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An Algorithmic Morphology Matrix for Aircraft Fuel System Design
Linköpings universitet, Institutionen för ekonomisk och industriell utveckling, Maskinkonstruktion. Linköpings universitet, Tekniska högskolan.
Linköpings universitet, Institutionen för ekonomisk och industriell utveckling, Maskinkonstruktion. Linköpings universitet, Tekniska högskolan.
Linköpings universitet, Institutionen för ekonomisk och industriell utveckling, Maskinkonstruktion. Linköpings universitet, Tekniska högskolan.
2006 (engelsk)Inngår i: 25th Congress of the International Council of the Aeronautical Sciences, Hamburg, Germany, 2006, nr ICAS-2006-9.2.2Konferansepaper, Publicerat paper (Fagfellevurdert)
sted, utgiver, år, opplag, sider
2006. nr ICAS-2006-9.2.2
HSV kategori
Identifikatorer
URN: urn:nbn:se:liu:diva-12982OAI: oai:DiVA.org:liu-12982DiVA, id: diva2:17586
Tilgjengelig fra: 2008-04-01 Laget: 2008-04-01 Sist oppdatert: 2009-03-02
Inngår i avhandling
1. On aircraft fuel systems: conceptual design and modeling
Åpne denne publikasjonen i ny fane eller vindu >>On aircraft fuel systems: conceptual design and modeling
2007 (engelsk)Doktoravhandling, med artikler (Annet vitenskapelig)
Abstract [en]

The largest and most important fluid system in an aircraft is the fuel system. Obviously, future aircraft projects involve the design of fuel system to some degree. In this project design methodologies for aircraft fuel systems are studied, with the aim to shortening the system development time.

This is done by means of illustrative examples of how optimization and the use of matrix methods, such as the morphological matrix, house of quality and the design structure matrix, have been developed and implemented at Saab Aerospace in the conceptual design of aircraft fuel systems. The methods introduce automation early in the development process and increase understanding of how top requirements regarding the aircraft level impact low-level engineering parameters such as pipe diameter, pump size, etc. The morphological matrix and the house of quality matrix are quantified, which opens up for use of design optimization and probabilistic design.

The thesis also discusses a systematic approach when building a large simulation model of a fluid system where the objective is to minimize the development time by applying a strategy that enables parallel development and collaborative engineering, and also by building the model to the correct level of detail. By correct level of detail is meant the level that yields a simulation outcome that meets the stakeholders’ expectations. The experienced gained at Saab in building a simulation model, mainly from the Gripen fuel system, but also the accumulated experience from other system models, is condensed and fitted into an overall process.

sted, utgiver, år, opplag, sider
Institutionen för ekonomisk och industriell utveckling, 2007
Serie
Linköping Studies in Science and Technology. Dissertations, ISSN 0345-7524 ; 1067
Emneord
Aircraft, morphological matrix, simulation, Saab, Gripen
HSV kategori
Identifikatorer
urn:nbn:se:liu:diva-11146 (URN)978-91-85643-04-2 (ISBN)
Disputas
2007-02-23, C3, Hus C, Campus Valla, Linköpings universitet, Linköping, 10:15 (engelsk)
Opponent
Veileder
Tilgjengelig fra: 2008-04-01 Laget: 2008-04-01 Sist oppdatert: 2020-03-24

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Gavel, HampusAndersson (Ölvander), JohanJohansson (Lundén), Björn

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