Hover-capable Flapping-wing Aircraft

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dc.contributor.assigneeTexas A&M University Systemen
dc.creatorBenedict, Moble
dc.creatorColeman, David A.
dc.date.accessioned2023-05-03T13:33:32Z
dc.date.available2023-05-03T13:33:32Z
dc.date.filed12/20/2018
dc.date.issued10/25/2022
dc.description.abstractA flapping-wing aircraft includes a support frame, a motor coupled to the support frame, a pair of wings coupled to the support frame, and a linkage assembly coupled to the support frame and configured to translate an output torque of the motor into flapping motion of the wings, wherein the linkage assembly includes a first link coupled to a rotational output of the motor, a second link pivotably coupled to the first link at a first pivot joint, a third link pivotably coupled to the second link at a second pivot joint, and a fourth link pivotably coupled to the support frame and slidably coupled to the third link, and wherein the fourth link is coupled to a first wing of the pair of wings.en
dc.description.countryUS
dc.format.digitalOriginreformatted digitalen
dc.identifier.patentapplicationnumber16/762516
dc.identifier.urihttps://hdl.handle.net/1969.1/197544
dc.languageEN
dc.publisherUnited States. Patent and Trademark Officeen
dc.publisher.digitalTexas A&M University. Libraries
dc.rightsPublic Domain (No copyright - United States)en
dc.rights.urihttp://rightsstatements.org/vocab/NoC-US/1.0/
dc.subject.cpcprimaryB64C 19/02
dc.subject.cpcprimaryB64C 3/26
dc.subject.cpcprimaryB64C 33/02
dc.subject.cpcprimaryF16H 21/40
dc.subject.cpcprimaryB64C 3/185
dc.subject.cpcprimaryB64D 27/24
dc.subject.cpcprimaryB64C 13/18
dc.titleHover-capable Flapping-wing Aircraften
dc.typeUtility patenten

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