A
|
 |
| actual |
difference between the direction of a ply and the delta or
deviation angle. |
C
|
|
| core |
insert enabling to stiffen the part. |
| core sampling |
piercing of the part at one point to get the laminate. |
D
|
|
| deformation |
a producibility analysis mode based on the angle between
the two vectors of the fiber mesh. |
| delta |
angle of deviation computed when performing a producibility
analysis, that is angle between the transferred theoretical rosette and the
actual fiber direction (along the X axis). |
| deviation |
a producibility analysis mode based on the angle between
the x axis of the transferred rosette and the x axis of the fiber mesh. |
| draping direction |
direction whereby the plies are laid on the mold.
With the draping direction shown, material is applied on the upper/concave
side of the surface. If you reverse the draping direction, material will be
applied on the lower/convex side of the surface.
Note that the order of pPlies from top to bottom in the stacking corresponds
to the draping direction arrow from tail/base to head/tip. |
E
|
|
| EEOP |
Engineering Edge Of Part: engineering outer boundary of the
plies. |
| EOP |
Edge Of Part: outer boundary of the plies. |
| ETBS |
Edge To Be Staggered: common edge between two adjacent
zones. |
I
|
|
| IML |
Inner Mold Line: top surface of the Composites part. |
| ITP |
Imposed Thickness Point: connection point between
transition zones, and zones on which the user wants to impose a thickness. |
L
|
|
| laminate |
number of layers per association material / direction for
one zone. |
M
|
|
| MEOP |
Manufacturing Edge Of Part: manufacturing outer boundary of
the plies. |
P
|
|
| ply |
piece of fabric. |
| producibility |
simulation of the fibers behavior to detect
manufacturability problems. |
R
|
|
| rosette |
defines the axis (X, Y, Z) in which the directions are
stored. |
S
|
|
| sequence |
manufacturing notion. Set of plies that the machine puts on
the mold in one path. |
| stack-up file |
file containing the stacking order of the Composites part. |
| staggering |
ply drop-off to avoid ply build-up. |
| strategy point |
point used to start the circular propagation of the fibers
in the producibility tool. |
T
|
|
| transition zone |
zone defining the geometric area of the ply drop-off
between two zones. |
Z
|
|
| zone |
conceptual definition of the Composites part. Geometrical
area in which the laminate is constant. |
