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US Patent 7797922 Gas turbine engine case and method of making

Patent 7797922 was granted and assigned to Pratt & Whitney Canada on September, 2010 by the United States Patent and Trademark Office.

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Patent abstract

A casing for an aircraft turbine bypass engine comprises a splitter having slots to receive and be welded to a plurality of struts extending between an outer ring and an inner hub of the casing.

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