Integrated Working Fluid and System Optimization for Airborne Waste Heat Recovery Applications

Integrated Working Fluid and System Optimization for Airborne Waste Heat Recovery Applications

Master Thesis (2025)
Author(s)

M.E. Krikke (TU Delft - Aerospace Engineering)

Contributor(s)

Carlo M. De Servi – Mentor (TU Delft - Flight Performance and Propulsion)

L. Galieti – Mentor (TU Delft - Flight Performance and Propulsion)

Piero Colonna – Graduation committee member (TU Delft - Flight Performance and Propulsion)

K. Hooman – Graduation committee member (TU Delft - Heat Transformation Technology)

Faculty
Aerospace Engineering
More Info
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Publication Year
2025
Language
English
Graduation Date
20-05-2025
Awarding Institution
Delft University of Technology
Programme
['Aerospace Engineering']
Faculty
Aerospace Engineering
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Abstract

This study investigates optimizing working fluids and system design for Waste Heat Recovery (WHR) in turboelectric aircraft, focusing on the Onera Dragon concept. Using the PC-SAFT equation of state and QSPR models, the research identifies optimal fluids for an Organic Rankine Cycle (ORC)-based airborne WHR system. The method includes optimizing pseudo-fluids, which are mapped to real fluids based on PC-SAFT parameter proximity. A bi-objective optimization also attempts to find real-fluid optima directly. The best pseudo-fluid achieved a 1.56% fuel saving, while the best real fluid, acetyl chloride, achieved 1.37%, outperforming cyclopentane’s 0.92%. The bi-objective approach did not yield better real-fluid results. Binary mixtures of non-polar pseudo-fluids and blends of cyclopropane and cyclopentane showed no improvement, indicating no benefit from temperature glide in the condenser.

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