摘要 |
One embodiment of the present invention is an integrated aero-engine flowpath structure. Another embodiment is a method of manufacturing integrated aero-engine flowpath structure. Other embodiments include apparatuses, systems, devices, hardware, methods, and combinations for aero-engine flowpath structures. Further embodiments, forms, features, aspects, benefits, and advantages of the present application shall become apparent from the description and figures provided herewith. |
申请人 |
ROLLS-ROYCE NORTH AMERICAN TECHNOLOGIES, INC.;RESS, ROBERT, A.;YOUNT, RANDALL, E.;DESTEFANO, THOMAS, D.;PATEL, JITENDRA, R. |
发明人 |
RESS, ROBERT, A.;YOUNT, RANDALL, E.;DESTEFANO, THOMAS, D.;PATEL, JITENDRA, R. |