US 12338014 B2 / Jun 24, 2025

Off-center parachute flight termination system including latch mechanism disconnectable by burn wire

Systems, devices, and methods including: a latching mechanism comprising: a first latch configured to attach to a door of an unmanned aerial vehicle (UAV); a second latch configured to attach to a portion of the UAV distal from the first latch; a string connected between the first and second latch, where the string secures the door shut; at least two radio modules in communication with a ground control station; and at least two burn wires in contact with a portion of the string between the first latch and the second latch; where current from a backup battery passes to at least one burn wire when the burn signal is received, where the burn wire causes the connection between the first latch and the second latch to be broken and the door of the UAV is separated from the UAV, and where the parachute is deployed when the door of the UAV is separated from a rest of the UAV.

Publication details

Recorded assignee
AeroVironment, Inc.
Publication number
US 12338014 B2
Publication type
Utility patent grant
Publication date
Jun 24, 2025
Filing date
Nov 16, 2023
CPC classes
B64U70/83, B26F3/12, B64D17/34, B64D17/62, B64D17/80, B64U10/13, B64U20/65, B64U2101/20, B64U2201/20
Inventors
Lisoski; Derek, Sechrist; William Stuart

Party names reflect the published document. Current ownership and legal status can change.

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