Have a personal or library account? Click to login
Transforming a Cantilever with Fixed Joints into Trussed Configurations: A Case Study in Creative Design Thinking & Prototyping Cover

Transforming a Cantilever with Fixed Joints into Trussed Configurations: A Case Study in Creative Design Thinking & Prototyping

Open Access
|May 2025

Figures & Tables

Figure 1.

Realized T1 configuration of the Y-shaped, cantilever arm assembled from standardized beech wood profiles and bespoke, 3D printed joints
Realized T1 configuration of the Y-shaped, cantilever arm assembled from standardized beech wood profiles and bespoke, 3D printed joints

Figure 2.

Left: Benchmark Y-shaped, polyhedral cantilever with fixed joints in side and top view. Right: T1 with coordinates, and indication of node 10 (load point c10), node 23 (load point c23), and node 15 (0/0/0 = c0)
Left: Benchmark Y-shaped, polyhedral cantilever with fixed joints in side and top view. Right: T1 with coordinates, and indication of node 10 (load point c10), node 23 (load point c23), and node 15 (0/0/0 = c0)

Figure 3.

Y-shaped, polyhedral cantilever with fixed joints as benchmark versus configurations T1-T5. The arrows indicate the differences between the individual configurations
Y-shaped, polyhedral cantilever with fixed joints as benchmark versus configurations T1-T5. The arrows indicate the differences between the individual configurations

Figure 4.

Optimized cross-sections for beech wood (color coded) for configurations T1 to T5. Dimensions of standardized circular profile cross-sections in 2, 2.2, 2.5, 3, 3.5, 4, 4.5, 5, and 6 cm in diameter
Optimized cross-sections for beech wood (color coded) for configurations T1 to T5. Dimensions of standardized circular profile cross-sections in 2, 2.2, 2.5, 3, 3.5, 4, 4.5, 5, and 6 cm in diameter

Figure 5.

Configuration T1 and its displacements as simulated in Karamba3D. The cantilever was loaded by self-weight and vertical loads of 0.5 kN to both nodes 10 and 23
Configuration T1 and its displacements as simulated in Karamba3D. The cantilever was loaded by self-weight and vertical loads of 0.5 kN to both nodes 10 and 23

Figure 6.

Left: Resultant force replacing concentrical tension rods in multi-arm nodes by use of graphic statics. Center: 3D printing Node 11 including two through-the-joint-mounted fittings (also see Figure 8) by PrusaSlicer, Prusa i3 MK3 and PLA NX2. Right: 3D printed joints ready for T1 assembly
Left: Resultant force replacing concentrical tension rods in multi-arm nodes by use of graphic statics. Center: 3D printing Node 11 including two through-the-joint-mounted fittings (also see Figure 8) by PrusaSlicer, Prusa i3 MK3 and PLA NX2. Right: 3D printed joints ready for T1 assembly

Figure 7.

Left: Two point-clouds from laser-scan with local coordinate system, target balls and reconstructed cylinders. Center: Scans from unloaded (green) and loaded (red) structure. Right: Example of reconstructed cylinder from approximately 1300 scanned points
Left: Two point-clouds from laser-scan with local coordinate system, target balls and reconstructed cylinders. Center: Scans from unloaded (green) and loaded (red) structure. Right: Example of reconstructed cylinder from approximately 1300 scanned points

Figure 8.

Top: Overview of nodes. Bottom left: Node 19 with six wooden members and one threated tension rod. Bottom center: Node 19 in the realized structure. Bottom Right: Identical point 



c→19
{\vec {\rm c}_{19}}


 (blue dot) of the joint i=19 with six wooden members
Top: Overview of nodes. Bottom left: Node 19 with six wooden members and one threated tension rod. Bottom center: Node 19 in the realized structure. Bottom Right: Identical point c→19 {\vec {\rm c}_{19}} (blue dot) of the joint i=19 with six wooden members

Results of the computational comparison between the different configurations at the two load points

load point c10 {{\rm{\vec c}}_{{\rm{10}}}} load point c23 {{\rm{\vec c}}_{{\rm{23}}}}
Difference vector Δci {\rm{\Delta }}{{\rm{\vec c}}_i} : Δx [cm]:3.211.39
Δy [cm]:0.521.84
Δz: [cm]:3.603.57
Euclidian norm Δci \left\| {{\rm{\Delta }}{{{\rm{\vec c}}}_i}} \right\| [cm]: 4.854.25
Directional angle αi [°]: 0.10.4
initial configurationend configurationinitial configurationend configuration
elevation to the horizontal plane βi [°]:40.4339.6927.4126.79
DOI: https://doi.org/10.2478/acee-2025-0009 | Journal eISSN: 2720-6947 | Journal ISSN: 1899-0142
Language: English
Page range: 113 - 128
Submitted on: Jun 24, 2024
Accepted on: Jan 3, 2025
Published on: May 10, 2025
Published by: Silesian University of Technology
In partnership with: Paradigm Publishing Services
Publication frequency: 4 issues per year

© 2025 Günther H. Filz, Robert Eberle, Pia V. Nagl, Thomas Weinold, published by Silesian University of Technology
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 License.