Gas turbine engines and compression systems therefor
Number of patents in Portfolio can not be more than 2000
United States of America
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Mar 24, 2020
Grant Date -
May 30, 2019
app pub date -
Nov 30, 2017
filing date -
Nov 30, 2017
priority date (Note) -
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Abstract
A gas turbine engine, with a conical screw integrated compression system, that utilizes at least one conical screw as an intermediary fluid transport device to facilitate the multi-staging of non-axial compressors, such as centrifugal and diagonal compressors, as well as or alternatively to combine non-axial compressors to axial compressors and to the fan. The conical screw in the compression system applies axial flow translation and funnels, as necessary, the exit flow of the impeller, fan or compressor into the next impeller or compressor.
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