Week 8 - Challenge 5 - Door Trim Lower
DOOR TRIM
OBJECTIVE:
To create the Door Trim Lower's Plastic Component using the Class A Surface that is provided. Desired Thickness of the Plastic Component is 2.5mm with 3.2 degrees as the Draft Angle.
First, we have to create the required Tooling-Axis for the given Class A Surface while meeting the requirements of the necessary Draft Angle & then perform the Draft-Analysis Operation on the Class A Surface itself.
After that, we have to create the required Class B & Class C Surfaces using which we have to make the Final Plastic Component and perform Draft Analysis on it as well.
INTRODUCTION:
CLASS A SURFACE:
Types of Surfaces and their importance for an Automotive Plastic Designer:
- Class A Surface: Class A is an aesthetic surface with the highest quality finish. Most Class A Surfaces for an Automotive Component are made using 'Autodesk-Alias' based on the final Concept-Sketch. All Class A surfaces should have 'Curvature-Continuity', meaning the continuity between the surfaces should share the same boundary. It is taken as a reference by the Automotive Plastic Designer to create 'Class B' and 'Class C' Surfaces.
- Class B Surface: The Class B Surface resides below the Class A Surface at a certain thickness. It is created using Engineering Principles that consist of all the necessary features such as Ribs, Bosses, Snaps, etc. This surface isn't visible to the observer from the outside.
- Class C Surface: The Class C Surface is the surface created between the Class A and Class B surfaces to join them.
Now, we will begin by checking the State of Connectivity for the Class A Surface and ensure that there are no gaps between the surfaces as all the surfaces should be joined well together with each other and shouldn't consist of any discontinuities between them.
By using the 'Boundary' Command' from the Operations Toolbar:
In this case, we have to click on the 'Boundary' command and then select the Class-A Surface. After that, we'll click on the 'Preview' button to highlight all the boundaries that are on the Class-A surface and check if there are any internal boundaries other than the outer edge boundaries.
In our case, there are two boundaries present on the Class-A Surface one of which is the Outer-Edge Boundary & the other is the Inner Hole-Boundary. Hence, we can conclude that all the surfaces are well connected.

TOOLING DIRECTION:
The Tooling Direction is the direction that the mold pulls apart. The mold is built in two separate pieces,
- A Cavity side and
- The Core side.
The Core pulls apart from the Cavity and that's the Dyeline or the Tooling Direction. The direction in which the mold or core and cavity open is the tooling axis.
FEATURES OF THE TOOL:
DRAFT ANALYSIS FOR THE CLASS A SURFACE USING THE MAIN TOOLING AXIS:
Before starting with a Draft Analysis Operation, we will go to the 'Customize View Parameters' option under the 'View Toolbar'. Then we will enter the 'Customize View Mode' where we will go under the 'Mesh' option and select 'Material' and press 'OK'.
To start the Draft Analysis in the 'Generative Surface Design Workbench', we will go to 'Insert' and then look for the option called 'Analysis'. Once found, we will go under that and click on 'Feature Draft Analysis. This will open the 'Draft Analysis' Dialogue box. There, we will ensure that under 'Mode' we have selected 'Quick Analysis', under 'Display' we will select 'Show or Hide the Color Scale' and then select '3 Degrees' as the permissible draft angle. Then, under 'Direction' we will choose the icon with the symbol of the compass on it which stands for 'Use the Compass to define the new current draft direction'.
- Cavity half – The cavity half is the side of a tool that does not move. It is typically attached to the side of the molding machine.
- Core half – The side of the tool that opens and closes with the molding machine against the cavity half. It opens when removing the part from the tool.
- Cooling lines – Channels that allow coolant to flow throughout the tool and control the cooling of the plastic part.
- Ejector system – Pins on the core half of the tool that helps push the cooled part out after molding.
- Runner – A flow path for the plastic resin allowing the press to inject material directly into the part cavity.
- Side actions – Moving pieces within the part cavity added to allow for undercuts

