Drone Payload Release Button with Sloping Aperture Edges

The release mechanism is segmented into distinct functional components: a button member for actuation, an aperture with sloping edges for guiding, and a tag system for payload attachment. This segmentation allows each component to perform its specific function reliably while keeping the overall design simple and manageable.

The mechanism employs self-service features where the sloping edges of the aperture automatically guide the tag into the correct position, and the button member automatically returns to its initial position after actuation. This self-guiding and self-resetting capability enhances reliability without adding complex control systems.

The attachment mechanism transitions from a static secured state to a dynamic release state through simple button actuation. The sloping edges provide a dynamic guiding path that automatically engages the tag during insertion and facilitates easy ejection during release, enabling both secure attachment and quick release operations.

The tag serves as an intermediary element between the button member and the payload. It transmits the actuation force from the button to the payload while maintaining secure attachment during transport, and enables clean separation during release without requiring direct manipulation of the payload itself.

Instead of using a complex active ejection system that pushes the tag out, the design inverts the approach by using passive gravity-assisted ejection. The sloping edges are configured so that when the button member returns to its initial position, the tag naturally slides out along the sloping surface under gravity, achieving automatic ejection without additional actuators or complex mechanisms.

The design replaces complex mechanical ejection systems with a simpler gravity-based passive ejection mechanism. The sloping edges create a gravity-assisted path that automatically ejects the tag after payload release, eliminating the need for motors, springs, or other active mechanical ejection components.