Separating structure at tail end of sliding track of unmanned plane ejector

Abstract

The invention provides a separating structure at the tail end of a sliding track of an unmanned plane ejector. The separating structure mainly comprises a traction ring wrapping body hook, an electric ejector rod with a hook, an ejector rod motor and the like, wherein the traction ring wrapping body hook is connected with the electric ejector rod with the hook; and the ejector rod motor which is fixed on the bottom of the separating structure is connected with the tail end of the electric ejector rod. When the motor rotates, a traction ring can be driven to move vertically, and the unmanned plane ejector can be separated from the sliding track.

Description

Technical field [0001] The invention relates to a release structure at the end of the slide track of a UAV catapult, in particular to a release structure for a magnetic ring at the end of the slide track of a small aircraft ejection booster. It belongs to the technical field of unmanned aerial vehicle catapults. Background technique [0002] In the field of ejection of small UAVs weighing more than 50 kg, there is no electromagnetic catapult suitable for such UAVs in China. According to reports, only the United States and Israel have similar UAV boosters. Domestically produced rubber band catapults can only eject UAVs under 50 kg can be boosted, and UAVs weighing more than 50 kg can only be boosted by solid explosive rockets, which is very dangerous and very difficult to carry and transport. Contents of the invention [0003] The loose structure at the end of the sliding track of the UAV catapult is mainly composed of a traction ring inclusion hook, an electric ejector wi...

AI Technical Summary

Problems solved by technology

[0002] In the field of ejection of small UAVs weighing more than 50 kg, there is no electromagnetic catapult suitable for such UAVs in China. According to reports, only the United States and Israel have similar UAV boosters. Do...