US Patent 11760464 Yaw alleviation mechanism for aircraft collision
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US Patent 11760464 Yaw alleviation mechanism for aircraft collision
Article
Patent abstract
A yaw alleviation device for an aircraft containing rotatable wing roots attached to wings. The device includes a spring configured to operatively connect to a wing; and a buckling member to operatively connect to the wing. The spring is configured to extend from an original unstrained position upon the buckling member undergoing buckling from an original unbuckled position to cause rotation of one or both wings in rotationally opposite directions. The buckling member may be positioned parallel and at an offset distance to the spring.
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Patent Number
Patent Inventor Names
Christopher M. Kroninger
John T. Hrynuk
Michael R. Dorothy
Robert A. Haynes
Todd C. Henry
Date of Patent
September 19, 2023
Patent Application Number
17326911
Date Filed
May 21, 2021
Patent Citations
Patent Primary Examiner
CPC Code
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