Conference paper Open Access

Assessing the Integration of Electrified On-Board Systems in an MDAO framework for a small transport aircraft

Fioriti, M.; Della Vecchia, P.; Donelli, G.; Hansmann, P.


Citation Style Language JSON Export

{
  "DOI": "10.2514/6.2021-3094", 
  "author": [
    {
      "family": "Fioriti, M."
    }, 
    {
      "family": "Della Vecchia, P."
    }, 
    {
      "family": "Donelli, G."
    }, 
    {
      "family": "Hansmann, P."
    }
  ], 
  "issued": {
    "date-parts": [
      [
        2021, 
        7, 
        28
      ]
    ]
  }, 
  "abstract": "<p>The integration of on-board systems design within the aircraft design process is often<br>\nconsidered only in the late part of the initial design. This is acceptable for civil aircraft using<br>\nstandard technology systems. However, facing with MEA and AEA concepts and different<br>\npossible architectures, the systems design and the assessment of their effects on the overall<br>\naircraft should be moved up in the usual design process. This paper deals with evaluation of<br>\nthe effect of different on-board systems architecture, with a different electrification level, on<br>\nthe overall aircraft design. These effects have been evaluated using three different MDA<br>\nworkflows developed within the AGILE4.0 European research project. The workflows are<br>\ndefined with an increasing number of disciplines to show how the effect of a proper selection<br>\nof a systems architecture is differently caught by each one. In this way it is possible to define<br>\nwhich disciplines should be included for the systems architecture assessment. The results show<br>\na save of 1% of MTOM for the AEA applied to a small turboprop aircraft when only the OBS<br>\nmass is assessed. Increasing workflow complexity, adding performance and engine design the<br>\nsave increase to 1.2%. Finally, the save increases to 1.3% when the effect on engine SFC is<br>\nalso considered.<br>\n&nbsp;</p>", 
  "title": "Assessing the Integration of Electrified On-Board Systems in an MDAO framework for a small transport aircraft", 
  "type": "paper-conference", 
  "id": "5735193"
}
42
55
views
downloads
Views 42
Downloads 55
Data volume 38.9 MB
Unique views 35
Unique downloads 49

Share

Cite as