forces
bearing on them and how the internal forces are distributed within them.
That is, |
they
exhibit plate action as opposed to the lattice action we just covered.
The equation |
describing the stability of pure plate structures is: |
. |
E = 3 F - 6
where E = edges |
F = faces |
. |
Notice
that, in terms of plate action, this equation asserts that the cube plate
structure just |
pictured
in Fig. 203 is stable. But the cube lattice structure is not
stable. Why is this so? |
. |
Pure
plate structures are entirely composed of rigid plates that are joined
together edge to |
edge
with flexible hinge joints. These edges are called shear lines
because the internal |
stresses
generated by an external load are distributed over the surface area of
the plates, |
which are
then concentrated as shear forces along the entire length of the edges
where the |
|
plates are joined. This shear force consists of a pair of
equal, |
|
parallel forces acting in opposite directions with no distance |
between them, as shown in the animation to the left. Note |
how pressing on the opposite vertices of the cube plate |
structure causes the plates to shear past each other when |
there is no hinge pin, or pinge, to resist this stress.
Normally |
the pinges of the structure resist this shearing when they are |
positioned between the plates. The pinges, plus the rigidity
|
(demonstration model) |
of
the plates enables the structure to achieve a state of stable |
Fig. 204 - Plates of a cube |
equilibrium so that it resists shear failure when loaded. Due |
shearing past each other |
to
the hinge able nature of this joint the plates do not
|
|
experience bending moments when the structure is loaded at |
|
its
vertices. Therefore pure plate structures are statically
determinate, although the static |
analysis
techniques are considerably more complex than those for trusses, or even
lattices. |
. |
The
following images show building sections that are modeled as plate
structures. Each is |
|
|
 |
|
a) 9 = 3 ( 5 ) - 6 |
*b) 9 = 3 ( 5 ) - 6 |
*c) 12 = 3 ( 6 ) - 6 |
d) 8 < 3 ( 5 ) - 6 |
stable |
stable |
stable |
unstable |
click image to enlarge |
Fig. 205 - Plate stability analysis of structures
(static demonstration models) |
|
* Note:
for modeling purposes, all panels lying in the same plane are counted as
one plate |
. |
analyzed
for its stability as a pure plate structure using E = 3 F - 6. Note
that most of the |
models
are stable except d), a square pyramid peaked roof. It is
undoubtedly rigid since |
. |
Back
to Knowhere |
 |
Page 121
- Building stability - Plate action |
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