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Implementation of a new inlet protection system into HEMS fleet

Bartosz Stanisław Przybyła (Faculty of Mechanical Engineering and Mechatronics, West Pomeranian University of Technology Szczecin, Szczecin, Poland)
Radoslaw Przysowa (Department for Aero-Engines, Air Force Institute of Technology, Warszawa, Poland)
Zbigniew Zapałowicz (Faculty of Mechanical Engineering and Mechatronics, West Pomeranian University of Technology Szczecin, Szczecin, Poland)

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 2 December 2019

Issue publication date: 13 January 2020

133

Abstract

Purpose

EC-135P2+ helicopters operated by Polish Medical Air Rescue are highly exposed to environmental particles entering engines when performing helicopter emergency medical services. This paper aims to assess the effectiveness of inlet barrier filters installed to protect the engines, including their impact on maintenance.

Design/methodology/approach

The organisation adopted a comprehensive set of measures to predict and limit the impact of dust ingestion including visual inspections, health management and engine trend monitoring based on ground power checks’ (GPC) results. Three alternative particle separation solutions were considered. Finally, helicopter inlets were modified to allow the selected filter system to be installed, which reduced the number of particles ingested by the engine and prevented from premature overhauls.

Findings

The analyses carried out enabled not only the selection of the optimal filtration solution and its seamless implementation into the fleet but also confirmed its efficiency. After installing the filters, engines’ lifetime is extended from 500 to 4,500 flight hours while operating costs and the number of maintenance tasks was reduced significantly.

Originality/value

Lessons learned from operational experience show that a well-matched particle separation system can mitigate accelerated engine deterioration even if the platform is continuously exposed to environmental particles. The remaining useful life of engines can be predicted using performance models and data from GPC.

Keywords

Acknowledgements

This article is based upon a conference paper Implementation of a New Inlet Protection System into HEMS Fleet, hosted on www.sto.nato.int/publications/STO

Citation

Przybyła, B.S., Przysowa, R. and Zapałowicz, Z. (2019), "Implementation of a new inlet protection system into HEMS fleet", Aircraft Engineering and Aerospace Technology, Vol. 92 No. 1, pp. 67-79. https://doi.org/10.1108/AEAT-11-2018-0289

Publisher

:

Emerald Publishing Limited

Copyright © 2019, Emerald Publishing Limited

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