Abstract: A method of managing aircraft exhaust includes providing hot air at a hot air mass flow rate, providing cold air at a cold air mass flow rate, and mixing the hot air and the cold air at a variable hot air mass flow rate to cold air mass flow rate ratio, wherein the variable hot air mass flow rate to cold air mass flow rate ratio is selectively maintained independent of at least one of (1) a variation in the hot air mass flow rate and (2) a variation in a translational speed of the aircraft.
Type:
Grant
Filed:
September 21, 2012
Date of Patent:
May 10, 2016
Assignee:
Bell Helicopter Textron Inc.
Inventors:
Daniel B. Robertson, Dudley E. Smith, Robert M. Laramee