Christoph Kralovec, Martin Schagerl, Kai-Uwe Schröder,
"Multidisciplinary Conceptual and Structural Design of a New Generation of Aircraft Overhead Stowage Compartment"
, in Deutsche Gesellschaft für Luft- und Raumfahrt (DGLR): Deutscher Luft- und Raumfahrtkongress 2015, DGLR-Publikationsdatenbank, 2015
Original Titel:
Multidisciplinary Conceptual and Structural Design of a New Generation of Aircraft Overhead Stowage Compartment
Sprache des Titels:
Deutsch
Original Buchtitel:
Deutscher Luft- und Raumfahrtkongress 2015
Original Kurzfassung:
This article outlines the systematic approach used to develop a new generation of aircraft overhead stowage
compartment. The discussed overhead stowage compartment is movable. The innovative character and the challenge of
the presented movable overhead stowage compartment is mainly driven by the removal of the classic housing, a
significant stowage enlargement that implies the increase of the payload and demands for a supporting actuator for
opening and closing, improved ergonomics in terms of loading and presence in the cabin and a simple structure that
meets all mechanical needs at the same time with a reduced mass related to comparable existing solutions. The
performed design procedure is based on the state of the art methods of engineering design for mechatronical systems
and its main design stages, system design, domain-specific design and system integration. The focus of the present work
is on the system design in the early design stage and on the structural design within the domain-specific design. It is
presented how the performed systematic approach generates novel design concepts and how a concept develops until
the prototype stage. The work outlines the step-by-step development of the multidisciplinary design concept by analyzing,
abstracting and solving the design task on the basis of an introduced evaluation scheme. Furthermore, the integration of
the structural design in the domain-specific design phase is explicated and the working steps of the structural design are
demonstrated by the considered overhead stowage compartment. Finally, the integration of the domain-specific solutions
to the overall multidisciplinary solution of the aircraft overhead stowage compartment is described and the results of the
successful application of the systematic design approach are presented.
Forschungs-