An assembly for an aircraft having a propeller, including an engine assembly having an engine shaft configured for driving engagement with the propeller. The engine assembly includes first and second heat exchangers configured for circulation of at least one of a liquid coolant and a lubricant therethrough. A wheel well is configured for receiving a retracted landing gear. A first cooling duct receives the first heat exchanger and has a first outlet downstream of the first heat exchanger, and a second cooling duct receives the second heat exchanger and has a second outlet downstream of the second heat exchanger. The outlets are in direct fluid communication with an environment of the aircraft, and laterally spaced from each other. The wheel well is located between the outlets. A method of cooling an engine assembly is also discussed.
AIRCRAFT WITH WHEEL WELL BETWEEN COOLING DUCT OUTLETS
2019-08-22
Patent
Elektronische Ressource
Englisch
Aircraft with wheel well between cooling duct outlets
Europäisches Patentamt | 2020
|AIRCRAFT WITH WHEEL WELL BETWEEN COOLING DUCT OUTLETS
Europäisches Patentamt | 2019
|AIRCRAFT WITH WHEEL WELL BETWEEN COOLING DUCT OUTLETS
Europäisches Patentamt | 2021
|Improved Trench Film Cooling With Shaped Trench Outlets
Online Contents | 2013
|Improved Trench Film Cooling With Shaped Trench Outlets
Online Contents | 2013
|