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Aerospace Fuel Cell Systems

Aerospace Fuel Cell Systems

Proton Exchange Membrane Fuel Cell

Overview

The experiment observed the results of subjecting a hydrogen-anode, air-breathing cathode Proton Exchange Membrane (PEM) fuel cell stack to the pressures and temperatures encountered at atmospheric conditions existing at altitudes up to 55,000 feet.

Experimental results were used to develop a computer model that can accurately simulate fuel cell performance at these extreme low pressure and low temperature conditions.

Experimental Setup photo collageExperimental Setup

Goals

Results

  1. PEM fuel cell performance at conditions existing at high altitudes can be measured experimentally.
  2. Voltage, current, and hydrogen consumption decrease with a decrease in pressure.  This effect depends on the load applied to the stack.


    Fuel cell voltage, current, and hydrogen consumption
    all decrease with decreasing pressure.
    Fuel cell voltage, current, and hydrogen consumption all decrease with decreasing pressure. Chart #1

    Fuel cell voltage, current, and hydrogen consumption all decrease with decreasing pressure. Chart #2

    Fuel cell voltage, current, and hydrogen consumption all decrease with decreasing pressure. Chart #3


  3. The exchange current density (io) term used in the Tafel equation has a high dependence on the ambient air pressure for an air-breathing PEMFC stack.
  4. Using a pressure and temperature dependent io, a computer model can predict actual fuel cell stack performance at high altitudes reasonably well.


The computer model is used to predict fuel cell performance used
to provide 36 kW of auxiliary power on a large passenger jet.


charts: The computer model is used to predict fuel cell performance used to provide 36 kW of auxiliary power on a large passenger jet.

charts: The computer model is used to predict fuel cell performance used to provide 36 kW of auxiliary power on a large passenger jet.

Recent Publications

Pratt, J. (2004).  “Experimental Evaluation and Computer Simulation of a Proton Exchange Membrane Fuel Cell at High-Altitude Conditions,” M.S. Thesis, University of California Irvine, Irvine, CA, 2004.

Pratt, J., Brouwer, J., and Samuelsen, G. S. (2003). “Experimental Evaluation and Computer Simulation of an Air-Breathing PEM Fuel Cell at Aircraft Flight Altitudes,” 2003 Fuel Cell Seminar,  Nov. 3-6, Miami Beach, FL.

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