IP Library Granted Patent US 10,784,451
Granted Patent B2
US 10,784,451 · App. 15/999,682 · Granted Sep 22, 2020

Flexible laminate having viscoelasticity and flexible display using same

Inventors: Takeaki Tsuda (Tokyo, JP); Michitaka Suto (Odawara, JP); Haruna Mizuno (Chiba, JP); Haruhiko Furukawa (Chiba, JP); Maki Itoh (Ichikawa, JP)
Assignee: DOW TORAY CO., LTD.
H01L51/0097B32B7/022B32B7/12H01L27/3244B32B2457/20
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Quick Facts
Patent No.
US 10,784,451
App. No.
15/999,682
Granted
Sep 22, 2020
Kind
B2
Abstract

A flexible laminate, in which it is possible to achieve both flexibility and durability, is disclosed. A flexible display using the flexible laminate is also disclosed. The flexible laminate includes one or more units of a laminate structure in which two hard layers interposing one or more intermediate layers therebetween are bonded together as one unit. The intermediate layer has viscoelasticity. When the flexible laminate is bent, a neutral plane is formed in each inner portion of the hard layers that are bonded together to interpose the intermediate layer therebetween.

Claims (134)

1. A flexible laminate comprising:

one or more units of a laminate structure in which two hard layers interposing one or more intermediate layers are bonded together as one unit;

wherein:

the intermediate layer has viscoelasticity;

in a case that the flexible laminate is bent, a neutral plane is formed in each inner portion of the hard layers that are bonded together to interpose the intermediate layer therebetween; and

when a Young's modulus EH of a hard layer, a Young's modulus ET of the intermediate layer, a sectional moment of inertia of the hard layer IH, and a sectional moment of inertia of the intermediate layer IH are defined for the one unit of the laminate structure, in a case that the flexible laminate is bent, a value of EH*IH is at least 10 times a value of ET*IT, and a neutral plane is formed in each inner portion of the hard layers that are bonded together to interpose the intermediate layer therebetween without a neutral plane being formed inside the intermediate layer.

2. The flexible laminate according to claim 1 , wherein:

another hard layer is provided with a support mechanism interposing the flexible laminate from a laminate direction such that, in a case that the flexible laminate is bent, the other hard layer shifts, via the intermediate layer, only in a direction substantially parallel to a laminate surface direction with respect to one of the hard layers that are bonded together to interpose the intermediate layer therebetween.

3. The flexible laminate according to claim 2 , wherein:

a step is formed at an end portion of the flexible laminate to correspond to a shift of the other hard layer with respect to one of the hard layers that are bonded together to interpose the intermediate layer therebetween in a case that the flexible laminate is bent.

4. The flexible laminate according to claim 1 , wherein:

in a case that the flexible laminate is bent with a constant radius of curvature to be substantially U-shaped, the intermediate layer is configured to substantially satisfy relationships represented by relational formulas (1) to (3);

a material inherent fracture strain exceeds the maximum shear strain defined by relational formula (5) in a maximum shear strain region when the flexible laminate is bent; and

a material inherent fracture shear stress exceeds a maximum shear stress defined by relational formula (4) in the maximum shear strain region when the flexible laminate is bent:

R 1θ1= R 2θ2  (1)

R 2− R 1= t +( h 1+ h 2)/2  (2)

L =(θ1−θ2)( R 1+ R 2)/2  (3)

τ xy=G*L/t   (4)

γ(=2ε xy )= L/t   (5)

where, in the relational formulas (1) to (5);

R1 is a curvature radius at a center of a thickness direction of one hard layer bonded to the intermediate layer,

R2 is a curvature radius at a center of the thickness direction of the other hard layer bonded to the intermediate layer,

θ1 is a curvature angle at a center of the thickness direction of one hard layer bonded to the intermediate layer,

θ2 is a curvature angle at a center of the thickness direction of the other hard layer bonded to the intermediate layer,

t is a thickness of the intermediate layer,

h1 is a thickness of one hard layer bonded to the intermediate layer,

h2 is a thickness of the other hard layer bonded to the intermediate layer,

L is a shift amount of the other hard layer with respect to one hard layer bonded to the intermediate layer at a curvature end portion of the curvature radius (R1+R2)/2,

τxy is a shear stress of the intermediate layer,

G is an elastic shear modulus of the intermediate layer,

γ (=2εxy) is a shear strain of the intermediate layer, and

εxy is a strain tensor.

5. The flexible laminate according to claim 4 , wherein:

another hard layer is provided with a support mechanism interposing the flexible laminate from a laminate direction such that, in a case that the flexible laminate is bent, the other hard layer shifts, via the intermediate layer, only in a direction substantially parallel to a laminate surface direction with respect to one of the hard layers that are bonded together to interpose the intermediate layer therebetween; and

the shift amount L is substantially identical to a shift amount of the other hard layer with respect to one of the hard layers bonded together to interpose the intermediate layer therebetween at the end portion of the flexible laminate.

