DLR Institute of Structures and Design releases video on TB-Rumpf welded thermoplastic composites
Autoclave-free consolidation and resistance welding validated for future aircraft thermoplastic composite fuselage.
Photo Credit: DLR Institute of Structures and Design
CW published news about this in Sept. 2021 (see “DLR Institute of Structures and Design increases maturity of thermoplastic composite fuselage structures”). Now, DLR Institute of Structures and Design (Stuttgart, Germany) has released a video showcasing its work as part of the BMWK-funded LuFoV-3 project called TB-Rumpf. In this project, DLR has demonstrated autoclave-free consolidation and resistance welding of thermoplastic composite laminates as technology bricks for future aircraft fuselages. This work was carried out in collaboration with aerospace industry partners and research institutes.
Shooting and postproduction: Lichtwerk-Fotografie Tobias Blaser
For more information, visit DLR TB-Rumpf
Related Content
-
PEEK vs. PEKK vs. PAEK and continuous compression molding
Suppliers of thermoplastics and carbon fiber chime in regarding PEEK vs. PEKK, and now PAEK, as well as in-situ consolidation — the supply chain for thermoplastic tape composites continues to evolve.
-
Materials & Processes: Fibers for composites
The structural properties of composite materials are derived primarily from the fiber reinforcement. Fiber types, their manufacture, their uses and the end-market applications in which they find most use are described.
-
Materials & Processes: Fabrication methods
There are numerous methods for fabricating composite components. Selection of a method for a particular part, therefore, will depend on the materials, the part design and end-use or application. Here's a guide to selection.
