Abstract: One embodiment of the present invention is a gas turbine engine with a bypass mixer. Other embodiments include apparatuses, systems, devices, hardware, methods, and combinations for gas turbine engines and bypass mixers. Further embodiments, forms, features, aspects, benefits, and advantages of the present application will become apparent from the description and figures provided herewith.
Type:
Grant
Filed:
August 5, 2011
Date of Patent:
January 27, 2015
Assignee:
Rolls-Royce North American Technoloies, Inc.