6. The flexible laminate according to claim 1 , wherein:

the intermediate layer that configures the flexible laminate is composed from at least one type of adhesive selected from the group consisting of: a silicone-based pressure sensitive adhesive, an acrylic-based pressure sensitive adhesive, and a urethane-based pressure sensitive adhesive.

7. The flexible laminate according to claim 1 , wherein:

the intermediate layer that configures the flexible laminate is composed from at least one type of adhesive; and

a loss factor tans of the adhesive that configures the intermediate layer at a shear frequency of 1 Hz is in a range of 0.2 to 5.0 in a temperature range of −40° C. to 100° C.

8. The flexible laminate according to claim 1 , wherein:

an end portion of the flexible laminate can be bent by 90 degrees or more with respect to one end portion of the flexible laminate.

9. The flexible laminate according to of claim 1 , wherein:

one hard layer of the hard layers bonded together to interpose the intermediate layer therebetween is a light emitting layer for a flexible display, and the other hard layer is one or more types selected from: a support layer, an optical functional layer, a protective layer, and a flexible display transparent electrode layer.

10. A flexible display comprising the flexible laminate according to claim 9 .

11. The flexible laminate according to claim 7 , wherein:

the adhesive that configures the intermediate layer is selected from the group consisting of: a silicone-based pressure sensitive adhesive, an acrylic-based pressure sensitive adhesive, and a urethane-based pressure sensitive adhesive.

12. A flexible laminate comprising:

one or more units of a laminate structure in which two hard layers interposing one or more intermediate layers are bonded together as one unit;

wherein:

the intermediate layer has viscoelasticity;

in a case that the flexible laminate is bent, a neutral plane is formed in each inner portion of the hard layers that are bonded together to interpose the intermediate layer therebetween; and

another hard layer is provided with a support mechanism interposing the flexible laminate from a laminate direction such that, in a case that the flexible laminate is bent, the other hard layer shifts, via the intermediate layer, only in a direction substantially parallel to a laminate surface direction with respect to one of the hard layers that are bonded together to interpose the intermediate layer therebetween.

13. A flexible laminate comprising:

one or more units of a laminate structure in which two hard layers interposing one or more intermediate layers are bonded together as one unit;

wherein:

the intermediate layer has viscoelasticity;

in a case that the flexible laminate is bent, a neutral plane is formed in each inner portion of the hard layers that are bonded together to interpose the intermediate layer therebetween; and

in a case that the flexible laminate is bent with a constant radius of curvature to be substantially U-shaped, the intermediate layer is configured to substantially satisfy relationships represented by relational formulas (1) to (3);

a material inherent fracture strain exceeds the maximum shear strain defined by relational formula (5) in a maximum shear strain region when the flexible laminate is bent; and

a material inherent fracture shear stress exceeds a maximum shear stress defined by relational formula (4) in the maximum shear strain region when the flexible laminate is bent:

R 1θ1 =R 2θ2  (1)

R 2− R 1= t +( h 1+ h 2)/2  (2)

L =(θ1−θ2)( R 1+ R 2)/2  (3)

τ xy=G*L/t   (4)

γ(=2ε xy )= L/t   (5)

where, in the relational formulas (1) to (5);

R1 is a curvature radius at a center of a thickness direction of one hard layer bonded to the intermediate layer,

R2 is a curvature radius at a center of the thickness direction of the other hard layer bonded to the intermediate layer,

θ1 is a curvature angle at a center of the thickness direction of one hard layer bonded to the intermediate layer,

θ2 is a curvature angle at a center of the thickness direction of the other hard layer bonded to the intermediate layer,

t is a thickness of the intermediate layer,

h1 is a thickness of one hard layer bonded to the intermediate layer,

h2 is a thickness of the other hard layer bonded to the intermediate layer,

L is a shift amount of the other hard layer with respect to one hard layer bonded to the intermediate layer at a curvature end portion of the curvature radius (R1+R2)/2,

τxy is a shear stress of the intermediate layer,

G is an elastic shear modulus of the intermediate layer,

γ (=2εxy) is a shear strain of the intermediate layer, and

εxy is a strain tensor.

14. The flexible laminate according to claim 13 , wherein:

another hard layer is provided with a support mechanism interposing the flexible laminate from a laminate direction such that, in a case that the flexible laminate is bent, the other hard layer shifts, via the intermediate layer, only in a direction substantially parallel to a laminate surface direction with respect to one of the hard layers that are bonded together to interpose the intermediate layer therebetween; and

the shift amount L is substantially identical to a shift amount of the other hard layer with respect to one of the hard layers bonded together to interpose the intermediate layer therebetween at the end portion of the flexible laminate.

