CN105648875A - Airplane anti-icing runway - Google Patents
Airplane anti-icing runway Download PDFInfo
- Publication number
- CN105648875A CN105648875A CN201610076419.4A CN201610076419A CN105648875A CN 105648875 A CN105648875 A CN 105648875A CN 201610076419 A CN201610076419 A CN 201610076419A CN 105648875 A CN105648875 A CN 105648875A
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- China
- Prior art keywords
- runway
- honeycomb
- layer
- heat
- electrothermal tube
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- E—FIXED CONSTRUCTIONS
- E01—CONSTRUCTION OF ROADS, RAILWAYS, OR BRIDGES
- E01C—CONSTRUCTION OF, OR SURFACES FOR, ROADS, SPORTS GROUNDS, OR THE LIKE; MACHINES OR AUXILIARY TOOLS FOR CONSTRUCTION OR REPAIR
- E01C11/00—Details of pavings
- E01C11/24—Methods or arrangements for preventing slipperiness or protecting against influences of the weather
- E01C11/26—Permanently installed heating or blowing devices ; Mounting thereof
- E01C11/265—Embedded electrical heating elements ; Mounting thereof
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- Engineering & Computer Science (AREA)
- Architecture (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- Road Paving Structures (AREA)
Abstract
The invention discloses an airplane anti-icing runway. The airplane anti-icing runway comprises a controller, a connecting circuit, temperature detectors, an airplane runway body, a water supply system and a water drainage system. The airplane runway body is divided into five layers and sequentially comprises an anti-abrasion layer, a heat conduction layer, an anti-electromagnetic-interference layer, an insulating layer and a heat insulating layer from top to bottom. The insulating layer is filled with fillers and a honeycomb electrical heated tube. The controller controls the honeycomb electrical heated tube to work and produce heat. According to the airplane anti-icing runway, the heat produced through the honeycomb electrical heated tube is transferred to the upper surface of the runway, and after ice and snow are melted, snow water flows into the water drainage system through permeation and drain holes; by means of the system, the accumulated snow and the frozen ice on the airplane runway body are made to be directly melted without being shoveled after snowing, so that an airplane takes off and lands normally.
Description
Technical field
The present invention relates to runway field, be specifically related to a kind of anti-freeze runway of aircraft.
Background technology
At present, changeable weather and the delayed flight that causes happens occasionally, particularly the heavy snow in winter is given and is taken off the inconvenience that landing brings, and often all needs airport is closed, causes a large amount of passenger to be detained. Be on the one hand that aircraft mechanical part is existed certain impact by cold weather, another aspect is frozen covering for runway by accumulated snow, and aircraft cannot normally take off landing; Conventional way is that runway is cleaned by the employing deicing vehicle that clears the snow, but the method inefficiency, needs many and cleans simultaneously, length consuming time and also the deicing vehicle that clears the snow is with high costs.
Summary of the invention
It is an object of the invention to the problem above overcoming prior art to exist, for aircraft snowfield ice landing of taking off a kind of scheme quick, safe and effective is provided, without rooting out accumulated snow on runway and freezing after snow, directly melt accumulated snow on runway and freeze, for taking off landing.
For realizing above-mentioned technical purpose, reaching above-mentioned technique effect, the present invention is achieved through the following technical solutions:
A kind of anti-freeze runway of aircraft, including controller, connects circuit, temperature-detecting device, runway, supply and drain water system, it is characterised in that: described controller, temperature-detecting device, runway connect by connecting circuit; Described temperature-detecting device is arranged on runway both sides; Described runway is divided into five layers, is followed successively by wearing layer, heat-conducting layer, anti-electromagnetic interference layer, insulating barrier, insulating layer from top to bottom; Described wearing layer scribbles wear-resistant coating, heat-conducting layer transmission heat, anti-electromagnetic interference layer shields the electromagenetic wave radiation that lower floor's electric current produces; Described wearing layer, heat-conducting layer, anti-electromagnetic interference layer are un-densified many hollow structures; Inserts, honeycomb electrothermal tube it is provided with in described insulating barrier; Described inserts is provided with osculum; Described insulating layer trap heat is transmitted to underground, connects supply and drain water system under insulating layer; Described controller controls the work of honeycomb electrothermal tube, produce heat the accumulated snow reaching on runway by heat by heat-conducting layer, by snow melting, the melt water melted through wearing layer, heat-conducting layer, anti-electromagnetic interference layer to the osculum of insulating barrier, it flow to insulating layer again, eventually enter in supply and drain water system.
