CN214266826U

CN214266826U - Plane material of aviation seat

Info

Publication number: CN214266826U
Application number: CN202022328289.3U
Authority: CN
Inventors: 邱炳梁; 李天发; 张博海
Original assignee: Dongguan Baoliang Material Technology Co ltd
Current assignee: Dongguan Baoliang Material Technology Co ltd
Priority date: 2020-10-19
Filing date: 2020-10-19
Publication date: 2021-09-24
Anticipated expiration: 2030-10-19

Abstract

The utility model discloses an aviation seat plane materiel, including seat plane materiel main part, the upper end of seat plane materiel main part is provided with fire-retardant antifouling mechanism, the lower extreme surface of fire-retardant antifouling mechanism is provided with first resin glue membrane, the lower extreme surface of first resin glue membrane is provided with ventilative resilience mechanism, ventilative resilience mechanism's lower extreme surface is provided with second resin glue membrane, the lower extreme surface of second resin glue membrane is provided with degradation resistance to compression mechanism. An aviation seat plane materiel, through fire-retardant antifouling mechanism for the seat plane materiel has better fire-retardant antifouling performance, and the inside anti-cutting cloth that sets up of fire-retardant antifouling mechanism, make this product can prevent sharp-pointed object's damage, and through being provided with ventilative resilience mechanism, travelling comfort when making the seat plane materiel use improve, and, through the degradation resistance to compression mechanism that sets up, improved the feature of environmental protection and the life of seat plane materiel, bring better use prospect.

Description

Plane material of aviation seat

Technical Field

The utility model relates to an aviation seat field specifically is an aviation seat plane materiel.

Background

The airline seat is a key device for the comfort of passengers traveling in flight and is one of the most important airborne devices in civil aircraft projects.

Current aviation seat is when the installation is used, for passenger's travelling comfort, can fill a large amount of sponges or soft filler in its lower part, just so lead to the gas permeability of cushion poor, and sponge or soft filler are easily burnt, the security is low, and can rub oil stain when using, the inside difficult clearance of infiltration surface fabric, influence the aesthetic property of seat, after seat uses a period of time simultaneously, because of the deformation that inside filler was pressed, make the travelling comfort of seat reduce, the life of seat has been shortened, certain adverse effect has been brought to people's use, for this, we propose an aviation seat plane materiel.

SUMMERY OF THE UTILITY MODEL

Technical problem to be solved

Not enough to prior art, the utility model provides an aviation seat plane materiel possesses advantages such as antifouling, fire-retardant, ventilative, memory resilience, environmental protection, can effectively solve the problem in the background art.

(II) technical scheme

In order to achieve the above purpose, the utility model adopts the following technical scheme: the utility model provides an aviation seat plane materiel, includes seat plane materiel main part, the upper end of seat plane materiel main part is provided with fire-retardant antifouling mechanism, the lower extreme surface of fire-retardant antifouling mechanism is provided with first resin adhesive film, the lower extreme surface of first resin adhesive film is provided with ventilative resilience mechanism, the lower extreme surface of ventilative resilience mechanism is provided with second resin adhesive film, the lower extreme surface of second resin adhesive film is provided with degradation resistance to compression mechanism.

Preferably, the outer surface of the lower end of the flame-retardant and antifouling mechanism is connected with the outer surface of the upper end of the breathable resilience mechanism in an undetachable manner through a first resin adhesive film, the outer surface of the lower end of the breathable resilience mechanism is connected with the outer surface of the upper end of the degradation and compression-resistant mechanism in an undetachable manner through a second resin adhesive film, the thickness of the flame-retardant and antifouling mechanism is 1-1.5cm, the thickness of the first resin adhesive film is 0.2-0.4cm, the thickness of the breathable resilience mechanism is 0.8-1cm, and the thickness of the degradation and compression-resistant mechanism is 0.8-1 cm.

Preferably, fire-retardant antifouling mechanism includes anti-skidding bump, antifouling layer, first UV glue film, anti-cutting cloth, second UV glue film and fire-retardant layer, anti-skidding bump all is located antifouling layer's upper end surface, and anti-skidding bump has a plurality of groups, antifouling layer's lower extreme surface is provided with first UV glue film, the lower extreme surface of first UV glue film is provided with anti-cutting cloth, anti-cutting cloth's lower extreme surface is provided with second UV glue film, the lower extreme surface of second UV glue film is provided with fire-retardant layer.

Preferably, the outer surface of the lower end of the anti-skid salient points is undetachably connected with the outer surface of the upper end of the anti-fouling layer through an adhesive, the anti-skid salient points are hemispherical, the diameter of each anti-skid salient point is 1.9-2.1cm, the outer surface of the lower end of the anti-fouling layer is undetachably connected with the anti-cutting cloth through a first UV adhesive layer, the thickness of the anti-fouling layer is 0.2-0.3cm, the thickness of the anti-cutting cloth is 0.3-0.4cm, the outer surface of the lower end of the anti-cutting cloth is undetachably connected with the outer surface of the upper end of the flame-retardant layer through a second UV adhesive layer, the thicknesses of the first UV adhesive layer and the second UV adhesive layer are both 0.15-0.25cm, and the thickness of the flame-retardant layer is 0.2-0.3 cm.

Preferably, ventilative resilience mechanism includes ventilative layer, third UV glue film and resilience layer, the lower extreme surface on ventilative layer is provided with the third UV glue film, the lower extreme surface on third UV glue film is provided with resilience layer.

Preferably, the outer surface of the lower end of the breathable layer is connected with the outer surface of the upper end of the rebound layer in an undetachable manner through a third UV adhesive layer, the thickness of the breathable layer is 0.3-0.35cm, honeycomb-shaped air holes are formed in the breathable layer, the diameter of each air hole is 0.5-1.0cm, the thickness of the third UV adhesive layer is 0.15-0.25cm, the thickness of the rebound layer is 0.35-0.4cm, a plurality of spherical hollows are formed in the rebound layer, and the diameter of each spherical hollow is 0.8-1.2 cm.

Preferably, degradation resistance to compression mechanism is including degradation layer, fourth UV glue film and compressive layer, the lower extreme surface on degradation layer is provided with the fourth UV glue film, and the lower extreme surface on fourth UV glue film is provided with the compressive layer.

Preferably, the outer surface of the lower end of the degradation layer is connected with the outer surface of the upper end of the pressure-resistant layer in an undetachable manner through a fourth UV adhesive layer, the thickness of the degradation layer is 0.35-0.4cm, the thickness of the fourth UV adhesive layer is 0.15-0.25cm, and the thickness of the pressure-resistant layer is 0.3-0.35 cm.

(III) advantageous effects

Compared with the prior art, the utility model provides an aviation seat plane materiel possesses following beneficial effect:

1. this aircraft seat plane materiel, through the fire-retardant antifouling mechanism who sets up, the material on fire-retardant layer is fibrous polymer, decompose and absorb the heat when polymer and fire contact burning, this has just reduced and has taken place the required heat of schizolysis by burning thing, just also prevent to continue the burning, lower floor's anti-cutting cloth is package steel silk yarn material, and cross distribution, sharp-pointed article hardly punctures, antifouling layer is nanofiber, nanofiber gap size is less than the molecular size of most of pollutants far away, can effectually prevent the infiltration of pollutant, play antifouling effect.

2. This aviation seat plane materiel, through the ventilative heat dissipation mechanism that sets up, the material on ventilative layer is polymer PTFE, has fine ventilation effect, and the material on resilience layer is the memory cotton, and when human contact material, the material will respond to human body temperature, and the softness that gradually changes gets up, has absorbed human pressure again simultaneously to adjust the most comfortable posture state with the human body, improve the travelling comfort when using.

3. This aviation seat plane materiel, through the degradation resistance to compression mechanism that sets up, the material on degradation layer is the lactic acid material, changes the back of eliminating at the surface fabric, buries it in the soil in unison, after a period, can be absorbed the degradation by microorganism in the soil, plays the effect of environmental protection, and resistance to compression layer has strengthened the bearing nature of seat surface fabric, protects its upper portion surface course can not be sat by the higher passenger of weight bad, improves the practicality and the life of seat.

Drawings

Fig. 1 is the utility model relates to an overall structure schematic diagram of aircraft seat plane materiel.

Figure 2 is the utility model discloses an overall structure cross-sectional view of aircraft seat plane materiel.

Fig. 3 is the utility model relates to a structural schematic diagram of fire-retardant antifouling mechanism in aircraft seat plane materiel.

Fig. 4 is the structural schematic diagram of the ventilation and heat dissipation mechanism in the surface material of the aircraft seat of the present invention.

