SHEET MATERIAL FOR AIRCRAFT INTERIOR EQUIPMENT AND MANUFACTURING METHOD THEREFOR
20170165951 ยท 2017-06-15
Assignee
Inventors
Cpc classification
B32B2307/3065
PERFORMING OPERATIONS; TRANSPORTING
B32B37/04
PERFORMING OPERATIONS; TRANSPORTING
B29C66/71
PERFORMING OPERATIONS; TRANSPORTING
B32B37/10
PERFORMING OPERATIONS; TRANSPORTING
B64D2045/009
PERFORMING OPERATIONS; TRANSPORTING
B29C65/02
PERFORMING OPERATIONS; TRANSPORTING
B32B27/12
PERFORMING OPERATIONS; TRANSPORTING
B32B27/06
PERFORMING OPERATIONS; TRANSPORTING
B32B37/203
PERFORMING OPERATIONS; TRANSPORTING
B29K2995/0016
PERFORMING OPERATIONS; TRANSPORTING
B32B5/02
PERFORMING OPERATIONS; TRANSPORTING
B32B37/02
PERFORMING OPERATIONS; TRANSPORTING
B29K2675/00
PERFORMING OPERATIONS; TRANSPORTING
B29C66/45
PERFORMING OPERATIONS; TRANSPORTING
B64D11/0647
PERFORMING OPERATIONS; TRANSPORTING
International classification
B64D11/06
PERFORMING OPERATIONS; TRANSPORTING
B29C65/00
PERFORMING OPERATIONS; TRANSPORTING
B32B37/04
PERFORMING OPERATIONS; TRANSPORTING
B32B37/02
PERFORMING OPERATIONS; TRANSPORTING
B32B37/10
PERFORMING OPERATIONS; TRANSPORTING
B32B27/06
PERFORMING OPERATIONS; TRANSPORTING
B29C65/02
PERFORMING OPERATIONS; TRANSPORTING
B32B37/20
PERFORMING OPERATIONS; TRANSPORTING
B32B5/02
PERFORMING OPERATIONS; TRANSPORTING
Abstract
A sheet material (30) is constituted by an FBL to which one surface (36a) of a fire-retardant urethane material (36) is melted and fused and an outer cover (34) to which the other surface (36b) of the fire-retardant urethane material (36) is melted and fused.
Claims
1. A sheet material for aircraft interior equipment, comprising: a fire-retardant urethane material; an FBL (Fire Blocking Layer: fire-resistant cloth) fused to one of surfaces of the fire-retardant urethane material via a melting layer; and an outer cover (skin material) fused to the other surface of the fire-retardant urethane material via a melting layer.
2. The sheet material for aircraft interior equipment according to claim 1, wherein a thickness of the melting layer of the fire-retardant urethane material to be fused to the FBL is approximately 1.5 mm; a thickness of the melting layer of the fire-retardant urethane material to be fused to the outer cover is approximately 1.5 mm; and a thickness of the remaining fire-retardant urethane material is approximately 1.5 mm.
3. A manufacturing method of a sheet material for aircraft interior equipment, comprising the steps of: preparing a roll of a fire-retardant urethane material and a roll of an FBL; heating and melting the surface of the fire-retardant urethane material facing the FBL roll; compressively bonding the melted surface of the fire-retardant urethane material and a surface of the FBL roll to produce a fire-retardant urethane FBL roll; preparing a fused fire-retardant urethane FBL roll and an outer cover roll; heating and melting a surface of the fire-retardant urethane material of the fire-retardant urethane FBL roll facing the outer cover roll; and compressively bonding the melted surface of the fire-retardant urethane material and a back surface of the outer cover.
4. The manufacturing method of a sheet material for aircraft interior equipment according to claim 3, wherein a temperature for heating the surface of the fire-retardant urethane material is 800 to 900 C.; and the heating time is 0.5 to 1.5 seconds.
Description
BRIEF DESCRIPTION OF DRAWINGS
[0018]
[0019]
[0020]
[0021]
[0022]
[0023]
[0024]
[0025]
[0026]
DESCRIPTION OF EMBODIMENTS
[0027]
[0028]
[0029]
[0030]
[0031] The sheet material 30 of the present invention has a sectional structure in which an FBL (fire-resistant cloth) 32 and an outer cover (skin material) 34 are laminated on each of both surfaces of a fire-retardant urethane material 36.
[0032]
[0033] In
[0034] Flame at approximately 800 to 900 C. is applied by the burner 200 to the heated surface 100a for about 0.5 to 1.0 seconds so as to melt the surface.
[0035] The fire-retardant urethane FBL roll 120 is wound into a roll shape in a state in which the fire-retardant urethane roll 100 is on a front side and the FBL roll 110 is on a back side.
[0036] Subsequently, as illustrated in
[0037] Regarding the material pulled out of the fire-retardant urethane FBL roll 120, flame of approximately 800 to 900 C. is applied by the burner 200 to a heated surface 100b of the fire-retardant urethane roll 100 for 0.5 to 1.0 seconds so as to melt the same, and the material is passed together with the outer cover 130 between the pressing roll 210 and the base 220 and compressively fused.
[0038] A completed sheet material 150 is manufactured having a lengthy band shape with a surface 130a of the outer cover 130 and the FBL roll 110 as both surfaces.
[0039] This is cut out to an appropriate dimension and used as the sheet material 30 illustrated in
[0040] The fire-retardant urethane 36 has a thickness T.sub.2 in an initial stage. A melting layer 36a is melt into the FBL having a thickness T.sub.1 and the fire-retardant urethane 36 and the FBL are fused. A melted dimension T.sub.2a is approximately 1.5 mm.
[0041] Moreover, the outer cover 34 has a thickness T.sub.3, and a melting layer 36b of the fire-retardant urethane material 36 is melted into the outer cover 34.
[0042] A melted dimension T.sub.2b, is approximately 1.5 mm.
[0043] As a result, a thickness T.sub.2c of the remaining fire-retardant urethane is approximately 1.5 mm.
[0044]
[0045] As described above, the present invention can obtain a sheet material for aircraft interior equipment, which can maintain good appearance of the outer cover surface and has high durability.
REFERENCE SIGNS LIST
[0046] 1 Seat in an aircraft [0047] 10 Upper inner pad [0048] 20 Lower inner pad [0049] 30 Sheet material [0050] 32 FBL (fire-resistant cloth) [0051] 34 Outer cover [0052] 36 Fire-retardant urethane material [0053] 100 Fire-retardant urethane roll [0054] 110 FBL roll [0055] 120 Fire-retardant urethane FBL roll [0056] 130 Outer cover roll [0057] 200 Burner [0058] 210 Pressing roll [0059] 220 Base