Further, described honeycomb electrothermal tube mode of operation is quick heating mode, holding mode;Described temperature-detecting device arranges and is spaced apart 10 meters, and when snowing, honeycomb electrothermal tube is set to quick heating mode by controller, is signaled to controller when temperature-detecting device detection temperature is higher than 5 DEG C, and honeycomb electrothermal tube is holding mode by controller.
Further, described inserts is wrapped with insulation honeycomb electrothermal tube, and inserts is hydrophobic material.
Further, described honeycomb electrothermal tube is internal is electrothermal tube, outer wrap insulation sleeve, and insulation wall thickness is more than 2mm, and the honeycomb electrothermal tube length of side is more than 100mm.
Further, described wearing layer thickness is more than 20mm.
Further, described honeycomb electrothermal tube is non-closed-loop structure, is provided with upper contactor, lower contactor, contravention gap; Described upper contactor, lower contactor are sequentially ingressed into connection circuit by both positive and negative polarity unanimously order; Described contravention gap is between upper contactor, lower contactor, and the gap width in contravention gap is more than 10mm.
The invention has the beneficial effects as follows: the present invention is aircraft snowfield ice, and landing of taking off provides a kind of scheme quick, safe and effective, controller is utilized to control heat transmission runway upper surface produced by honeycomb electrothermal tube, after melting ice and snow, snow water flow in drainage system by permeating with osculum, this system make snow after without the accumulated snow of rooting out on runway with freeze, directly melt the ice and snow on runway, in order to aircraft normally takes off landing.
Described above is only the general introduction of technical solution of the present invention, in order to better understand the technological means of the present invention, and can be practiced according to the content of description, below with presently preferred embodiments of the present invention and coordinate accompanying drawing describe in detail as after. The specific embodiment of the present invention is shown in detail in by following example and accompanying drawing thereof.
Accompanying drawing explanation
Accompanying drawing described herein is used for providing a further understanding of the present invention, constitutes the part of the application, and the schematic description and description of the present invention is used for explaining the present invention, is not intended that inappropriate limitation of the present invention. In the accompanying drawings:
Fig. 1 is the anti-freeze runway runway layering schematic diagram of aircraft of the present invention;
Fig. 2 is the insulating barrier section partial schematic diagram of the present invention;
Fig. 3 is a kind of honeycomb electrothermal tube schematic diagram of the present invention;
Fig. 4 is a kind of honeycomb electrothermal tube partial schematic diagram of the present invention;
Number in the figure illustrates: wearing layer 1, heat-conducting layer 2, insulating barrier 3, insulating layer 4, osculum 5, inserts 6, honeycomb electrothermal tube 7, anti-electromagnetic interference layer 21, upper contactor 71, lower contactor 72, contravention gap 73.
Detailed description of the invention
Below with reference to the accompanying drawings and in conjunction with the embodiments, the present invention is described in detail.
With reference to shown in Fig. 1-4, including controller, connecting circuit, temperature-detecting device, runway, supply and drain water system, it is characterised in that: described controller, temperature-detecting device, runway connect by connecting circuit; Described temperature-detecting device is arranged on runway both sides; Described runway is divided into five layers, is followed successively by wearing layer 1, heat-conducting layer 2, anti-electromagnetic interference layer 21, insulating barrier 3, insulating layer 4 from top to bottom; Scribbling wear-resistant coating on described wearing layer 1, heat-conducting layer 2 transmits heat, and anti-electromagnetic interference layer 21 shields the electromagenetic wave radiation that lower floor's electric current produces; Described wearing layer 1, heat-conducting layer 2, anti-electromagnetic interference layer 21 are un-densified many hollow structures, in order to the snow water of thawing can pass through smoothly; Inserts 6, honeycomb electrothermal tube 7 it is provided with in described insulating barrier 3;Described inserts 6 is provided with osculum 5; Described insulating layer 4 trap heat is transmitted to underground, and insulating layer connects supply and drain water system 4 times; Described controller controls honeycomb electrothermal tube 7 and works, produce heat the accumulated snow reaching on runway by heat by heat-conducting layer 2, by snow melting, the melt water melted passes through the osculum 5 of wearing layer 1, heat-conducting layer 2, anti-electromagnetic interference layer 21 to insulating barrier 3, it flow to insulating layer again, eventually enter in supply and drain water system. The electromagenetic wave radiation that operating current produces is completely cut off by anti-electromagnetic interference layer 21.
