Upload
others
View
8
Download
0
Embed Size (px)
Citation preview
The information in this presentation is proprietary and confidential and shall not be disclosed to or
used by a third party unless specif ically authorised by the relevant GKN plc group company.
MSc. Thesis presentation
Topology-optimization-based model definition with manufacturing constraints
1
Mariniello Emanuele I 12/06/2019
Supervisors Co-supervisor
Prof. Alberto Boschetto Ing. Timi Ojo Rus
Prof.ssa Luana Bottini
Proprietary and confidential restrictions on title slide apply throughout this presentation
11155
Rev.
2
Aim
2
Proprietary and confidential restrictions on title slide apply throughout this presentation
11155
Rev.
2
Presentation outline
3
1. Introduction
- Additive Manufacturing
- Topology Optimization
2. Topology Optimization
- Methodology
- Outputs
3. Post Processing
- Methodology
- Outputs
- Comparison
4. Conclusions and Further works
Proprietary and confidential restrictions on title slide apply throughout this presentation
11155
Rev.
2
Additive Manufacturing
4
The Additive Manufacturing processes are classified into 7 categories:
a) VAT Photopolymerization
b) Material Jetting
c) Binder Jetting
d) Material Extrusion
e) Powder Bed Fusion
f) Sheet Lamination
g) Directed Energy Deposition
Proprietary and confidential restrictions on title slide apply throughout this presentation
11155
Rev.
2
Topology Optimization
5
It is a mathematical method that optimizes material with the typical goal of reduce the
mass of an object without compromise the mechanical resistance of its structure.
Solid Isotropic Material with Penalization (SIMP)
Proprietary and confidential restrictions on title slide apply throughout this presentation
11155
Rev.
2
Topology Optimization Software
6
➢ Hyperworks
➢ Ansys
➢ Siemens NX
Proprietary and confidential restrictions on title slide apply throughout this presentation
11155
Rev.
2
Topology Optimization - Procedure
7
1. Enough space to insert the pin in the lug;
2. Each interfaces between two consecutive sectors
needs to be flat;
3. Original flanges to maintain the seal condition and
design guidelines;
4. No application of “Air Force Method” normative.
Design Space constraints:
Proprietary and confidential restrictions on title slide apply throughout this presentation
11155
Rev.
2
Design Space and No Design Space
8
Proprietary and confidential restrictions on title slide apply throughout this presentation
11155
Rev.
2
Mechanical Loads
9
Proprietary and confidential restrictions on title slide apply throughout this presentation
11155
Rev.
2
Mechanical Loads
10
Dummy
TRS
Load
Constraints
Proprietary and confidential restrictions on title slide apply throughout this presentation
11155
Rev.
2
Topology Optimization parameters
11
Mindim: 7,5
Maxdim: 15
Stress Constraint: < 800 MPa
Volume fraction: 0,05
Objective function: minimize compliance
Proprietary and confidential restrictions on title slide apply throughout this presentation
11155
Rev.
2 Threshold:
0,505
TO Hyperworks Output
12
Proprietary and confidential restrictions on title slide apply throughout this presentation
11155
Rev.
2
Post Processing constraints
13
1. The output of the TO has rough surface, it must be smoothed;
2. The connection between BHS and TRS must be closed;
3. Geometry on the bottom that allows to perform the liquid penetrate
inspection;
4. To reduce excessive use of support material, the structure needs to
have an overhang angle lower than 45 degrees, where it is possible.
Proprietary and confidential restrictions on title slide apply throughout this presentation
11155
Rev.
2
Post Processing “Concept 1” (No overhang angle constraints)
14
Weight Reduction:
31 %
Proprietary and confidential restrictions on title slide apply throughout this presentation
11155
Rev.
2
Post Processing “Concept 2” (with overhang angle constraints)
15
Proprietary and confidential restrictions on title slide apply throughout this presentation
11155
Rev.
2
Post Processing “Concept 2” (with overhang angle constraints)
16
Weight Reduction:
28 %
Proprietary and confidential restrictions on title slide apply throughout this presentation
11155
Rev.
2
“Concept 1” vs “Concept 2”
17
Concept 1 Concept 2
OTM
Displacement AnalysisOriginal
≈ 4 mm
≈ 3,8 mm
≈ 6 mm
Proprietary and confidential restrictions on title slide apply throughout this presentation
11155
Rev.
2
“Concept 1” vs “Concept 2”
18
FBO Tension
Stress Analysis
Concept 1
Concept 2
Max ≈ 1000 MPa
Max ≈ 780 MPa
Max ≈ 750 MPa
Original
Proprietary and confidential restrictions on title slide apply throughout this presentation
11155
Rev.
2
Post Processing “Concept 3” (Trade off)
19
Weight Reduction:
25 %
Proprietary and confidential restrictions on title slide apply throughout this presentation
11155
Rev.
2
“Original” vs “Concept 3” – Stiffness X
20
Original Concept 3
≈ 3,8 mm ≈ 4,2 mm
Proprietary and confidential restrictions on title slide apply throughout this presentation
11155
Rev.
2
“Original” vs “Concept 3” – FBO Tension
21
Original Concept 3
Max ≈ 750 MPa Max ≈ 1100 Mpa
(locally)
Proprietary and confidential restrictions on title slide apply throughout this presentation
11155
Rev.
2
Conclusion
22
• Weight reduction of 25%
• Reduction of support area of 13%
• More investigations about stresses
Proprietary and confidential restrictions on title slide apply throughout this presentation
11155
Rev.
2
Further Works
Presentation title 23
1. Topology Optimization implementing of the thermal stresses, drag
forces, fatigue and unexpected loads on the TRS;
2. Performing the Topology Optimization at more sectors at the same
time because each sector has different stresses;
Proprietary and confidential restrictions on title slide apply throughout this presentation
11155
Rev.
2
24
Thanks for the attention