CN204713426U - Aircraft can peel off formula film-type deicer - Google Patents
Aircraft can peel off formula film-type deicer Download PDFInfo
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- CN204713426U CN204713426U CN201520269669.0U CN201520269669U CN204713426U CN 204713426 U CN204713426 U CN 204713426U CN 201520269669 U CN201520269669 U CN 201520269669U CN 204713426 U CN204713426 U CN 204713426U
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- film
- peel
- heater mat
- power supply
- heating power
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Abstract
In order to overcome the deficiency of existing aircraft deicing technology, the utility model proposes a kind of aircraft and can peel off formula film-type de-icing method, it is the position easily frozen at airplane skin, paste one or more layers and reduce the film that thus can peel off by viscosity during electro heat, freezing on it is together peeled off by this film, reaches deicing effect.This film is designed to polylith splicing, and also bulk film can arrange the impression or line of cut being convenient to tear, the glue of sticking film easily falls low-viscosity viscose glue after selecting and being heated.Have one deck electric heating layer between film and fuselage and between film and film, electric heating layer is electrically connected with heating power supply.When temperature sensor or inductor sense icing on aircraft, heating power supply conducting, by heater mat homogeneous heating, conducted heat on the glue of film by the heater mat heated, its viscosity is reduced, film is torn along mesh lines and together peels off down with the ice sheet on it, reaches aircraft deicing object.
Description
Technical field
This technology belongs to aircraft deicing field, relates to aircraft furtherly and can peel off formula film-type deicer.
Technical background
At present, aircraft deicing is a difficult problem, and especially in time freezing in aircraft high-altitude flight way, limit flight limit deicing is difficult especially.Have technology to claim airplane skin is heated, but practical application there is no feasibility.
Summary of the invention
In order to overcome the deficiency of existing aircraft deicing technology, the utility model proposes a kind of aircraft and can peel off formula film-type deicer, it is the position easily frozen at airplane skin, paste one or more layers and reduce the film that thus can peel off by viscosity during electro heat, freezing on it is together peeled off by this film, reaches deicing effect.
Realizing the technical solution of the utility model is, at the position sticking film that aircraft fuselage cover is easily frozen, film is designed to polylith splicing, and also bulk film can arrange the impression or line of cut being convenient to tear, the glue of sticking film easily falls low-viscosity viscose glue after selecting and being heated.Have one deck electric heating layer between film and fuselage and between film and film, electric heating layer is electrically connected with heating power supply.When temperature sensor or inductor sense icing on aircraft, heating power supply conducting, by heater mat homogeneous heating, conducted heat on the glue of film by the heater mat heated, its viscosity is reduced, film is torn along mesh lines and together peels off down with the ice sheet on it, reaches aircraft deicing object.
Accompanying drawing explanation
Fig. 1 is heater mat and film schematic cross section on airplane skin.
Fig. 2 is that film divides Block tridiagonal systems schematic diagram.
Fig. 3 is film cut-off rule schematic diagram.
Fig. 4 is thermal cutting and method of heating schematic diagram.
Fig. 5 is folded projections schematic diagram.
Fig. 6 is additional projection thing schematic diagram.
In Fig. 1,1. airplane skin, 2. adhered layer, 3. heater mat, 4. film, 11. ice sheets.
In Fig. 2,5. piecemeal splicing line, 6. film piecemeal.
In Fig. 3,6. film piecemeal, 7. cut-off rule.
In Fig. 4,6. film piecemeal, 8. fervent secant, 9. heating power supply, 10. wire.
In Fig. 5,5. piecemeal splicing line, 6. film piecemeal, 12. folded projections.
In Fig. 6,5. piecemeal splicing line, 6. film piecemeal, 13. additional projection.
Detailed description of the invention
In Fig. 1, airplane skin 1 has adhered layer 2, adhered layer 2 has heater mat 3, heater mat 3 has adhered layer 2, adhered layer 2 has film 4.---heater mat---adhered layer---film, can multilayer repeatedly as required for adhered layer.In practical application, adhered layer 2 can be independent one deck, also can be the adhesive-layer (be commonly called as " gum) that film 4 inherently adheres to; Also can be mixed with conductive material in adhered layer 2, namely heater mat 3 and adhered layer 2-in-1 two be one.
In Fig. 2, whole film is spliced by polylith film piecemeal 6, every block film piecemeal 6 and adjacent between form piecemeal splicing line 5.
In Fig. 3, bulk film, it has cut-off rule 7 be divided into film piecemeal 6; Cut-off rule 7 can be the line as the sawtooth hole composition on stamp, also can be the line of cut do not cut, certainly may also be by any way be conducive to reduce the disposal that bulk strength and being conducive to tears from cut-off rule.
