Patent 8356467 was granted and assigned to Pratt & Whitney Rocketdyne on January, 2013 by the United States Patent and Trademark Office.
A system, such as a turbine power production system, including a plurality of combustion chambers. The combustion chamber may be provided with an ignition system that allows for substantially simultaneous ignition of each of the plurality of the combustors. Generally, a detonation wave may be provided to each of the combustion chambers substantially simultaneously from a single ignition combustion wave chamber.