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Performance variation of a helicopter turboprop with respect to manufacturing tolerances
KTH, School of Engineering Sciences (SCI), Aeronautical and Vehicle Engineering, Flight Dynamics.
2013 (English)Independent thesis Advanced level (degree of Master (Two Years)), 20 credits / 30 HE creditsStudent thesis
Abstract [en]

This paper focuses on the performance dispersion of the turboprop Turbomeca Arriel2D.

The first part describes the engine architecture and the different aerodynamic parameters which affect the performance characteristics. Then an inventory of the most important tolerances with respect to engine performance is taken. The second part describes why and how a new model of the turboprop has been created to evaluate the degradation. Finally, the results obtained with a Monte-Carlo Method are close to the empirical methods and give several hints in order to improve the manufacturing tolerances.

Place, publisher, year, edition, pages
2013. , 14 p.
Series
Trita-AVE, ISSN 1651-7660 ; 2013:19
National Category
Aerospace Engineering
Identifiers
URN: urn:nbn:se:kth:diva-129419OAI: oai:DiVA.org:kth-129419DiVA: diva2:652377
Subject / course
Aeronautical Engineering
Examiners
Available from: 2013-09-30 Created: 2013-09-30 Last updated: 2013-09-30Bibliographically approved

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CiteExportLink to record
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Citation style
  • apa
  • harvard1
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Language
  • de-DE
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  • en-US
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  • nn-NO
  • nn-NB
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  • Other locale
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Output format
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