In Fig. 4, fervent secant 8 is made up of heating wire, and fervent secant 8 layout setting will coincide with piecemeal splicing line 5 or cut-off rule 7, and fervent secant is electrically connected with heating power supply 9 by wire 10.
Embodiment 1
On airplane skin 1 surface, to be spliced bulk and even whole film 4 with polylith film piecemeal 6, every block film piecemeal 6 is independent, forms piecemeal splicing line 5 between adjacent, in piecemeal splicing line 5 corresponding position, be distributed with the fervent secant 8 of resistor wire composition, between film 4 and airplane skin 1, and between film 4 and film 4, there is heater mat 3, after airplane skin 1 freezes, connect heater mat 3 heating power supply 9, and connect the fervent secant 8 be made up of resistor wire, like this, ice sheet 11 melts from piecemeal splicing line 5 or cut-off rule 7 place by fervent secant 8, ice sheet 11 is made to form the thawing line matched with the piecemeal splicing line 5 of film piecemeal 6, namely ice sheet is cut into the sheet ice sheet of fritter one fritter by fervent secant 8, at this moment, owing to connecting the heating power supply 9 of heater mat 3, thus adhered layer 2 also heats by heater mat 3, after adhered layer 2 is heated, viscosity declines, thus ice sheet 11 is peeled off down by one piece of block, serve deicing effect, heater mat 3 is Electric radiant Heating Film preferably.
Embodiment 2
Embodiment 2 is roughly the same with embodiment 1, difference be embodiment 2 be the bulk film having cut-off rule 7, after airplane skin 1 freezes, connect heating power supply 9 and fervent secant 8 power supply of heater mat 3, film 4 is torn from cut-off rule 7 and peels off, and is also torn from cut-off rule 7 peels off with one piece of ice cube layer 11.
Described film 4 is the film of any Pasting.Cut-off rule 7 is physical segmentation or chemical method segmentation.
Embodiment 3
In Fig. 5,5. piecemeal splicing line, 6. film piecemeal, 12. folded projections.Folded projections 12 is exactly by edge fold in the edge of film piecemeal 6, form the folded projections 12 with film piecemeal 6 plane certain angle, after the effect of this folded projections 12 is film piecemeal 6 freezes, by the ice sheet that comes off film piecemeal 6 can be torn from splicing line 5 by the tightly coated folded projections 12 of ice sheet 11 and drop.
Embodiment 4
In Fig. 6,5. piecemeal splicing line, 6. film piecemeal, 13. additional projection.Additional projection 13 is exactly the edge's additional projection thing at film piecemeal 6, form additional projection 13, after the effect of this additional projection 13 is film piecemeal 6 freezes, by the ice sheet that comes off film piecemeal 6 can be torn from splicing line 5 by the tightly coated additional projection 13 of ice sheet 11 and drop.This additional projection 13 can be original setting on film piecemeal 6, also can add up by suppressing or pasting.
Described adhered layer (2) is heat-foamable material, refers in viscose glue and is added with the material that heat produces bubble.When heater mat 3 heats, in viscose glue, produce bubble, film 4 is heaved, reduces its adhesion firmness, be convenient to it and carry ice sheet 11 and together peel off.
Described film 4 is heat deformable material, refers to that film 4 can adopt heat-shrinkage material, thermal expansion material and other heat deformable material.When heater mat 3 heats, the film 4 be made up of heat deformable material on it or contraction, or expand, or do other distortion, be convenient to its ice sheet 11 carried on it and come off.
Described film 4 is heat softener material, and referring to that film 4 adopts after heated can deliquescing, the material that even can liquefy or vaporize, and is also that just ice sheet 11 is thereon peeled off.Described film (4) comprises paper, plastics, textile cloth, nonwoven cloth, silk screen, all planar solid things of filter screen, also comprises that can brush and be sprayed on solid can the liquid coating of film former, and this liquid coating is wanted to solidify.Actual to use, can by film coating and adhered layer and the two-in-one or three-in-one application of heater mat.Such as, can add conductive material in adhered layer, form thin film layer, be also film coating, adhered layer and heater mat three laminated.
