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Tail end magnetic ring releasing device for aircraft booster

A booster and aircraft technology, applied in the direction of launching/dragging transmissions, etc., can solve the problems of high risk, difficulty in carrying and transportation, etc.

Inactive Publication Date: 2014-03-26
卓向东
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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. Domestically produced rubber band catapults can only eject Boost drones below 50 kg, and drones weighing more than 50 kg can only be boosted by solid explosive rockets, which is very dangerous and very difficult to carry and transport

Method used

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Examples

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Embodiment Construction

[0004] The loose structure of the magnetic ring at the end of the taxiing track of a small aircraft, the main structure includes the inclusion hook of the traction ring, the electric ejector rod with the hook and the ejector motor; the inclusion hook of the traction ring is connected with the electric ejector rod with the hook , the ejector motor fixed at the bottom is connected to the end of the electric ejector; when the motor rotates, it can drive the traction ring to produce vertical displacement, so as to realize loosening.

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PUM

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Abstract

The invention provides a tail end magnetic ring releasing device for an aircraft booster. The tail end magnetic ring releasing device mainly and structurally comprises a towing ring wrapping body hook, an electric ejecting rod with a hook, an ejecting rod motor and the like. The towing ring wrapping body hook is connected with the electric ejecting rod with the hook. The ejecting rod motor fixed to the bottom is connected with the tail end of the electric ejecting rod. When the motor rotates, a towing ring can be driven to shift perpendicularly, and therefore releasing is achieved.

Description

Technical field [0001] The invention relates to an end magnetic ring loosening device of an aircraft booster, in particular to a release structure for a magnetic ring end of a 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 of the magnetic ring at the end of the taxiing track of a small aircraft, the main structure includes the inclusion hook of the traction ring, t...

Claims

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Application Information

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IPC IPC(8): B64F1/06
Inventor 卓向东
Owner 卓向东
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