Abstract
| Language | English |
|---|---|
| Number of pages | 4 |
| Publication status | Published - 6 Feb 2019 |
| Event | MEA2019 (More Electric Aircraft) - Diagora, Centre de Congrès et d’Exposition, Toulouse, France Duration: 6 Feb 2019 → 7 Feb 2019 https://www.see.asso.fr/en/node/22822 |
Conference
| Conference | MEA2019 (More Electric Aircraft) |
|---|---|
| Country | France |
| City | Toulouse |
| Period | 6/02/19 → 7/02/19 |
| Internet address |
Fingerprint
Keywords
- hybrid electric propulsion aircraft
- propulsion
- propulsion design
Cite this
}
Feature modelling as a new architectural approach for the accelerated integration and early-stage development of hybrid-electric propulsion, MEA and MEE architectures. / Sztykiel, Michal; Norman, Patrick; Galloway, Stuart; Burt, Graeme.
2019. Paper presented at MEA2019 (More Electric Aircraft), Toulouse, France.Research output: Contribution to conference › Paper
TY - CONF
T1 - Feature modelling as a new architectural approach for the accelerated integration and early-stage development of hybrid-electric propulsion, MEA and MEE architectures
AU - Sztykiel, Michal
AU - Norman, Patrick
AU - Galloway, Stuart
AU - Burt, Graeme
PY - 2019/2/6
Y1 - 2019/2/6
N2 - This paper presents a feature modelling philosophy and the developed tool, which can be used to support the conceptual design of future generation aircraft electrical architectures. The proposed feature model has been developed in FeatureIDE and consists of four sequential modelling stages, which are programmed to automatically narrow the selection of feasible design options in order to accelerate the complete system specification and documentation. The paper illustrates the feature modelling process, which starts from the identification of high-level aircraft and engine characteristics, considers medium-level electrical architecture layout options, before finally considering the detailed low-level characteristics of individual components.
AB - This paper presents a feature modelling philosophy and the developed tool, which can be used to support the conceptual design of future generation aircraft electrical architectures. The proposed feature model has been developed in FeatureIDE and consists of four sequential modelling stages, which are programmed to automatically narrow the selection of feasible design options in order to accelerate the complete system specification and documentation. The paper illustrates the feature modelling process, which starts from the identification of high-level aircraft and engine characteristics, considers medium-level electrical architecture layout options, before finally considering the detailed low-level characteristics of individual components.
KW - hybrid electric propulsion aircraft
KW - propulsion
KW - propulsion design
UR - https://www.see.asso.fr/en/MEA2019
M3 - Paper
ER -