Figure 5 is the utility model relates to a degradation resistance to compression mechanism's among aircraft seat plane materiel structural schematic diagram.

In the figure: 1. a seat facestock body; 2. a flame-retardant antifouling mechanism; 3. a first resin film; 4. a breathable rebound mechanism; 5. a second resin film; 6. a degradation compression-resistant mechanism; 201. anti-skid bumps; 202. an antifouling layer; 203. a first UV glue layer; 204. cutting-resistant cloth; 205. a second UV glue layer; 206. a flame retardant layer; 401. a breathable layer; 402. a third UV adhesive layer; 403. a resilient layer; 601. a degradation layer; 602. a fourth UV adhesive layer; 603. and a pressure resistant layer.

Detailed Description

In order to make the technical means, creation features, achievement purposes and functions of the present invention easy to understand, the present invention is further described below with reference to the following embodiments.

As shown in fig. 1-5, an aviation seat surface material comprises a seat surface material main body 1, wherein a flame-retardant antifouling mechanism 2 is arranged at the upper end of the seat surface material main body 1, a first resin adhesive film 3 is arranged on the outer surface of the lower end of the flame-retardant antifouling mechanism 2, a breathable rebound mechanism 4 is arranged on the outer surface of the lower end of the first resin adhesive film 3, a second resin adhesive film 5 is arranged on the outer surface of the lower end of the breathable rebound mechanism 4, and a degradation compression-resistant mechanism 6 is arranged on the outer surface of the lower end of the second resin adhesive film 5.

Furthermore, the outer surface of the lower end of the flame-retardant and antifouling mechanism 2 is undetachably connected with the outer surface of the upper end of the breathable resilience mechanism 4 through the first resin adhesive film 3, the outer surface of the lower end of the breathable resilience mechanism 4 is undetachably connected with the outer surface of the upper end of the degradation and compression resistant mechanism 6 through the second resin adhesive film 5, the thickness of the flame-retardant and antifouling mechanism 2 is 1-1.5cm, the first resin adhesive film 3 and the second resin adhesive film 5 are both made of epoxy resin materials and are 0.2-0.4cm, the thickness of the breathable resilience mechanism 4 is 0.8-1cm, the thickness of the degradation and compression resistant mechanism 6 is 0.8-1cm, and the connection stability between the mechanisms is improved.

Further, fire-retardant antifouling mechanism 2 includes anti-skidding bump 201, antifouling layer 202, first UV glue film 203, anti-cutting cloth 204, second UV glue film 205 and fire-retardant layer 206, anti-skidding bump 201 all is located antifouling layer 202's upper end surface, and anti-skidding bump 201 has a plurality of groups, antifouling layer 202's lower extreme surface is provided with first UV glue film 203, first UV glue film 203's lower extreme surface is provided with anti-cutting cloth 204, anti-cutting cloth 204's lower extreme surface is provided with second UV glue film 205, second UV glue film 205's lower extreme surface is provided with fire-retardant layer 206, the life of surface fabric is improved.

Furthermore, the outer surface of the lower end of the anti-slip salient point 201 is undetachably connected with the outer surface of the upper end of the anti-fouling layer 202 through an adhesive, the anti-slip salient point 201 is hemispherical, the diameter of the anti-slip salient point is 1.9-2.1cm, the outer surface of the lower end of the anti-fouling layer 202 is undetachably connected with the anti-cutting cloth 204 through a first UV adhesive layer 203, the anti-cutting cloth 202 is made of nano fibers, the thickness of the anti-cutting cloth is 0.2-0.3cm, the anti-cutting cloth 204 is made of steel wire wrapping yarns and is distributed in a crossed mode, the thickness of the anti-cutting cloth is 0.3-0.4cm, the outer surface of the lower end of the anti-cutting cloth 204 is undetachably connected with the outer surface of the upper end of the flame-retardant layer 206 through a second UV adhesive layer 205, the first UV adhesive layer 203 and the second UV adhesive layer 205 are made of acrylic ester materials, the thickness of 0.15-0.25cm, the flame-retardant layer 206 is made of fiber polymer, the thickness of 0.2-0.3cm, and the inside of the anti-slip salient point is protected from being damaged by foreign objects.

Further, ventilative resilience mechanism 4 is including ventilative layer 401, third UV glue film 402 and resilience layer 403, and the lower extreme surface of ventilative layer 401 is provided with third UV glue film 402, and the lower extreme surface of third UV glue film 402 is provided with resilience layer 403, improves the comfort when using.

