CPC H04N 23/685 (2023.01) [B64C 39/024 (2013.01); B64D 47/08 (2013.01); F16C 11/0695 (2013.01); F16F 13/007 (2013.01); F16F 15/022 (2013.01); F16F 15/067 (2013.01); F16M 11/06 (2013.01); F16M 11/10 (2013.01); F16M 11/123 (2013.01); F16M 11/18 (2013.01); F16M 11/2071 (2013.01); F16M 13/02 (2013.01); F16M 13/022 (2013.01); G03B 15/006 (2013.01); G03B 17/561 (2013.01); H04N 23/60 (2023.01); B64U 10/13 (2023.01); B64U 30/20 (2023.01); B64U 50/13 (2023.01); B64U 2101/30 (2023.01); F16M 2200/041 (2013.01); F16M 2200/044 (2013.01); H04N 5/77 (2013.01); H04N 7/185 (2013.01)] | 21 Claims |
1. An aerial vehicle comprising:
a chassis;
one or more dampers coupled to the chassis; and
a gimbal sleeve configured to couple to a gimbal of the aerial vehicle, the gimbal sleeve at least partially extending into the chassis, the gimbal sleeve comprising:
a tube structured to couple with a gimbal connector of the gimbal, and an attachment mechanism configured to couple the tube to the chassis, wherein the attachment mechanism comprises:
one or more attachment points;
one or more pins; and
one or more tension elements; wherein the one or more pins extend from the one or more attachment points towards a lower surface of the chassis, further wherein the one or more pins mate with the one or more dampers.
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