Performance Assessment of Turbocharged Pem Fuel Cell Systems for Civil Aircraft Onboard Power Production

Author:

Campanari Stefano1,Manzolini Giampaolo1,Beretti Andrea1,Wollrab Uwe2

Affiliation:

1. Dipartimento di Energetica, Politecnico di Milano, Piazza Leonardo da Vinci 32, 20133 Milano, Italy

2. Systems Engineering, Fuel Cell Systems Development, AIRBUS Deutschland Gmbh, 21129Hamburg, Germany

Abstract

In recent years, civil aircraft projects are showing a continuous increase in the demand of onboard electrical power, both for the partial substitution of hydraulic or pneumatic controls and drives with electrical ones, and for the consumption of new auxiliary systems developed in response to flight safety and environmental control issues. Aiming to generate onboard power with low emissions and better efficiency, several manufacturers and research groups are considering the possibility to produce a relevant fraction of the electrical power required by the aircraft by a fuel cell system. The first step would be to replace the conventional auxiliary power unit (based on a small gas turbine) with a polymer electrolyte membrane (PEM) fuel cell type, which today is favored with respect to other fuel cell types; thanks to its higher power density and faster startup. The PEM fuel cell can be fed with a hydrogen rich gas coming from a fuel reformer, operating with the same jet fuel used by the aircraft, or relying on a dedicated hydrogen storage onboard. The cell requires also an air compression unit, where the temperature, pressure, and humidity of the air stream feeding the PEM unit during land and in-flight operation strongly influence the performance and the physical integrity of the fuel cell. In this work we consider different system architectures, where the air compression system may exploit an electrically driven compressor or a turbocharger unit. The compressor type and the system pressure level are optimized according to a fuel cell simulation model, which calculates the cell voltage and efficiency as a function of temperature and pressure, calibrated over the performances of real PEM cell components. The system performances are discussed under different operating conditions, covering ground operation, and intermediate and high altitude cruise conditions. The optimized configuration is selected, presenting energy balances and a complete thermodynamic analysis.

Publisher

ASME International

Subject

Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering

Reference27 articles.

1. Fuel Cell APU’S in Commercial Aircraft-An Assessment of SOFC and PEMFC Concepts;Eelman

2. Fuel Cell APU for Commercial Aircraft;Daggett

3. Anon, 2005, “6th European Framework Program, PROPAIR: Processing of Kerosene for PEM Fuel Cell Applications for Aircraft,” Airbus Internal Document, Part B, July.

4. Anon, 2005, “6th European Framework Program, CELINA: Fuel Cell Integration in a new Configured Aircraft,” Description of Work-Airbus Internal Documents, February.

5. Anon, 2006, “787 Special-Electric Dream,” Flight International, pp. 58–59; http://www.flightglobal.com/articles

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