Furthermore, the outer surface of the lower end of the breathable layer 401 is connected with the outer surface of the upper end of the resilient layer 403 through a third UV adhesive layer 402 in a non-detachable mode, the breathable layer 401 is made of high polymer PTFE and is 0.3-0.35cm in thickness, cellular air holes are formed in the breathable layer, the diameter of each air hole is 0.5-1.0cm, the third UV adhesive layer 402 is made of acrylate and is 0.15-0.25cm in thickness, the resilient layer 403 is made of memory cotton and is 0.35-0.4cm in thickness, a plurality of spherical hollows are formed in the resilient layer 403, and the diameter of each spherical hollow is 0.8-1.2cm to improve the air permeability of the fabric.

Further, degradation resistance to compression mechanism 6 includes degradation layer 601, fourth UV glue film 602 and resistance to compression layer 603, and the lower extreme surface of degradation layer 601 is provided with fourth UV glue film 602, and the lower extreme surface of fourth UV glue film 602 is provided with resistance to compression layer 603, strengthens the feature of environmental protection of surface fabric.

Furthermore, the outer surface of the lower end of the degradation layer 601 is connected with the outer surface of the upper end of the compression-resistant layer 603 in a non-detachable mode through a fourth UV adhesive layer 602, the degradation layer 601 is made of lactic acid and is 0.35-0.4cm thick, the fourth UV adhesive layer 602 is made of acrylate and is 0.15-0.25cm thick, the compression-resistant layer 603 is made of nylon cotton and is 0.3-0.35cm thick, and the compression resistance of the fabric is improved.

Principle of operation

The utility model discloses a by seat plane materiel main part 1, fire-retardant antifouling mechanism 2, first resin glue film 3, ventilative heat dissipation mechanism 4, second resin glue film 5, degradation resistance to compression mechanism 6, anti-skidding bump 201, antifouling layer 202, first UV glue film 203, anti-cutting cloth 204, second UV glue film 205, fire-retardant layer 206, ventilative layer 401, third UV glue film 402, resilience layer 403, degradation layer 601, fourth UV glue film 602 and parts such as resistance to compression layer 603, fire-retardant layer's material is fibrous polymer, decompose and absorb heat when polymer and the burning of fire contact, this has just reduced the required heat of quilt thing schizolysis, just prevent to continue burning, lower floor anti-cutting cloth is steel cord yarn material, and cross distribution, sharp-pointed object is difficult to puncture, antifouling layer is nanofiber, nanofiber gap size is far less than the molecular size of most pollutants, can effectively prevent the infiltration of pollutants, play antifouling effect, the material on ventilative layer is polymer PTFE, has fine ventilation effect, and the material on resilience layer is the memory cotton, when human contact material, the material will respond to the human body temperature, the softness that gradually changes gets up, human pressure has been absorbed again simultaneously, thereby adjust the most comfortable posture state with the human body, travelling comfort when improving the use, the material on degradation layer is the lactic acid material, after the surface fabric is changed and is eliminated, bury it in the soil in unison, after a period of time, can be absorbed the degradation by the interior microorganism of soil, play the effect of environmental protection, resistance to compression layer has strengthened the bearing nature of seat surface fabric, it can not be sat badly by the higher passenger of weight to protect its upper portion surface course, improve the practicality and the life of seat.

It is noted that, herein, relational terms such as first and second (a, b, etc.) and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are 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. Without further limitation, an element defined by the phrase "comprising an … …" does not exclude the presence of other identical elements in a process, method, article, or apparatus that comprises the element.

The basic principles and the main features of the invention and the advantages of the invention have been shown and described above. It will be understood by those skilled in the art that the present invention is not limited to the above embodiments, and that the foregoing embodiments and descriptions are provided only to illustrate the principles of the present invention without departing from the spirit and scope of the present invention. The scope of the invention is defined by the appended claims and equivalents thereof.

Claims

1. An aircraft seat facestock, comprising a seat facestock body (1), characterized in that: the upper end of seat plane materiel main part (1) is provided with fire-retardant antifouling mechanism (2), the lower extreme surface of fire-retardant antifouling mechanism (2) is provided with first resin glued membrane (3), the lower extreme surface of first resin glued membrane (3) is provided with ventilative resilience mechanism (4), the lower extreme surface of ventilative resilience mechanism (4) is provided with second resin glued membrane (5), the lower extreme surface of second resin glued membrane (5) is provided with degradation resistance to compression mechanism (6).