CREATING THE MAIN TOOLING AXIS:
It is evident from the above image that the Draft-Analysis on our Class A Surface was successful for the degree of 3 degrees.
CONSTRUCTION OF THE CLASS B SURFACE:
We'll start the procedure by creating an offset for the entire Class A Surface at a distance of 2.5mm as that is the desired thickness for our final plastic component.
As this is a complex surface hence the offset will fail to offset every element according to our necessity. It'll select some sub-elements that belong to the filleted regions by themselves that we have to remove to get the rest of the surface that is offset.
To fix all these Patches, we will use the JOIN command in which uncheck the CHECK CONNEXIVITY and in SUB-ELEMENTS TO REMOVE option we will select the filleted surface to remove and click OK. We will do the same for all PATCHES REGION.
After removing the filleted surface, we will disassemble the surface body by using the DISASSEMBLE command. Once the 2 surface domain created we will create the BOUNDARY curve for both surfaces.
After creating the boundary curves, we will use EXTRAPOLATE command to extend the surfaces till the intersection then we will use the TRIM command to remove the extra surfaces and they will be joined together automatically.
The same procedure is followed for all REGION PATCHES, and the final result is below with no PATCH REGION.
CLASS B SURFACE:

PROCEDURE TO CREATE THE CLASS C SURFACE:
We'll create the Class C Surface with respect to the Class A Surface and provide draft angles to those surfaces that are parallel to the Main Tooling Axis. Surfaces at the bottom won't be needing any draft angle as they'll get cleared by the core itself. To create the Class C Surface we have to use various commands such as Sweep with Reference Surface and With Draft-Direction depending upon the necessity and at places where it'll be difficult for us to create a surface using Sweep, we'll use Multi-Sections Surface to create those surfaces.
We've to create two Class C Surfaces, one is for the outer surfaces and the other is for the holed region inside the component and both of them are shown below:
Class C Surface:
After that, we've to trim these joined surfaces with the Class B Surface but before that, we'll create an intersection between these two surfaces and see whether they're feasible to be trimmed with one another. We'll extrapolate those regions where they aren't intersecting and use the intersection command again to inspect whether the intersection is successful or not. When we'll obtain a complete intersection between these two surfaces we'll trim them together to obtain the final closed body as shown below:

FINAL SURFACE BODY:
Finally, we'll go to the Part Workbench and use the option 'Closed Surface' from the 'Surface-based Features' toolbar to convert the final trimmed body into a solid body as shown below:

FINAL SOLID BODY:
After that, we’ll perform a Draft Analysis on the Final Part in Part Workbench.
DRAFT ANALYSIS FOR THE FINAL PART USING THE MAIN TOOLING AXIS:
We'll click on the 'Draft Analysis' under the 'Analysis' Toolbar in the Part Workbench.
Then, we’ll click on the Compass Symbol under 'Direction' which stands for 'Use the Compass to define the new current draft direction'.
We'll drag the compass and place the compass on the Main Tooling-Axis.
Then, we'll select 'Show or Hide the Color Scale' under 'Display' and define our Draft-Angle as 3-Degrees.
As this component was made from a trimmed Class A Surface and hence we aren't required to provide a draft angle to every region. We have provided a draft angle of 3degrees to all the required surfaces.
After that, we'll click the surface of the Final Part the results of which are shown below:

After that, we’ll perform a Draft Analysis on the Final Part in Part Workbench.
DRAFT ANALYSIS FOR THE FINAL PART USING THE MAIN TOOLING AXIS:
We'll click on the 'Draft Analysis' under the 'Analysis' Toolbar in the Part Workbench.
Then, we’ll click on the Compass Symbol under 'Direction' which stands for 'Use the Compass to define the new current draft direction'.
We'll drag the compass and place the compass on the Main Tooling-Axis.
Then, we'll select 'Show or Hide the Color Scale' under 'Display' and define our Draft-Angle as 3-Degrees.
As this component was made from a trimmed Class A Surface and hence we aren't required to provide a draft angle to every region. We have provided a draft angle of 3.2 degrees to all the required surfaces.
After that, we'll click the surface of the Final Part the results of which are shown below:
