Speed-reducing and stopping device for aircraft landing

A technology of stopping device and aircraft, applied in the direction of stopping device, etc., can solve the problems affecting the normal walking of personnel, vibration of blocking cables, and the inability of the aircraft to stop, and achieve the effect of avoiding severe vibration and unsightly appearance.

Inactive Publication Date: 2014-06-25
吴汉民
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

One is the risk that the aircraft cannot be stopped due to the failure of the tail hook to hook the arresting wire; the second is that after the aircraft stops, full-time personnel on the aircraft carrier deck need to remove the arresting wire from the tail hook of the aircraft, which is time-consuming and inconvenient. There are safety hazards when the arresting cable rebounds; the third is the risk that the arresting cable may break; the fourth is that when the aircraft wheels pass through the arresting cable at high speed, it will produce violent vibrations, which is unsafe; fifth, the several arresting cables on the deck are not beautiful, affecting personnel walk normally

Method used

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  • Speed-reducing and stopping device for aircraft landing

Examples

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Embodiment Construction

[0033] Embodiment is the landing process of the carrier-based aircraft (3) with tail electromagnet (7) on the aircraft carrier (1). Delimit a rectangular channel as the electromagnetic runway (2) in the center of the landing runway on the deck (10) of the aircraft carrier (1), then design the electromagnet silicon steel sheet size, enameled wire diameter and coil turns, the rated voltage of each group of electromagnets, Electric current etc., perforate on the deck (10) of electromagnetic runway (2) position then, electromagnet is packed in the deck (10), electromagnet magnetic pole direction is vertical with deck (10), and magnetic pole faces up one side and deck ( 10) On the same plane and fixed, the magnetic field on the side facing down and the surrounding sides of the magnetic pole is closed.

[0034] The runway control system (8) ensures sufficient power output according to the rated voltage and current design requirements of the electromagnetic runway (2) electromagnet. ...

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PUM

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Abstract

The invention provides a speed-reducing and stopping device for aircraft landing, and is particularly applicable to landing of a carrier-based aircraft. The speed-reducing and stopping device consists of an electromagnetic runway, a magnetic tail plate and a control system, wherein the electromagnetic runway is arranged in an aircraft landing runway; and the magnetic tail plate is arranged at the tail of the aircraft and can be unfolded or folded. In an aircraft landing process, the magnetic tail plate is unfolded, an electromagnet is electrified, and the direction of a magnetic pole of the magnetic tail plate is opposite to the direction of a magnetic pole of the electromagnetic runway; when the aircraft is close to the runway, the magnetic tail plate is attracted with the electromagnet of the runway, the aircraft is stopped from moving forwards, and the speed of the aircraft is sharply reduced, so that the aircraft can be safely landed within a short time and by a short distance. After the aircraft is stopped, the power of the electromagnet is failed or the current direction is changed, and the magnetic tail plate is separated from the electromagnetic runway and is folded, so that the aircraft can move to an objective position.

Description

technical field [0001] The invention relates to a deceleration and shutdown device for aircraft landing, and is especially suitable for the landing of carrier-based aircraft of an aircraft carrier. Background technique [0002] In order to stop the carrier-based aircraft in time on the deck, the landing deceleration stop device generally adopted is the aircraft tail hook aircraft carrier arresting cable deceleration device. But this deceleration shutdown device still has unsatisfactory part. One is the risk that the aircraft cannot be stopped due to the failure of the tail hook to hook the arresting wire; the second is that after the aircraft stops, full-time personnel on the aircraft carrier deck need to remove the arresting wire from the tail hook of the aircraft, which is time-consuming and inconvenient. There are safety hazards when the arresting cable rebounds; the third is the risk that the arresting cable may break; the fourth is that when the aircraft wheels pass th...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64F1/02
Inventor 吴汉民
Owner 吴汉民
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