TY - JOUR
T1 - Development of innovative automated solutions for the assembly of multifunctional thermoplastic composite fuselage
AU - Omairey, Sadik L.
AU - Sampethai, Sofia
AU - Hans, Luka
AU - Worrall, Chris
AU - Lewis, Stuart
AU - Muijs, Leo
AU - Veldman, Sebastiaan L.
AU - Doldersum, Marco
AU - Tonnaer, Rik
AU - More Authors, null
PY - 2021
Y1 - 2021
N2 - In this study, the development of innovative tooling and end-effector systems for the assembly of a multifunctional thermoplastic fuselage is presented. The increasing demand for cleaner and new aircraft requires utilising novel materials and technologies. Advanced thermoplastic composites provide an excellent material option thanks to their weldability, low density, low overall production cost, improved fracture toughness and recyclability. However, to fully appreciate their potentials, new manufacturing approaches and techniques are needed. Hence, this project develops three end-effector solutions to demonstrate the feasibility of assembling a full-scale multifunctional-integrated thermoplastic lower fuselage shell, including the integration of a fully equipped floor and cargo structure. The developed assembly solution comprises three individual yet well-integrated tooling systems that allow housing the skin and assembly; picking, placing and welding of the assembly parts, i.e. clips and stringers; and welding of frames and floor beam sub-assemblies. The process of developing these systems including the end-user requirements, technical challenges, tooling and end-effectors design and manufacturing process are detailed in this paper.
AB - In this study, the development of innovative tooling and end-effector systems for the assembly of a multifunctional thermoplastic fuselage is presented. The increasing demand for cleaner and new aircraft requires utilising novel materials and technologies. Advanced thermoplastic composites provide an excellent material option thanks to their weldability, low density, low overall production cost, improved fracture toughness and recyclability. However, to fully appreciate their potentials, new manufacturing approaches and techniques are needed. Hence, this project develops three end-effector solutions to demonstrate the feasibility of assembling a full-scale multifunctional-integrated thermoplastic lower fuselage shell, including the integration of a fully equipped floor and cargo structure. The developed assembly solution comprises three individual yet well-integrated tooling systems that allow housing the skin and assembly; picking, placing and welding of the assembly parts, i.e. clips and stringers; and welding of frames and floor beam sub-assemblies. The process of developing these systems including the end-user requirements, technical challenges, tooling and end-effectors design and manufacturing process are detailed in this paper.
KW - Aerospace
KW - Automation
KW - Composites
KW - End-effector
KW - Manufacturing
KW - Thermoplastic
UR - http://www.scopus.com/inward/record.url?scp=85112343247&partnerID=8YFLogxK
U2 - 10.1007/s00170-021-07829-2
DO - 10.1007/s00170-021-07829-2
M3 - Article
AN - SCOPUS:85112343247
VL - 117
SP - 1721
EP - 1738
JO - International Journal of Advanced Manufacturing Technology
JF - International Journal of Advanced Manufacturing Technology
SN - 0268-3768
IS - 5-6
ER -