2. An aircraft seat facestock according to claim 1, wherein: the lower extreme surface of fire-retardant antifouling mechanism (2) is connected for undetachable through first resin glued membrane (3) and the upper end surface of ventilative resilience mechanism (4), the lower extreme surface of ventilative resilience mechanism (4) is connected for undetachable through the upper end surface of second resin glued membrane (5) and degradation resistance to compression mechanism (6), the thickness of fire-retardant antifouling mechanism (2) is 1-1.5cm, the thickness of first resin glued membrane (3) and second resin glued membrane (5) is 0.2-0.4cm, the thickness of ventilative resilience mechanism (4) is 0.8-1cm, the thickness of degradation resistance to compression mechanism (6) is 0.8-1 cm.

3. An aircraft seat facestock according to claim 1, wherein: flame-retardant antifouling mechanism (2) are including anti-skidding bump (201), antifouling layer (202), first UV glue film (203), anti-cutting cloth (204), second UV glue film (205) and fire-retardant layer (206), anti-skidding bump (201) all are located the upper end surface of antifouling layer (202), and anti-skidding bump (201) have a plurality of groups, the lower extreme surface of antifouling layer (202) is provided with first UV glue film (203), the lower extreme surface of first UV glue film (203) is provided with anti-cutting cloth (204), the lower extreme surface of anti-cutting cloth (204) is provided with second UV glue film (205), the lower extreme surface of second UV glue film (205) is provided with fire-retardant layer (206).

4. An aircraft seat facestock according to claim 3, wherein: the outer surface of the lower end of each anti-skidding salient point (201) is in non-detachable connection with the outer surface of the upper end of the anti-fouling layer (202) through an adhesive, the anti-skidding salient points (201) are hemispherical, the diameter of each anti-skidding salient point (201) is 1.9-2.1cm, the outer surface of the lower end of the anti-fouling layer (202) is in non-detachable connection with the anti-cutting cloth (204) through a first UV adhesive layer (203), the thickness of the anti-cutting cloth (204) is 0.2-0.3cm, the outer surface of the lower end of the anti-cutting cloth (204) is in non-detachable connection with the outer surface of the upper end of the flame-retardant layer (206) through a second UV adhesive layer (205), the thicknesses of the first UV adhesive layer (203) and the second UV adhesive layer (205) are both 0.15-0.25cm, and the thickness of the flame-retardant layer (206) is 0.2-0.3 cm.

5. An aircraft seat facestock according to claim 1, wherein: ventilative resilience mechanism (4) are including ventilative layer (401), third UV glue film (402) and resilience layer (403), the lower extreme surface of ventilative layer (401) is provided with third UV glue film (402), the lower extreme surface of third UV glue film (402) is provided with resilience layer (403).

6. An aircraft seat facestock according to claim 5, wherein: the outer surface of the lower end of the air permeable layer (401) is connected with the outer surface of the upper end of the rebound layer (403) in an undetachable mode through a third UV adhesive layer (402), the thickness of the air permeable layer (401) is 0.3-0.35cm, honeycomb-shaped air vents are formed in the air permeable layer, the diameters of the air vents are 0.5-1.0cm, the thickness of the third UV adhesive layer (402) is 0.15-0.25cm, the thickness of the rebound layer (403) is 0.35-0.4cm, a plurality of spherical hollows are formed in the rebound layer (403), and the diameter of the spherical hollows is 0.8-1.2 cm.

7. An aircraft seat facestock according to claim 1, wherein: degradation resistance to compression mechanism (6) are including degradation layer (601), fourth UV glue film (602) and resistance to compression layer (603), the lower extreme surface of degradation layer (601) is provided with fourth UV glue film (602), and the lower extreme surface of fourth UV glue film (602) is provided with resistance to compression layer (603).

8. An aircraft seat facestock according to claim 7, wherein: the outer surface of the lower end of the degradation layer (601) is connected with the outer surface of the upper end of the compression-resistant layer (603) through a fourth UV adhesive layer (602) in an undetachable mode, the thickness of the degradation layer (601) is 0.35-0.4cm, the thickness of the fourth UV adhesive layer (602) is 0.15-0.25cm, and the thickness of the compression-resistant layer (603) is 0.3-0.35 cm.