A device for launching a drone using spring thrust, in which the means that control the unlocking of an ejection assembly from its armed position include a release housing containing a release chamber, at least one release element which, with the housing, delimits the chamber and is able to move, under the action of the pressure of a gas introduced into the chamber, from a position of rest to a release position in which the at least one release element unlocks the ejection assembly, and return means for returning the at least one release element to the position of rest. The invention also relates to a method for launching drones using the device and to a tool for implementing this method.
DEVICE FOR LAUNCHING A DRONE USING SPRING THRUST, METHOD FOR LAUNCHING DRONES USING THIS DEVICE, AND TOOL FOR IMPLEMENTING THIS METHOD
2025-05-22
Patent
Electronic Resource
English
IPC: | B64U |
European Patent Office | 2024
|Emerald Group Publishing | 2002
MULTICOPTER FOR LAUNCHING DRONE AND METHOD FOR LAUNCHING DRONE USING THE SAME
European Patent Office | 2025
|