Rolls-royce Corporation

Robert R Moritz

Gerard D Agnew

Michele Bozzolo

Olivier C Tarnowski

A system comprising a solid oxide fuel cell stack and a gas turbine engine. The stack comprises a plurality of solid oxide fuel cells, each fuel cell comprises an electrolyte, an anode and a cathode. The gas turbine engine comprises a compressor and a turbine with the compressor supplying oxidant to the cathodes. There are means to supply fuel to the anodes and to supply a portion of the unused oxidant from the solid oxide fuel cells to the cathodes. The means to supply a portion of the unused oxidant comprises a combustor and an ejector with the combustor burning a portion of the unused fuel from the solid oxide fuel cells in the portion of the unused oxidant from the fuel cells and is arranged to supply products of the combustor to the oxidant supplied by the compressor to the cathodes to preheat the oxidant supplied by the compressor.

Solid oxide fuel cell system

In order to evaluate the condensation amount in a jet engine intake duct, for calibrating the engine, apparatus are provided which induce a high speed flow of air through a duct. The duct is designed so that the air velocity within it very gradually increases along it until a choked (sonic) condition is reached. At or around sonic conditions static pressure is very responsive to changes in flow due to condensation. Thus by first obtaining a pressure profile along the duct under non-condensing conditions and then comparing this with a pressure profile under condensing conditions a condensation amount can be computed.

Method and apparatus for evaluating condensation amount

A low drag surface comprises at its upstream edge an intermittent linear vortex producing means extending transverse to the flow of fluid across the surface. The vortex producing means produces a succession of rolling vortices which roll across the surface reducing the drag between the main flow and the surface.

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Indianapolis, IN, United States of America

Robert R Moritz