PROPELLER DESIGN IMPROVED WITH REGARD TO ITS INTERACTION WITH A COMBUSTION AIR INLET
An aircraft assembly 100 includes an engine 110, and intake 120, and a propeller assembly 130. The engine 110 is mounted to at least one of a wing 112 or fuselage of an aircraft 102. The intake 120 is configured to provide air to the engine 110. The intake 120 includes a body 122 having an engine in...
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Format: | Patent |
Sprache: | eng ; fre ; ger |
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