Further, described honeycomb electrothermal tube 7 mode of operation is quick heating mode, holding mode; Described temperature-detecting device arranges and is spaced apart 10 meters, and when snowing, honeycomb electrothermal tube 7 is set to quick heating mode by controller, is signaled to controller when temperature-detecting device detection temperature is higher than 5 DEG C, and honeycomb electrothermal tube 7 is holding mode by controller.
Further, described inserts 6 is wrapped with insulation honeycomb electrothermal tube 7, and inserts 6 is hydrophobic material, it is prevented that honeycomb electrothermal tube 7 is caused short circuit or corrosion by water, makes the snow water following current of thawing to osculum 5.
Further, described honeycomb electrothermal tube 7 is internal is electrothermal tube, outer wrap insulation sleeve, and insulation wall thickness is more than 2mm, and honeycomb electrothermal tube 7 length of side is more than 100mm.
Further, described wearing layer 1 thickness is more than 20mm. Wearing layer hardness is high, not easy to wear.
Further, described honeycomb electrothermal tube 7 is non-closed-loop structure, is provided with upper contactor 71, lower contactor 72, contravention gap 73; Described upper contactor 71, lower contactor 72 are sequentially ingressed into connection circuit by both positive and negative polarity unanimously order; Described contravention gap 73 is between upper contactor 71, lower contactor 72, and the gap width in contravention gap 73 is more than 10mm. Current direction is stable, stops the phenomenon that short circuit is uneven with heating.
The present invention is aircraft snowfield ice, and landing of taking off provides a kind of scheme quick, safe and effective, controller is utilized to control heat transmission runway upper surface produced by honeycomb electrothermal tube, after melting ice and snow, snow water flow in drainage system by permeating with osculum, this system make snow after without the accumulated snow of rooting out on runway with freeze, directly melt the ice and snow on runway, in order to aircraft normally takes off landing.
The above, be only presently preferred embodiments of the present invention, and the present invention not does any pro forma restriction; The those of ordinary skill of all industry all can shown in by specification accompanying drawing and the above and implement the present invention swimmingly; But, all those skilled in the art without departing within the scope of technical solution of the present invention, utilize disclosed above technology contents and make a little change, modify and the equivalent variations of differentiation, be the Equivalent embodiments of the present invention; Meanwhile, all change of any equivalent variations, modification and differentiation etc. above example made according to the substantial technological of the present invention, all still fall within the protection domain of technical scheme.
Claims (6)
1. the anti-freeze runway of aircraft, including controller, connects circuit, temperature-detecting device, runway, supply and drain water system, it is characterised in that: described controller, temperature-detecting device, runway connect by connecting circuit; Described temperature-detecting device is arranged on runway both sides; Described runway is divided into five layers, is followed successively by wearing layer (1), heat-conducting layer (2), anti-electromagnetic interference layer (21), insulating barrier (3), insulating layer (4) from top to bottom;Described wearing layer (1) scribbles wear-resistant coating, heat-conducting layer (2) transmission heat, anti-electromagnetic interference layer (21) shields the electromagenetic wave radiation that lower floor's electric current produces; Described wearing layer (1), heat-conducting layer (2), anti-electromagnetic interference layer (21) are un-densified many hollow structures; Inserts (6), honeycomb electrothermal tube (7) it is provided with in described insulating barrier (3); Described inserts (6) is provided with osculum (5); Described insulating layer (4) trap heat is transmitted to underground, connects supply and drain water system under insulating layer (4); Described controller controls honeycomb electrothermal tube (7) work, produce heat the accumulated snow reaching on runway by heat by heat-conducting layer (2), by snow melting, the melt water melted through wearing layer (1), heat-conducting layer (2), anti-electromagnetic interference layer (21) to the osculum (5) of insulating barrier (3), it flow to insulating layer again, eventually enter in supply and drain water system.
2. a kind of anti-freeze runway of aircraft according to claim 1, it is characterised in that: described honeycomb electrothermal tube (7) mode of operation is quick heating mode, holding mode; Described temperature-detecting device arranges and is spaced apart 10 meters, when snowing, honeycomb electrothermal tube (7) is set to quick heating mode by controller, is signaled to controller when temperature-detecting device detection temperature is higher than 5 DEG C, and honeycomb electrothermal tube (7) is holding mode by controller.
