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Virtual testing of multifunctional moveable actuation systems

Hollmann, Rene Walter and Schäfer, Andreas and Bertram, Oliver and Rädel, Martin (2022) Virtual testing of multifunctional moveable actuation systems. CEAS Aeronautical Journal. Springer. doi: 10.1007/s13272-022-00602-5. ISSN 1869-5590.

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Official URL: https://link.springer.com/article/10.1007/s13272-022-00602-5

Abstract

This work presents the current state of the virtual testing activities performed within the Virtual Product House (VPH) start-up project. In this project a multidisciplinary, collaborative end-to-end process for virtual product design is developed. On the basis of preliminary design and concept studies on aircraft level, the process focusses on design, manufacturing and testing of aircraft systems and structural components with special attention to certification aspects. The initial use case considers the trailing edge flap of a long-range aircraft and its actuation system. Design and analysis tools are integrated in a remote workflow execution environment to automatically generate designs and evaluate them by virtual test means. Virtual tests facilitate knowledge on properties and behavior of the virtual product in early development phases and allow to optimize design flaws in consecutive design iterations to hence reduce the risk of costly corrections later in the development process. The testing is setup in multiple stages. Currently, domain-specific tests are carried out for the moveable structure and its actuation system, with the latter being in focus for the current text. These tests address the functional verification of the actuation system in nominal and failure cases. A SysML model comprising system requirements and architecture is used to model test cases and trace test results. On the basis of these test cases, simulation configurations for virtual tests are automatically built, executed and evaluated. With this method, a continuous evaluation of designs in terms of functional verification of the moveable actuation system is possible. Moreover, the automated execution of all steps allows to determine the effects of design changes quickly without a large amount of labor-intensive and error-prone work.

Item URL in elib:https://elib.dlr.de/187774/
Document Type:Article
Title:Virtual testing of multifunctional moveable actuation systems
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Hollmann, Rene WalterUNSPECIFIEDhttps://orcid.org/0000-0002-0546-7406UNSPECIFIED
Schäfer, AndreasUNSPECIFIEDhttps://orcid.org/0009-0001-3564-2578UNSPECIFIED
Bertram, OliverUNSPECIFIEDhttps://orcid.org/0000-0002-7732-9280UNSPECIFIED
Rädel, MartinUNSPECIFIEDhttps://orcid.org/0000-0002-3181-3202UNSPECIFIED
Date:1 August 2022
Journal or Publication Title:CEAS Aeronautical Journal
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:No
DOI:10.1007/s13272-022-00602-5
Publisher:Springer
ISSN:1869-5590
Status:Published
Keywords:Virtual testing, Virtual product, Modeling and simulation, MBSE
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Components and Systems
DLR - Research area:Aeronautics
DLR - Program:L CS - Components and Systems
DLR - Research theme (Project):L - Aircraft Systems
Location: Braunschweig
Institutes and Institutions:Institute of Flight Systems > Safety Critical Systems&Systems Engineering
Institute of Composite Structures and Adaptive Systems > Structural Mechanics
Institute of Flight Systems
Institute of Composite Structures and Adaptive Systems
Deposited By: Hollmann, Rene Walter
Deposited On:29 Aug 2022 09:10
Last Modified:29 Nov 2022 18:43

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