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High-speed taxi-vehicle which is provided with permanent magnetic accelerator and specially used for flight catapult

A technology of accelerators and catapults, applied in the direction of launching/dragging transmissions, etc., can solve problems such as difficulty in carrying and transportation, and high risk

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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Effect test

Embodiment Construction

[0004] It has a special high-speed taxiing trolley for permanent magnetic accelerator flight catapults. The main structure includes sliders, bottom plates, aircraft brackets, rear fixed magnetic rings, front ejection magnetic rings, front fixed pins and pin release structures; four sliders are installed On the lower part of the bottom plate, the aircraft bracket is installed on the bottom plate, the rear fixed magnetic ring and the front ejection magnetic ring are set on the aircraft bracket together, the bottom of the aircraft is installed in front of the front ejection magnetic ring, and the loose pin is installed in front of the bottom of the aircraft to fix it. airplane.

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PUM

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Abstract

The invention discloses a high-speed taxi-vehicle which is provided with a permanent magnetic accelerator and specially used for a flight catapult. The main structure of the high-speed taxi-vehicle comprises sliders, a base plate, an aircraft support, a rear fixing magnetic ring, a front catapult magnetic ring, a front fixing plug pin, a plug pin loosening structure and other components, wherein the four sliders are installed on the lower portion of the base plate, the aircraft support is installed on the base plate, the rear fixing magnetic ring and the front catapult magnetic ring are jointly arranged on the aircraft support in a sleeved mode, the bottom of an aircraft is installed in the front of the front catapult magnetic ring, the loosening plug pin is installed in the front of the bottom of the aircraft, and therefore the aircraft is fixed.

Description

Technical field [0001] The invention relates to a special high-speed gliding trolley with a permanent magnet accelerator for a flight catapult, in particular to a mobile permanent magnet isotropic repulsion accelerator on the upper part of an unmanned aerial vehicle. 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] It has a special high-speed taxiing trolley for permanent magnetic accelerator flight catapults. The main structure includ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64F1/06
Inventor 卓向东
Owner 卓向东