Page 35 - ILK Research Report 2020
P. 35

PEP4.0

            Development of a highly efficient linked product development process
            (PEP) for hybrid lightweight structures in the context of Industry 4.0



                                                                             Period
                                                                             01.07.2018 – 31.03.2022
                                                                             Project Director
                                                                             Prof. Dr.-Ing. habil. Maik Gude

                                                                             Contact Person
                                                                             Dr.-Ing. Sebastian Spitzer
                                                                             Funding
                                                                             •  Federal Ministry for Economic Affairs
                                                                               and Energy (BMWi)
                                                                             •  German Aerospace Center (DLR)

                                                                             Project Partner
                                                                             •  Rolls-Royce Deutschland Ltd & Co KG
                                                                             •  CTC GmbH
            Fig. 1: Interactive development process with the individual disciplines of design, layout and
            manufacturing (top) along the phases from specification of requirements to manufacturing
            (bottom)















            Fig. 2: Technological possibilities (left), functional necessities (right)
            and synthesis of technology and function in the structure (centre)

            In the project “PEP4.0”, the ILK is collaborating with Rolls-
            Royce Deutschland to research on efficient methods for   Fig. 3: Virtual (top) and real validation (bottom) from the overall
            developing an engine intermediate case (IMC) in met-  engine model (WEM, left) to the individual components of a Vane
            al-composite design. The basis for this is a digitally linked   (right) and linking of the individual elements via a digital twin (middle)
            product development process, which combines the
            methods, models and data of the individual disciplines   be able to assess the effect of a parameter change in the
            of design, dimensioning and manufacturing in a linked   overall system. In parallel, the virtual results and models
            development structure from the specification of require-  are verified and validated with real tests (see Fig. 3).
            ments up to the manufacturing (see Fig. 1).      The project is funded under the fifth aviation research
            Within  the  framework  of  the  project,  a  function-  and   program (LuFo) of the German Federal Ministry for Eco-
            stress-oriented design takes place (top-down, ILK). The   nomic Affairs and Energy BMWi (FKZ 20X1717B).
            design determined in this way is aligned with the tech-
            nological options available for aerospace applications
            (bottom-up). The synthesis of geometry and material re-
            sults in the function- and production-oriented structure
            of a lightweight intermediate case (see Fig. 2). The tech-                       Supervised by:
            nological work is carried out in close cooperation with
            CTC GmbH.
            Within individual development phases, models are con-
            sidered at different levels from the single component
            vane up to the overall engine model (WEM) in order to




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