Claims (10)
1. aircraft can peel off formula film-type deicer, comprise airplane skin, film, adhered layer, heater mat, heating power supply, fervent secant, it is characterized in that, airplane skin (1) is provided with adhered layer (2), heater mat (3), film (4), earnestly secant (8) and heating power supply (9); Airplane skin (1) is pasted with at least one deck and above film (4), there is heater mat (3) between film (4) and airplane skin (1), between film (4) and film (4), also have heater mat (3); Between layers, there is adhered layer (2) adhesion, the material that adhered layer (2) reduces for viscosity after being heated; Heater mat (3) is connected to heating power supply (9), fervent secant (8) also connects heating power supply (9), the ice sheet of airplane skin (1) (11) can be divided into independent sheet after connecting heating power supply (9) by fervent secant (8); By heating power supply (9) to heater mat (3) heating, film (4) viscosity can be made to reduce; When heater mat (3) and fervent secant (8) heat simultaneously, ice sheet (11) just comes off from airplane skin (1).
2. aircraft according to claim 1 can peel off formula film-type deicer, described heater mat (3) is conductivity type thin-film, heater mat (3) is electrically connected with heating power supply (9), when after heater mat (3) energising, heater mat (3) is heated properly, by the heater mat (3) heated, the adhered layer (2) on it is heated, reduce its caking ability, so that film (4) drives the ice sheet on it (11) to peel off from airplane skin (1); Described film (4) comprises paper, plastics, textile cloth, nonwoven cloth, silk screen, all planar solid things of filter screen, also comprises that can brush and be sprayed on solid can the liquid coating of film former, and this liquid coating is wanted to solidify.
3. according to claim 1ly peel off formula film-type de-icing method, its heater mat (3) is conductivity type adhesive coating, conductivity type adhesive coating and heater mat (3) unite two into one, and be electrically connected with heating power supply, when after the energising of conductivity type adhesive coating, conductivity type adhesive coating is heated properly, and its caking ability is lowered, so that film (4) drives the ice sheet on it (11) to peel off from airplane skin (1).
4. aircraft according to claim 1 can peel off formula film-type deicer, its film (4) is pieced together for polylith film piecemeal (6), to form more large-area pad pasting, be attached on airplane skin (1), between film piecemeal (6) is adjacent, form piecemeal splicing line (5).
5. aircraft according to claim 1 can peel off formula film-type deicer, its film (4) is provided with cut-off rule 7, cut-off rule 7 is by bulk film (4) split into grid shape, be convenient to tear from airplane skin drop to reduce film (4) whole Zhang Qiangdu, the film (4) of bulk is separated into some closed film piecemeals (6) by this cut-off rule 7, the object of this cut-off rule 7 is, when film (4) is subject to ice sheet (11) pulling force, can tears from cut-off rule 7 and come off.
6. aircraft according to claim 1 can peel off formula film-type deicer, its fervent secant (8) is the hot Silk of the latticed electricity of composition, fervent secant (8) will coincide with piecemeal splicing line (5) and cut-off rule 7, the two poles of the earth of this heating wire are electrically connected with heating power supply (9), when after fervent secant (8) energising, by the fervent secant (8) heated, its ice sheet along the line (11) is melted, be convenient to it and peeled off by one piece of block from airplane skin (1).
7. aircraft according to claim 1 can peel off formula film-type deicer, and its adhered layer (2) is heat expanded material.
8. aircraft according to claim 1 can peel off formula film-type deicer, and its film (4) is heat deformable material.
9. aircraft according to claim 1 can peel off formula film-type deicer, and its film (4) is heat softener material.
10. film piecemeal (6) according to claim 4, its edge is set to convex shape, and this convex shape comprises the folded projections of edge fold (12) and additional projection (13).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520269669.0U CN204713426U (en) | 2015-04-20 | 2015-04-20 | Aircraft can peel off formula film-type deicer |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520269669.0U CN204713426U (en) | 2015-04-20 | 2015-04-20 | Aircraft can peel off formula film-type deicer |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204713426U true CN204713426U (en) | 2015-10-21 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520269669.0U Expired - Fee Related CN204713426U (en) | 2015-04-20 | 2015-04-20 | Aircraft can peel off formula film-type deicer |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112629093A (en) * | 2021-03-09 | 2021-04-09 | 中国空气动力研究与发展中心低速空气动力研究所 | Method for removing ice growing on surface of film hot knife and model |
-
2015
- 2015-04-20 CN CN201520269669.0U patent/CN204713426U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112629093A (en) * | 2021-03-09 | 2021-04-09 | 中国空气动力研究与发展中心低速空气动力研究所 | Method for removing ice growing on surface of film hot knife and model |
| CN112629093B (en) * | 2021-03-09 | 2021-07-02 | 中国空气动力研究与发展中心低速空气动力研究所 | Method for removing ice growing on surface of film hot knife and model |
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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: 20151021 Termination date: 20160420 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |