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Rotary acceleration type takeoff launching rack

A launcher and acceleration technology, which is applied in the direction of launch/drag transmission, aircraft parts, ground devices, etc., can solve the problems of reduced aircraft combat capability, high maintenance costs, human and aircraft injuries, etc., to reduce the difficulty of landing, The effect of improving ship landing safety and improving combat effectiveness

Pending Publication Date: 2017-05-31
谭燕斌
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The take-off efficiency of vertical take-off and ski jump take-off is very low, and it cannot take off with full load, so the combat capability of the aircraft is greatly reduced; the structure of the ejection take-off device is complex, the cost is high, the energy consumption is high, the normal service life is short, and the maintenance cost is high; the area occupied Large, large acceleration overload during take-off, causing great damage to people and aircraft, and the take-off efficiency is not high

Method used

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  • Rotary acceleration type takeoff launching rack
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Embodiment

[0022] A rotary acceleration type take-off launcher, comprising

[0023] Launcher column 15, the launcher column 15 is a column that can accelerate the rotation around the axial direction, and the column has a built-in acceleration motor;

[0024] Launcher arm 14, described launcher arm 14 is telescopic, and described launcher arm 14 is arranged on the top of described launcher column 15, and the telescoping end of launcher arm 14 is provided with automatic gripper 13;

[0025] Lifting oil cylinder 16, described lifting oil cylinder 16 is arranged on the column body of described launching stand column 15, and the telescoping end of lifting oil cylinder 16 is connected with launching stand arm 14;

[0026] The rotary acceleration type take-off launcher includes an early warning command aircraft take-off launcher 1, a UAV take-off launcher 5 and a carrier-based fighter take-off launcher 7.

[0027] The rotary acceleration type take-off launcher is arranged on the deck shipboard...

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PUM

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Abstract

The invention discloses a rotary acceleration type takeoff launching rack for an aircraft carrier. The rotary acceleration type takeoff launching rack comprises a launching rack upright column, launching rack arms and a lifting oil cylinder. The launching rack upright rod is an upright column is an upright column with axial acceleration and rotation functions; the telescopic launching rack arms are arranged on the upper portion of the launching rack upright column, and automatic grips are arranged at telescopic ends of the launching rack arms; the lifting oil cylinder is arranged on a column body of the launching rack upright column, and a telescopic end of the lifting oil cylinder is connected with the launching rack arms; the rotary acceleration type takeoff launching rack comprises a warning director takeoff launching rack, unmanned aerial vehicle takeoff launching racks and ship-borne fighter aircraft takeoff launching racks. The rotary acceleration type takeoff launching rack can be arranged on decks of two ship sides of the aircraft carrier, the warning director takeoff launching rack, the unmanned aerial vehicle takeoff launching racks and an island of the aircraft carrier are arranged on the same side of the aircraft carrier, and the ship-borne fighter aircraft takeoff launching racks are arranged on the other side of the aircraft carrier. The rotary acceleration type takeoff launching rack has the advantages of safety, high efficiency, simple structure, small occupied space and low manufacturing cost and energy consumption.

Description

technical field [0001] The invention relates to an accelerated take-off device for aircraft carrier-based fighter jets, in particular to a rotary acceleration type take-off launcher. Background technique [0002] At present, the take-off methods of aircraft carrier-based fighter jets mainly include vertical take-off, ski jump take-off and catapult take-off, and catapult take-off is divided into steam catapult take-off and electromagnetic catapult take-off. These take-off modes have very high requirements on the performance of the aircraft itself. The take-off efficiency of vertical take-off and ski jump take-off is very low, and it cannot take off with full load, so the combat capability of the aircraft is greatly reduced; the structure of the ejection take-off device is complex, the cost is high, the energy consumption is high, the normal service life is short, and the maintenance cost is high; the area occupied Large, the acceleration overload is large during take-off, wh...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64F1/04B64F1/22
CPCB64F1/04B64F1/222
Inventor 谭燕斌
Owner 谭燕斌
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