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Stream/Area:
-
Subject:
-
Paper ID:
10.55041/IJSREM35180
Volume:
8 |
5 |
May 2024
Pages:
Publication Frequency:
Monthly (12 issues per year)
License:International Journal of Scientific Research in Engineering and Management follows the Creative Commons Attribution 4.0 (CC BY 4.0) License, allowing free use and distribution with proper attribution.
The objective of the study is to select a material for the propeller mount of a drone. Propeller mount is used to hold the propeller and motor firmly. Hence the material should possess good strength and wear properties. The existing material used in propeller mount is Aluminium made through the casting method. In this study, the Aluminium (Al) matrix with nano boron nitride (BN) and nano titanium di oxide (TiO2) reinforcements are used for fabrication of specimens through powder metallurgy route. The best specimen is chosen using multi-objective optimization grey relational analysis method. Based on the study, S2 (97.5 wt% Al + 1.25 wt% BN + 1.25 wt% TiO2) specimen is selected for fabrication of propeller mount in the drone.
KEYWORDS
Publication Date
12/31/45442
Peer Review Type
Double-Blind Peer Review
Review Rounds: 2
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Conflict of Interest
The authors declare no conflict of interest related to this research work.
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