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US Patent 10533559 Reverse flow engine architecture

Patent 10533559 was granted and assigned to Pratt & Whitney Canada on January, 2020 by the United States Patent and Trademark Office.

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Patent abstract

A reverse flow gas turbine engine has a low pressure (LP) spool and a high pressure (HP) spool arranged sequentially in an axial direction. The LP spool comprises an LP compressor disposed forward of an LP turbine and drivingly connected thereto via an LP compressor gear train. The HP spool comprises an HP compressor in flow communication with the LP compressor, and an HP turbine disposed forward of the HP compressor and drivingly connected thereto via an HP shaft.

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