Comparative Study of Ram Air Turbines based on Wind Tunnel Study for Specific Air Borne Energy Extraction

  • A. Arunachaleswaran National Flight Test Centre, Aeronautical Development Agency, Bangalore - 560 037 http://orcid.org/0000-0002-6823-778X
  • Muralidhar Madhusudan National Flight Test Centre, Aeronautical Development Agency, Bangalore - 560 037
  • A. Ramya Siemens Gamesa Renewable Energy, Bangalore - 560 100
  • S. Elangovan Bharath Institute of Higher Education and Research, Chennai - 600 073
  • M. Sundararaj Bharath Institute of Higher Education and Research, Chennai - 600 073
Keywords: Ram air turbine, Tip speed ratio, Angular velocity, Co-efficient of performance, Solidity, Energy, Aerodynamic braking

Abstract

Ram Air Turbines (RAT) are used for emergency on-board power generation on aircraft and associated systems. Many studies on usage of RATs have shown promising results in terms of using RATs as a source of emergency on-board power generation. Many external podded systems on aircraft utilise RATs for self-sufficient adaptation. These pods generate their own power using RATs for their power requirements instead of depending on the mother aircraft power. Commercial cargo planes use RATs for generating emergency hydraulic power. A RAT was suggested to be used for emergency power, during failure of main alternator on a prototype aircraft. A specific requirement of the RAT was also to produce high drag for aerodynamic braking when deployed and concurrently generate electrical energy. Three models with different solidity were studied in wind tunnel at different wind speeds for suitability of this drag-energy combination. This paper presents the results of the study. Based on the results, a suitable RAT was selected for further analysis and ground trials.

Published
2021-09-02
How to Cite
Arunachaleswaran, A., Madhusudan, M., Ramya, A., Elangovan, S., & Sundararaj, M. (2021). Comparative Study of Ram Air Turbines based on Wind Tunnel Study for Specific Air Borne Energy Extraction. Defence Science Journal, 71(5), 588-593. https://doi.org/10.14429/dsj.71.16636
Section
Aeronautical Systems

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