G - Physics – 06 – F
Patent
G - Physics
06
F
G06F 9/50 (2006.01) H04W 88/02 (2009.01) H04N 7/26 (2006.01)
Patent
CA 2626940
Cooling systems (102) for an aircraft (100) are provided. In an embodiment, a system includes an engine nacelle (103), an engine (101), a bypass duct (119), and a heat exchanger (136). The engine nacelle (103) includes an airflow inlet. The engine (101) is housed in the engine nacelle (103) in flow communication with the airflow inlet. The bypass duct (119) extends between the engine nacelle (103) and the engine (101) is in flow communication with the airflow inlet. The bypass duct (119) includes an outer wall (123) and an opening (124) formed therein. The heat exchanger (136) is integrated with the engine (101) and is disposed over the opening (124) of the bypass duct outer wall (123) between the bypass duct outer wall (123) and the engine nacelle (103).
Blake Cassels & Graydon Llp
Research In Motion Limited
LandOfFree
System and method for controlling processor usage according... does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with System and method for controlling processor usage according..., we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and System and method for controlling processor usage according... will most certainly appreciate the feedback.
Profile ID: LFCA-PAI-O-1473153