15. A flexible laminate comprising:

one or more units of a laminate structure in which two hard layers interposing one or more intermediate layers are bonded together as one unit;

wherein:

the intermediate layer has viscoelasticity;

in a case that the flexible laminate is bent, a neutral plane is formed in each inner portion of the hard layers that are bonded together to interpose the intermediate layer therebetween; and

in a case that the flexible laminate is bent with a constant radius of curvature to be substantially U-shaped, the intermediate layer is configured to substantially satisfy relationships represented by relational formulas (1) to (3);

a material inherent fracture strain exceeds the maximum shear strain defined by relational formula (5) in a maximum shear strain region when the flexible laminate is bent; and

a material inherent fracture shear stress exceeds a maximum shear stress defined by relational formula (4) in the maximum shear strain region when the flexible laminate is bent:

R 1θ1 =R 2θ2  (1)

R 2− R 1= t +( h 1+ h 2)/2  (2)

L =(θ1−θ2)( R 1+ R 2)/2  (3)

τ xy=G*L/t   (4)

γ(=2ε xy )= L/t   (5)

where, in the relational formulas (1) to (5);

R1 is a curvature radius at a center of a thickness direction of one hard layer bonded to the intermediate layer,

R2 is a curvature radius at a center of the thickness direction of the other hard layer bonded to the intermediate layer,

θ1 is a curvature angle at a center of the thickness direction of one hard layer bonded to the intermediate layer,

θ2 is a curvature angle at a center of the thickness direction of the other hard layer bonded to the intermediate layer,

t is a thickness of the intermediate layer,

h1 is a thickness of one hard layer bonded to the intermediate layer,

h2 is a thickness of the other hard layer bonded to the intermediate layer,

L is a shift amount of the other hard layer with respect to one hard layer bonded to the intermediate layer at a curvature end portion of the curvature radius (R1+R2)/2,

τxy is a shear stress of the intermediate layer,

G is an elastic shear modulus of the intermediate layer,

γ (=2εxy) is a shear strain of the intermediate layer, and

εxy is a strain tensor; and

wherein the shift amount L is substantially identical to a shift amount of the other hard layer with respect to one of the hard layers bonded together to interpose the intermediate layer therebetween at the end portion of the flexible laminate.

16. A flexible laminate comprising:

one or more units of a laminate structure in which two hard layers interposing one or more intermediate layers are bonded together as one unit;

wherein:

the intermediate layer has viscoelasticity;

in a case that the flexible laminate is bent, a neutral plane is formed in each inner portion of the hard layers that are bonded together to interpose the intermediate layer therebetween; and

the intermediate layer that configures the flexible laminate is composed from at least one type of adhesive selected from the group consisting of: a silicone-based pressure sensitive adhesive, an acrylic-based pressure sensitive adhesive, and a urethane-based pressure sensitive adhesive.

17. A flexible laminate comprising:

one or more units of a laminate structure in which two hard layers interposing one or more intermediate layers are bonded together as one unit;

wherein:

the intermediate layer has viscoelasticity;

in a case that the flexible laminate is bent, a neutral plane is formed in each inner portion of the hard layers that are bonded together to interpose the intermediate layer therebetween; and

the intermediate layer that configures the flexible laminate is composed from at least one type of adhesive; and

a loss factor tans of the adhesive that configures the intermediate layer at a shear frequency of 1 Hz is in a range of 0.2 to 5.0 in a temperature range of −40° C. to 100° C.

18. A flexible laminate comprising:

one or more units of a laminate structure in which two hard layers interposing one or more intermediate layers are bonded together as one unit;

wherein:

the intermediate layer has viscoelasticity;

in a case that the flexible laminate is bent, a neutral plane is formed in each inner portion of the hard layers that are bonded together to interpose the intermediate layer therebetween; and

one hard layer of the hard layers bonded together to interpose the intermediate layer therebetween is a light emitting layer for a flexible display, and the other hard layer is one or more types selected from: a support layer, an optical functional layer, a protective layer, and a flexible display transparent electrode layer.

19. A flexible display comprising a flexible laminate, the flexible laminate comprising:

one or more units of a laminate structure in which two hard layers interposing one or more intermediate layers are bonded together as one unit;

wherein:

the intermediate layer has viscoelasticity;

in a case that the flexible laminate is bent, a neutral plane is formed in each inner portion of the hard layers that are bonded together to interpose the intermediate layer therebetween; and

one hard layer of the hard layers bonded together to interpose the intermediate layer therebetween is a light emitting layer for a flexible display, and the other hard layer is one or more types selected from: a support layer, an optical functional layer, a protective layer, and a flexible display transparent electrode layer.

Assignments (2)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 13, 2020
From: TSUDA, TAKEAKI; SUTO, MICHITAKA; MIZUNO, HARUNA; FURUKAWA, HARUHIKO; ITOH, MAKI
To: DOW CORNING TORAY CO., LTD.
Reel/Frame 053486/0208 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 17, 2019
From: DOW CORNING TORAY CO., LTD.
To: DOW TORAY CO., LTD.
Reel/Frame 051322/0925 →
Priority Claims (1)
JP 2016-028696 · Feb 18, 2016 · national
Continuity (1)
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