Turbine bypass system

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United States of America Patent

PATENT NO 9726082
APP PUB NO 20130251504A1
SERIAL NO

13902133

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Abstract

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A turbine bypass system comprises a bypass path which is selectively operable to deliver hot gases to a gas cooler and a pebble bed positioned in the bypass path upstream of the gas cooler. The pebble bed absorbs heat from the bypass gases and thereby reduces the temperature of the bypass gases prior to delivery of the bypass gases to the gas cooler.

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Patent Owner(s)

Patent OwnerAddress
ARABELLE SOLUTIONS FRANCE32 AVENUE PABLO PICASSO NANTERRE 92000

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Tothill, Mark Harvey Bedford, GB 3 18

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