump in the car body 1, the steam that the nanometer heating pipe produces becomes high pressure steam after the force (forcing) pump pressurization, and then through 2 ejections of high speed spray gun.In the present embodiment, bay-lift 3 is installed on car body 1, high speed spray gun 2 is fixedly mounted on the bay-lift 3, can make its airframe to differing heights carry out ice-melt through the height of bay-lift 3 rising high speed spray guns 2.During practical implementation; Nanometer heating pipe and force (forcing) pump can be installed on the car body 1; Through pipeline high temperature and high pressure steam is transported on the high speed spray gun 2; Also can nanometer heating pipe and force (forcing) pump be directly installed on the bay-lift 3, the water in the water tank be pumped in the nanometer heating pipe, it is vaporized through water pump.
Please referring to accompanying drawing 2, the basic structure of present embodiment is identical with embodiment one, and difference is, in the present embodiment, aerial ladder 4 is installed on car body 1, and high speed spray gun 2 is installed on the aerial ladder 4, regulates the height of high speed spray gun 2 through aerial ladder 4.
The utility model adopts the nanometer heating pipe to produce steam, and then utilizes the high speed spray gun to spray, and handles thereby aircraft surfaces is carried out deicing, can increase deicing efficiency greatly, strengthens the safety of aircraft operation.
Claims (3)
1. aircraft deicing vehicle is characterized in that: the described ice machine that removes comprises car body, nanometer heating pipe and high speed spray gun, and car body is provided with water tank, and water tank is communicated with the nanometer heating pipe, is sprayed by the high speed spray gun behind the nanometer heating pipe generation steam.
2. aircraft deicing vehicle according to claim 1 is characterized in that: the described ice machine that removes also includes force (forcing) pump, and the steam that the nanometer heating pipe produces is sprayed by the high speed spray gun after the force (forcing) pump pressurization.
3. aircraft deicing vehicle according to claim 1 and 2 is characterized in that: the described ice machine that removes also includes bay-lift or aerial ladder, and bay-lift or aerial ladder are installed on the car body, and the high speed spray gun is installed on bay-lift or the aerial ladder.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011205258613U CN202389271U (en) | 2011-12-15 | 2011-12-15 | Deicing vehicle for airplane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011205258613U CN202389271U (en) | 2011-12-15 | 2011-12-15 | Deicing vehicle for airplane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202389271U true CN202389271U (en) | 2012-08-22 |
Family
ID=46664217
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2011205258613U Expired - Fee Related CN202389271U (en) | 2011-12-15 | 2011-12-15 | Deicing vehicle for airplane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202389271U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105672680A (en) * | 2016-02-05 | 2016-06-15 | 赵宽学 | High-altitude deicing machine |
| CN105882998A (en) * | 2016-04-26 | 2016-08-24 | 郭玉 | Hot-air quick defrosting vehicle |
| CN113895647A (en) * | 2021-10-11 | 2022-01-07 | 滨州学院 | Novel steam jet multifunctional aircraft deicing vehicle |
-
2011
- 2011-12-15 CN CN2011205258613U patent/CN202389271U/en not_active Expired - Fee Related
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105672680A (en) * | 2016-02-05 | 2016-06-15 | 赵宽学 | High-altitude deicing machine |
| CN105672680B (en) * | 2016-02-05 | 2017-12-01 | 赵宽学 | A kind of high-altitude ice removing machine |
| CN105882998A (en) * | 2016-04-26 | 2016-08-24 | 郭玉 | Hot-air quick defrosting vehicle |
| CN113895647A (en) * | 2021-10-11 | 2022-01-07 | 滨州学院 | Novel steam jet multifunctional aircraft deicing vehicle |
| CN113895647B (en) * | 2021-10-11 | 2023-01-17 | 滨州学院 | Steam jet multifunctional aircraft deicing vehicle |
| WO2023060712A1 (en) * | 2021-10-11 | 2023-04-20 | 滨州学院 | Novel steam jet multifunctional aircraft deicing vehicle |
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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: 20120822 Termination date: 20201215 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |