CN220721381U - Aircraft fabric with waterproof and sun-proof functions - Google Patents
Aircraft fabric with waterproof and sun-proof functions Download PDFInfo
- Publication number
- CN220721381U CN220721381U CN202322151594.3U CN202322151594U CN220721381U CN 220721381 U CN220721381 U CN 220721381U CN 202322151594 U CN202322151594 U CN 202322151594U CN 220721381 U CN220721381 U CN 220721381U
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- Prior art keywords
- fabric
- aircraft
- cloth
- waterproof
- sun
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- 239000004744 fabric Substances 0.000 title claims abstract description 127
- 230000008093 supporting effect Effects 0.000 claims abstract description 19
- 239000010410 layer Substances 0.000 claims description 30
- 238000009958 sewing Methods 0.000 claims description 15
- 239000002390 adhesive tape Substances 0.000 claims description 14
- BQCADISMDOOEFD-UHFFFAOYSA-N Silver Chemical compound [Ag] BQCADISMDOOEFD-UHFFFAOYSA-N 0.000 claims description 11
- 229910052709 silver Inorganic materials 0.000 claims description 11
- 239000004332 silver Substances 0.000 claims description 11
- 239000011247 coating layer Substances 0.000 claims description 9
- 230000037072 sun protection Effects 0.000 claims description 6
- 230000002093 peripheral effect Effects 0.000 claims description 3
- 239000011248 coating agent Substances 0.000 abstract description 12
- 238000000576 coating method Methods 0.000 abstract description 12
- 238000000034 method Methods 0.000 description 7
- 230000000694 effects Effects 0.000 description 5
- 230000008569 process Effects 0.000 description 5
- 230000009286 beneficial effect Effects 0.000 description 3
- 230000017525 heat dissipation Effects 0.000 description 3
- 238000004519 manufacturing process Methods 0.000 description 3
- 230000002265 prevention Effects 0.000 description 3
- 230000001681 protective effect Effects 0.000 description 3
- 238000009423 ventilation Methods 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 101100269850 Caenorhabditis elegans mask-1 gene Proteins 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 239000000428 dust Substances 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000009413 insulation Methods 0.000 description 1
- 230000001788 irregular Effects 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- 239000004576 sand Substances 0.000 description 1
- 238000004544 sputter deposition Methods 0.000 description 1
- 239000004575 stone Substances 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Landscapes
- Laminated Bodies (AREA)
Abstract
The utility model discloses an aircraft fabric with waterproof and sun-proof functions, which comprises a fabric and strapping, wherein the fabric is provided with an inner layer surface and an outer layer surface, a plurality of supporting bodies are arranged on the inner layer surface of the fabric, the fabric is abutted against a body of an aircraft through the supporting bodies, a plurality of strapping which are symmetrically arranged are arranged on two sides of the fabric, and the fabric can be detachably strapped on the body of the aircraft through the strapping. The aircraft fabric disclosed by the utility model has the waterproof and sun-proof functions, can protect the aircraft skin coating, is convenient to carry and operate, can be used by personnel of different levels, is particularly suitable for outfield work guarantee, greatly improves the working efficiency, has a simple integral structure, is high in practicability, and is suitable for popularization and application.
Description
Technical Field
The utility model relates to the technical field of aircraft masks, in particular to an aircraft mask with waterproof and sun-proof functions.
Background
In the daily parking process of the aircraft, the aircraft is required to be protected by adopting an aircraft fabric, corresponding parts required by the aircraft can be effectively shielded, and the aircraft is firmly fixed by using a binding belt. The common cloth is adopted, so that the requirements can be met in a common environment. In the practical application process, irregular rainwater and intense solar radiation can cause corrosion and damage to the aircraft to a certain extent. In particular, in summer, when the aircraft ground crew performs various maintenance works, the surface temperature of the aircraft skin can reach about 70 ℃, and the aircraft working system can be failed or important parts are damaged due to overhigh temperature, so that huge economic loss can be caused, and the flight task is influenced. Therefore, in order to ensure the flight safety of the aircraft, when the aircraft is parked on the ground, the surface of the aircraft needs to be covered with a cloth. At present, most of aircraft masks are single in form, large in mass and laborious to put on and take off.
Through retrieval, the Chinese patent with the bulletin number of CN 212890997U discloses a fixed-wing aircraft fabric structure, which comprises a machine head fabric, a machine body fabric and a machine tail fabric; the joint of the machine head fabric and the machine body fabric forms an overlapping part, and the joint of the machine body fabric and the machine tail fabric forms an overlapping part; the overlapping part is provided with a buckling structure, and the buckling structure prevents the two fabrics from sliding in a transition manner left and right and enables the two fabrics to be always overlapped and connected. The beneficial effects achieved by the utility model are as follows: the device is suitable for a strong wind environment, firm in connection, good in coating effect and convenient in coating operation.
The Chinese patent with the publication number of CN 210162237U discloses an inflatable aircraft fabric, which comprises: the cloth covering, tensioner, tensioning belt, elastic rope and rubber sleeve hook. The aircraft fabric is inflated to form a prefabricated shape, and the aircraft fabric is lifted and mounted on an aircraft body. The aircraft fabric is simple to install and operate, the installation ladder is not used, an operator can rapidly complete the whole operation, and the aircraft fabric is easy to store and small in size after being deflated.
In addition, the Chinese patent with the bulletin number of CN219277804U discloses an inflatable multifunctional aircraft fabric, which comprises an inner fabric layer, wherein the inner surface of the inner fabric layer is abutted against the airframe of an aircraft; the inner surface of the outer layer of the fabric is abutted against the outer surface of the inner layer of the fabric, and the outer surface of the inner layer and the inner surface of the outer layer are connected in a partial welding mode to form a sealed aircraft fabric; the inflation nozzle is arranged on the inner face of the inner layer and/or the outer face of the outer layer; the temperature control inflator pump is communicated with the inflating nozzle to inflate the aircraft fabric, the aircraft fabric can be rapidly inflated and molded to form an air chamber, and the functions of hail prevention, sand and dust prevention, broken stone prevention and sputtering can be achieved.
In the search of patent literature, the aircraft fabric structure can meet the use requirement, but in the specific application process, the inflatable structure is inconvenient to use. Accordingly, there is an urgent need to improve upon existing aircraft masks to provide an aircraft mask that is different from those disclosed in the prior art in order to meet the operational requirements.
Disclosure of Invention
The utility model aims at solving the technical problems in the background art, and provides the aircraft fabric which is simple in structure and convenient to operate, and can be directly covered on an aircraft, so that the aircraft fabric is convenient to detach, is beneficial to ventilation and heat dissipation of the surface of the aircraft, can protect the aircraft skin coating, and particularly has waterproof and sun-proof functions.
In order to solve the technical problems, the utility model adopts the following technical scheme: the utility model provides an aircraft fabric with waterproof and sun-proof function, is including covering cloth and tie, the covering cloth has interior aspect and outer face be equipped with a plurality of support bodies on the interior aspect of covering cloth, the covering passes through support body looks butt on the fuselage of aircraft the covering cloth both sides are equipped with a plurality of tie that are symmetrical state and arrange, the covering can dismantle the tie on the fuselage of aircraft through the tie.
Furthermore, the aircraft fabric with waterproof and sun-proof functions comprises the sleeve cover and the inner container, wherein the sleeve cover is made of flannelette to form a square or cylindrical structure, the inner container is a sponge inner container, the sleeve cover is filled with sponge to form the sponge inner container, and the support forms a flexible support body through the sleeve cover and the inner container.
Furthermore, the aircraft fabric with waterproof and sun-proof functions is waterproof, the support body is fixed on the fabric in a sewing mode, waterproof adhesive tapes are arranged at the sewing positions, and the waterproof adhesive tapes are PU waterproof adhesive tapes.
Furthermore, the outer layer surface of the aircraft fabric with the waterproof and sun-proof functions is also coated with a silver coating.
Further, the aircraft fabric with the waterproof and sun-proof functions comprises an inner fabric and an outer fabric, the inner fabric and the outer fabric are identical in structure, the outer fabric is arranged on the inner fabric and is sewn on the peripheral edges of the inner fabric and the outer fabric, the inner fabric and the outer fabric form a double-layer integrated structure, and the support body is fixed on the inner layer surface of the inner fabric in a sewing mode.
Further, the outer layer of the aircraft fabric with waterproof and sun-proof functions is coated with a silver coating.
Compared with the existing aircraft fabric, the aircraft fabric with the waterproof and sun-proof functions has the advantages that the overall structure is simple, the weight is light, the carrying is convenient, the operation and the use are convenient, the technical requirements on operators are low, the use of operators at different levels is convenient, the aircraft fabric is particularly suitable for being rapidly worn and unloaded in an external field, the wearing and unloading efficiency of the external field of the aircraft is greatly improved, and the attendance frequency of the external field of the aircraft is ensured; secondly, PU waterproof adhesive tapes are added at sewing positions, and silver coating layers are coated on the outer layers of the cloth, so that the protective performance of the cloth can be enhanced, important parts of an airplane are effectively prevented from being damaged due to rain or insolation, and the working temperature of an airplane system is prevented from being too high; thirdly, the adopted support body forms a flexible support body through the sleeve cover and the liner, so that the aircraft skin is not damaged, and a good protection effect is achieved.
Therefore, the aircraft fabric disclosed by the utility model has the waterproof and sun-proof functions, can play a role in protecting the aircraft skin coating, is convenient to carry and operate, can meet the use requirements of personnel of different levels, is particularly suitable for outfield work guarantee, greatly improves the working efficiency, has a simple integral structure and strong practicability, and is suitable for popularization and application.
Drawings
The utility model is described in further detail below with reference to the accompanying drawings.
FIG. 1 is a schematic diagram of the structure of the present utility model;
FIG. 2 is a second schematic diagram of the structure of the present utility model;
fig. 3 is a schematic view of the structure of the present utility model in use.
The figure shows: 1-cloth, 2-strapping, 3-supporter, 31-cover, 32-inner bag, 4-silvered coating, 5-aircraft skin.
Detailed Description
Further advantages and effects of the present utility model will become apparent to those skilled in the art from the disclosure of the present utility model, which is described by the following specific examples.
It should be understood that the structures, proportions, sizes, etc. shown in the drawings are for illustration purposes only and should not be construed as limiting the utility model to the extent that it can be practiced, since modifications, changes in the proportions, or adjustments of the sizes, which are otherwise, used in the practice of the utility model, are included in the spirit and scope of the utility model which is otherwise, without departing from the spirit or scope thereof. Also, the terms such as "upper", "lower", "left", "right" and the like are used herein for descriptive purposes only and are not intended to limit the scope of the utility model for which the utility model may be practiced.
In the description of the present utility model, it should be noted that, unless explicitly stated and limited otherwise, the terms "connected", "provided" and "having a meaning of" connected "are to be interpreted in a broad sense, and may be, for example, fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; can be directly connected or indirectly connected through an intermediate medium. The specific meaning of the above terms in the present utility model will be understood in specific cases by those of ordinary skill in the art.
It should be noted that the term "comprises," "comprising," or any other variation thereof is intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.
Example 1
As shown in fig. 1 to 3, an aircraft fabric with waterproof and sun-proof functions according to this embodiment includes a fabric 1 and a binding belt 2, the fabric 1 has an inner layer and an outer layer, a plurality of supporting bodies 3 are arranged on the inner layer of the fabric 1, the fabric 1 is abutted to the body of the aircraft through the supporting bodies 3, a plurality of binding belts 2 which are symmetrically arranged are arranged on two sides of the fabric 1, and the fabric 1 is detachably bound to the body of the aircraft through the binding belt 2.
For waterproof, the cover cloth 1 is waterproof, the support body 3 is fixed on the cover cloth 1 in a sewing mode, waterproof adhesive tapes are arranged at the sewing positions, and the waterproof adhesive tapes are PU waterproof adhesive tapes. The positions of the PU waterproof adhesive tapes are not shown in the figure because of the large number of sewing positions, and rainwater can be prevented from entering from sewing pinholes by using the waterproof adhesive tapes arranged at the sewing positions.
In order to lighten the overall weight of the aircraft fabric, the aircraft skin 5 is protected, the supporting body 3 comprises a sleeve cover 31 and an inner container 32, the sleeve cover 31 is made of flannelette to form a square or cylindrical structure, the inner container 32 is a sponge inner container, the sleeve cover 31 is filled with sponge to form a sponge inner container, and the supporting body 3 forms a flexible supporting body through the sleeve cover 31 and the inner container 32. The flexible supporting body is adopted, and the sponge has good supporting property, softness and portability, the sponge density is 45, the sponge is not easy to deform and collapse, and scraps are not generated, so that the sponge can play a good supporting role. Meanwhile, the material adopted at the contact position of the support body 3 and the aircraft skin 5 is flannel, the flannel is soft, and the sleeve cover 31 made of the flannel can not damage the coating of the aircraft skin 5, so that a good protective effect is achieved on the coating of the aircraft skin 5.
Example 2
In this embodiment, in order to facilitate sun protection and heat insulation, the outer layer surface of the fabric 1 is further coated with a silver coating layer 4, and the coated silver coating layer 4 is used to reflect sunlight and block ultraviolet rays, and meanwhile, the fabric 1 is supported by a support body, which is also beneficial to ventilation and heat dissipation of the surface of an aircraft.
Example 3
In the embodiment, in order to further enhance the sun-proof and heat-insulating effects, an inner cloth and an outer cloth with the same structure are adopted, sewn into a double-layer integrated structure, the peripheral edges of the inner cloth and the outer cloth are sewn, and a supporting body 3 is fixed on the inner layer surface of the inner cloth in a sewing mode; and a silver coating layer 4 is coated on the outer layer of the outer cloth.
Other aspects of the utility model are not specifically described and are well known to those skilled in the art.