3. a kind of anti-freeze runway of aircraft according to claim 1, it is characterised in that: described inserts (6) is wrapped with insulation honeycomb electrothermal tube (7), and inserts (6) is hydrophobic material.
4. a kind of anti-freeze runway of aircraft according to claim 1, it is characterised in that: described honeycomb electrothermal tube (7) is internal is electrothermal tube, outer wrap insulation sleeve, and insulation wall thickness is more than 2mm, and honeycomb electrothermal tube (7) length of side is more than 100mm.
5. a kind of anti-freeze runway of aircraft according to claim 1, it is characterised in that: described wearing layer (1) thickness is more than 20mm.
6. a kind of anti-freeze runway of aircraft according to claim 1, it is characterised in that: described honeycomb electrothermal tube (7) is non-closed-loop structure, is provided with upper contactor (71), lower contactor (72), contravention gap (73); Described upper contactor (71), lower contactor (72) are sequentially ingressed into connection circuit by both positive and negative polarity unanimously order; Described contravention gap (73) is positioned between upper contactor (71), lower contactor (72), and the gap width of contravention gap (73) is more than 10mm.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610076419.4A CN105648875A (en) | 2016-02-02 | 2016-02-02 | Airplane anti-icing runway |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610076419.4A CN105648875A (en) | 2016-02-02 | 2016-02-02 | Airplane anti-icing runway |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105648875A true CN105648875A (en) | 2016-06-08 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610076419.4A Pending CN105648875A (en) | 2016-02-02 | 2016-02-02 | Airplane anti-icing runway |
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| CN (1) | CN105648875A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108601129A (en) * | 2017-12-29 | 2018-09-28 | 合肥工业大学 | A kind of ice-melt snow electromagnetic heating system |
| CN109487650A (en) * | 2018-10-11 | 2019-03-19 | 东北林业大学 | A kind of winter cities non-motorized lane setting method |
| CN109778635A (en) * | 2019-03-25 | 2019-05-21 | 青岛智慧城市产业发展有限公司 | A kind of automatic snow-melting linked system based on sponge airport |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH04319103A (en) * | 1991-04-18 | 1992-11-10 | Taisei Corp | Regulator for road surface temperature |
| KR100743473B1 (en) * | 2006-03-10 | 2007-07-30 | (주)지케이 | An elastic pavement with a heating layer |
| CN201665809U (en) * | 2010-03-15 | 2010-12-08 | 邵建人 | Anti-freezing airport pavement surface structure |
| RU2414558C2 (en) * | 2008-07-24 | 2011-03-20 | Общество с ограниченной ответственностью "Эдлайн Проект" | Surface heating device |
| CN103276652A (en) * | 2013-05-23 | 2013-09-04 | 陈瑞文 | System capable of automatically removing ice on ground surface by applying natural resources |
| CN104894944A (en) * | 2015-06-25 | 2015-09-09 | 浙江佳中木业有限公司 | Anti-freezing road |
-
2016
- 2016-02-02 CN CN201610076419.4A patent/CN105648875A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH04319103A (en) * | 1991-04-18 | 1992-11-10 | Taisei Corp | Regulator for road surface temperature |
| KR100743473B1 (en) * | 2006-03-10 | 2007-07-30 | (주)지케이 | An elastic pavement with a heating layer |
| RU2414558C2 (en) * | 2008-07-24 | 2011-03-20 | Общество с ограниченной ответственностью "Эдлайн Проект" | Surface heating device |
| CN201665809U (en) * | 2010-03-15 | 2010-12-08 | 邵建人 | Anti-freezing airport pavement surface structure |
| CN103276652A (en) * | 2013-05-23 | 2013-09-04 | 陈瑞文 | System capable of automatically removing ice on ground surface by applying natural resources |
| CN104894944A (en) * | 2015-06-25 | 2015-09-09 | 浙江佳中木业有限公司 | Anti-freezing road |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108601129A (en) * | 2017-12-29 | 2018-09-28 | 合肥工业大学 | A kind of ice-melt snow electromagnetic heating system |
| CN109487650A (en) * | 2018-10-11 | 2019-03-19 | 东北林业大学 | A kind of winter cities non-motorized lane setting method |
| CN109778635A (en) * | 2019-03-25 | 2019-05-21 | 青岛智慧城市产业发展有限公司 | A kind of automatic snow-melting linked system based on sponge airport |
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Application publication date: 20160608 |