GAS TURBINE COMBUSTION CHAMBER WITH INTEGRATED TURBINE INLET GUIDE VANE RING AS WELL AS METHOD FOR MANUFACTURING THE SAME
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United States of America Patent
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Jan 12, 2017
app pub date -
Jul 5, 2016
filing date -
Jul 6, 2015
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Abstract
A gas turbine combustion chamber with an outer combustion chamber wall and an inner combustion chamber wall, wherein the outer combustion chamber wall and the inner combustion chamber wall are respectively formed in one piece with an outer or an inner ring-shaped platform that are connected in one piece with turbine inlet guide vanes which are arranged around the circumference, wherein the gas turbine combustion chamber is mounted only by means of a suspension device that is formed in one piece at the outer platform, as well as a method for manufacturing the same.
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