Thermal catalytic ignition system for airborne applications

Electric heating – Heating devices – Resistive element: igniter type

Reexamination Certificate

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C102S202500, C089S001814

Reexamination Certificate

active

07569796

ABSTRACT:
A power source is provided for a resistive heating element that heats a catalyst bed of a reactor that receives a monopropellant fuel and reacts the fuel in the presence of the catalyst bed to provide hot gas driving a turbine. The power source is a capacitor that discharges its charge across the resistive heating element so that its temperature is elevated to a point where the reaction of the monopropellant fuel occurs. The power source may be used in airborne applications, such as emergency power systems for aircraft, where it is desirable to minimize the weight of the unit and to allow the unit to use safer monopropellant fuels.

REFERENCES:
patent: 4500775 (1985-02-01), Sangu et al.
patent: 4510377 (1985-04-01), Merritt et al.
patent: 4925386 (1990-05-01), Donnelly et al.
patent: 5608179 (1997-03-01), Voecks et al.
patent: 6244036 (2001-06-01), Christie et al.
patent: 6769241 (2004-08-01), Spanjers et al.
Mike Koerner, “Recent Developments in Aircraft Emergency Power”, symposium, American Institute of Aeronautics and Astronautics, 2000, Honeywell Corporation, Torrance, CA.

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