Unmanned aerial vehicle drag augmentation by reverse propeller rotation

An air vehicle configured to augment effective drag to change the rate of descent of the air vehicle in flight via propeller shaft rotation direction reversal, i.e., thrust reversal.

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Bibliographic Details
Main Authors Keennon, Matthew Todd, Cowley, Martyn
Format Patent
LanguageEnglish
Published 23.03.2021
Subjects
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Summary:An air vehicle configured to augment effective drag to change the rate of descent of the air vehicle in flight via propeller shaft rotation direction reversal, i.e., thrust reversal.
Bibliography:Application Number: US201916728366