Layered sandwich structure
View Patent ↗This homogenized, multilayer sandwich structure has a total bending stiffness. The structure has two external skins each of a material having a modulus, a thickness and a width with contribution to the total moment of inertia. The structure also has a core of a foam material sandwiched between the two external skins, wherein the core has a modulus, a thickness and a width with contribution to the total moment of inertia. The external skins are fixed to the core, the strength of the structure being dependent on the core thickness via cubic power, as well as on the placement of the layers within the structure.
1. A process for calculating the total bending stiffness (S T ) of a non-homogenous multilayer sandwich structure comprising the steps of:
providing non-homogenous a multilayer structure wherein each layer has a modulus (E 1 ), each layer has a moment of inertial (I i ), each layer has a thickness, each layer has a location in the structure, each layer has a width;
calculating a neutral axis location in the non-homogenous, multilayer structure;
depicting a layer E 1 as a reference layer;
achieving layer homogenization by changing the width of a layer by a multiplier n i calculated as a ratio of that layer's modulus to the modulus of the reference layer;
wherein the layer homogenization is represented by the formula:
calculating the total stiffness of the multilayer structure (S T ),
S
T
=
∑
i
=
1
n
S
i
=
∑
i
=
1
n
E
i
·
I
i
=
E
1
∑
i
=
1
n
E
i
E
1
I
i
=
E
1
∑
i
=
1
n
n
i
I
i
Eq
.
(
1
)
Where:
n
i
=
E
i
E
1
is the ratio of the modulus of the i th layer to the reference (i=1) layer.
2. A process according to claim 1 wherein:
I
i
=
Wn
i
h
i
3
12
+
Wn
i
h
i
(
r
i
-
R
)
2
Eq
.
(
2
)
Where:
R
=
∑
i
=
1
n
n
i
h
i
r
i
∑
i
=
1
n
n
i
h
i
is a neutral axis of a composite layer
And:
r
i
=
∑
i
=
1
i
-
1
h
i
+
1
2
h
i
is a distance from the reference layer to the mid-plane position of the i th layer
And W is the composite width and h i is the thickness of the i th layer.