RF-Bracket Design

Mass reduction of a mechanical bracket by redesigning the bracket without compromising on thermal, structural and EMC aspects

Master Thesis (2018)
Authors

R.M.J. Caenen (TU Delft - Aerospace Engineering)

Supervisors

Alessandra Menicucci ()

Faculty
Aerospace Engineering, Aerospace Engineering
Copyright
© 2018 Roger Caenen
More Info
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Publication Year
2018
Language
English
Copyright
© 2018 Roger Caenen
Graduation Date
03-04-2018
Awarding Institution
Delft University of Technology
Programme
Aerospace Engineering | Space Systems Engineering
Faculty
Aerospace Engineering, Aerospace Engineering
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Abstract

This thesis shows the mass reduction of a mechanical bracket, without compromising on thermal, EMC and structural aspects. The focus was on analysing thermal aspects related to bracket design. Models were made to show the deflection and solder layer stresses due to CTE mismatches between the bracket and PCB. A thermal heat transfer model was built to analyse the temperature distribution over the bracket and PCB. Using these models, the performance of different materials can be analysed. The most promising candidate for bracket design was aluminum silicon. This material was used in the design of a new bracket. The resulting bracket has a mass of 74 g, which is only 8 % of the mass of the original copper bracket.

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