Invention Application
US20130251504A1 TURBINE BYPASS SYSTEM 有权
涡轮旁路系统

TURBINE BYPASS SYSTEM
Abstract:
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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