IP Library Granted Patent US 7,208,223
Granted Patent B2
US 7,208,223 · App. 10/699,077 · Granted Apr 24, 2007

Composite sheet material

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Quick Facts
Patent No.
US 7,208,223
App. No.
10/699,077
Granted
Apr 24, 2007
Kind
B2
Abstract

Composite sheet material comprises a core ( 12 ) formed from cellular material having a respective skin of continuous sheet material on each side thereof. Both the core and the skins are formed of thermoplastic materials and the skins are attached to the core by a thermoplastic adhesive having a fusion temperature less than that of both the core and the skins.

Claims (23)

1. A composite sheet material comprising:

a rigid core ( 34 ) of honeycomb cellular material having a first and a second side and an initial thickness; and the rigid core ( 34 ) being formed of a plurality of individually extruded tubes arranged adjacently and in parallel and in a hexagonal pattern to form a honeycomb structure in which each tube has a first end in contact with a first side skin and a second end in contact with a second side skin;

the first skins is formed of continuous sheet material on the first side of the rigid core and the second skin is formed of continuous sheet material on the second side of the rigid core and the first and the second skins each have an initial thickness; and

the first and the second skins ( 32 , 36 ) are formed of a reinforced thermoplastic laminate thermoformable in a temperature range of 150° C. to 300° C.; and

the tubes are formed of polyetherimid material thermoformable in a temperature range up to 170° C.; and

the composite sheet material being formed of the rigid core ( 34 ) and the first and the second skins ( 32 , 36 ) is uniformly compressed while heated to a temperature in a thermoformable range of 150° C. to 170° C. so as to have a uniform thickness less than a sum of the initial thickness of the rigid core ( 34 ), the first side skin ( 32 ) and the second side skin ( 36 );

wherein in each tube, regions of a wall of the tube adjacent the first and second ends of the tube are distorted so as to bridge interstices between the first ends and the second ends of each adjacent ones of the tubes to thereby increase the contact surface area between the tube and the first side and the second side skins and walls.

2. The composite sheet material according to claim 1 , wherein the first and the second skins ( 32 , 36 ) are secured to the rigid core ( 34 ) using a separate polyester base thermoplastic adhesive which has a fusion temperature of less than 150° C.

3. The composite sheet material according to claim 1 , wherein the extruded tubes have circular cross-section.

4. The composite sheet material according to claim 1 , wherein the rigid core ( 12 , 34 ) has a lower fusion temperature than a fusion temperature of the first skin ( 14 , 16 ) and of the second skin ( 32 , 36 ).

5. A composite sheet material comprising:

a rigid core ( 12 , 34 ) of honeycomb cellular material having an initial thickness and being formed by a plurality of individually extruded tubes arranged adjacently and in parallel and in a hexagonal pattern to form a honeycomb; and

a first skin of continuous sheet material on a first side of the rigid core ( 12 , 34 ) and a second skin of continuous sheet material on a second side of the rigid core, and the first skin ( 14 , 32 ) and the second skin ( 16 , 36 ) each have an initial thickness;

wherein each tube has a first end in contact with a first side skin and a second end in contact with a second side skin;

the tubes are formed of polyetherimid material thermoformable in a temperature range up to 170° C.

the first and the second skins ( 14 , 16 ; 32 , 36 ) are formed of a reinforced thermoplastic laminate thermoformable in a temperature range of 150° C. to 300° C.; and the first and the second skins ( 14 , 16 ; 32 , 36 ) are each attached to a corresponding side of the rigid core by a polyester base thermoplastic adhesive having a fusion temperature less than 150° C.; and

the composite sheet material formed of the rigid core, the first and the second skins is uniformly compressed, while heated to a temperature in a thermoformable range of 150° C. to 170° C., so as to have a uniform thickness less than a sum of the initial thicknesses of the rigid core and the first and second skins so that in each tube, regions of a wall of the tube adjacent the first and second ends of the tube are distorted so as to bridge interstices between the first ends and the second ends of each of adjacent ones of the tubes to thereby increase the contact surface area between the tube and the first side and second side skins and walls.

6. A composite sheet material comprising:

a rigid core ( 34 ) of honeycomb cellular material having a first side and a second side and an initial thickness and formed of a plurality of individually extruded tubes arranged adjacently and in parallel and in a hexagonal pattern to form a honeycomb with each tube extending from a first end at the first side to a second end at the second side; and

a first skin of continuous sheet material on the first side and a second skin of continuous sheet material on the second side of side, with the first and the second skins each having an initial thickness;

wherein the tubes are formed of polyetherimid material thermoformable in a temperature range of 150° C. to 170° C.; and

the first and the second skins are formed of a reinforced thermoplastic laminate thermoformable in a temperature range of approximately 170° to 300° C.; and

in each tube, regions of a wall of the tube adjacent the first and second ends of the tube are distorted so as to bridge interstices between the first ends and the second ends of each of adjacent ones of the tubes to thereby increase the contact surface area between the tube and the first side and second side skins and walls, wherein the composite sheet material has a uniform thickness.

Assignments (5)
CHANGE OF NAME Recorded Nov 20, 2020
From: ZODIAC SEATS UK LIMITED
To: SAFRAN SEATS GB LIMITED
Reel/Frame 054427/0469 →
CHANGE OF NAME Recorded Nov 27, 2012
From: CONTOUR AEROSPACE LIMITED
To: ZODIAC SEATS UK LIMITED
Reel/Frame 029355/0619 →
CORRECTIVE ASSIGNMENT TO CORRECT THE ASSIGNEE NAME PREVIOUSLY RECORDED ON REEL 027106 FRAME 0031. ASSIGNOR(S) HEREBY CONFIRMS THE THE ASSIGNEE NAME SHOULD BE CONTOUR AEROSPACE LIMITED. Recorded Nov 7, 2011
From: PREMIUM AIRCRAFT INTERIORS UK LIMITED
To: CONTOUR AEROSPACE LIMITED
Reel/Frame 027183/0309 →
CHANGE OF NAME Recorded Oct 24, 2011
From: PREMIUM AIRCRAFT INTERIORS UK LIMITED
To: COUNTOR AEROSPACE LIMITED
Reel/Frame 027106/0031 →
CHANGE OF NAME Recorded Mar 14, 2007
From: BRITAX AIRCRAFT INTERIORS UK LIMITED
To: PREMIUM AIRCRAFT INTERIORS UK LIMITED
Reel/Frame 019007/0859 →