According to the aircraft fabric, in a specific manufacturing process, waterproof fabric can be adopted to manufacture the fabric 1 corresponding to the waterproof fabric according to the appearance structure of the aircraft, meanwhile, a sleeve cover 31 filled with sponge is sewn on the inner layer surface of the fabric 1, meanwhile, strapping 2 with the corresponding length is selected to be sewn on the two side surfaces of the fabric 1, and PU adhesive tapes are added at corresponding sewing positions, so that the manufacturing of the aircraft fabric can be completed. The inner layer surface of the cover cloth 1 is provided with the plurality of supporting bodies 3, and the cover cloth 1 is supported by the supporting bodies 3 which are abutted against the body of the aircraft, so that air can circulate freely, ventilation and heat dissipation of the surface of the aircraft are facilitated, and a protective effect on the coating of the aircraft skin 5 can be achieved; meanwhile, as the PU adhesive tape is added at the sewing position, the cloth is provided with a silver coating layer, has good protection performance and can play a role in water resistance; in addition, the outer layer of the fabric 1 is coated with the silver coating layer 4, and the coated silver coating layer 4 can reflect sunlight and block ultraviolet rays, so that a sun-proof effect can be achieved, important parts of an aircraft are effectively prevented from being damaged due to rain or insolation, and the working temperature of an aircraft system is prevented from being too high. When the mask is used, the mask 1 can be paved on an airplane through the strapping 2, and the mask is light in weight, so that the requirements on the field are not high, and the technical level requirements on operators are low.
Therefore, the aircraft fabric disclosed by the utility model has the waterproof and sun-proof functions, can also play a role in protecting the coating of the aircraft skin 5, is convenient to carry and operate, can be used by personnel of different levels, is particularly suitable for outfield work guarantee, greatly improves the working efficiency, has a simple integral structure, is high in practicability, and is suitable for popularization and application.
The protection scope of the present utility model is not limited to the technical solutions disclosed in the specific embodiments, but the above description is only a preferred embodiment of the present utility model, and is not limited to the present utility model, and any minor modifications, equivalent substitutions and improvements made according to the technical solutions of the present utility model should be included in the protection scope of the technical solutions of the present utility model.
Claims (6)
1. The utility model provides an aircraft fabric with waterproof and sun-proof function, includes fabric (1) and tie (2), its characterized in that: the novel fabric is characterized in that the fabric (1) is provided with an inner layer surface and an outer layer surface, a plurality of supporting bodies (3) are arranged on the inner layer surface of the fabric (1), the fabric (1) is abutted to the body of an airplane through the supporting bodies (3), a plurality of strapping (2) which are symmetrically arranged are arranged on two sides of the fabric (1), and the fabric (1) can be detachably bound to the body of the airplane through the strapping (2).
2. An aircraft fabric with waterproof and sun protection functions according to claim 1, characterized in that: the supporting body (3) comprises a sleeve cover (31) and an inner container (32), wherein the sleeve cover (31) is of a square or cylindrical structure manufactured by flannelette, the inner container (32) is a sponge inner container, the sleeve cover (31) is filled with sponge to form a sponge inner container, and the supporting body (3) forms a flexible supporting body through the sleeve cover (31) and the inner container (32).
3. An aircraft fabric with waterproof and sun protection functions according to claim 2, characterized in that: the cloth cover (1) is waterproof cloth, the supporting body (3) is fixed on the cloth cover (1) in a sewing mode, waterproof adhesive tapes are arranged at the sewing positions, and the waterproof adhesive tapes are PU waterproof adhesive tapes.
4. An aircraft fabric with waterproof and sun protection functions according to claim 3, characterized in that: the outer layer surface of the cloth (1) is also coated with a silver coating layer (4).
5. An aircraft fabric with waterproof and sun protection functions according to claim 3, characterized in that: the inner cloth is characterized in that the inner cloth and the outer cloth are arranged in the same structure, the outer cloth is arranged on the inner cloth, the peripheral edges of the inner cloth and the outer cloth are sewed, the inner cloth and the outer cloth form a double-layer integrated structure, and the support body (3) is fixed on the inner layer surface of the inner cloth in a sewing mode.
6. An aircraft fabric with waterproof and sun protection functions according to claim 5, wherein: the outer layer of the outer cloth is coated with a silver coating layer (4).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322151594.3U CN220721381U (en) | 2023-08-11 | 2023-08-11 | Aircraft fabric with waterproof and sun-proof functions |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322151594.3U CN220721381U (en) | 2023-08-11 | 2023-08-11 | Aircraft fabric with waterproof and sun-proof functions |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220721381U true CN220721381U (en) | 2024-04-05 |
Family
ID=90502873
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202322151594.3U Active CN220721381U (en) | 2023-08-11 | 2023-08-11 | Aircraft fabric with waterproof and sun-proof functions |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220721381U (en) |
-
2023
- 2023-08-11 CN CN202322151594.3U patent/CN220721381U/en active Active
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| Date | Code | Title | Description |
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