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aircraft electromagnetic runway

A technology for aircraft and runways, applied in the direction of roads, roads, ships for aircraft, etc., can solve the problems of low flexibility, long landing runway distance, large footprint, etc., to achieve shortened taxiing distance, flexibility and practicality High, small footprint effect

Active Publication Date: 2020-05-01
合肥凯石投资咨询有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] The technical problem to be solved by the present invention is to provide an aircraft electromagnetic runway, which solves the shortcomings of traditional aircraft such as long landing runway distance, large floor space, and low flexibility.

Method used

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Embodiment Construction

[0029] In order to make the technical means, creative features, goals and effects achieved by the present invention easy to understand, the present invention will be further described below in conjunction with specific illustrations.

[0030] combine Figure 1 to Figure 7 Shown, the embodiment structure of a kind of aircraft electromagnetic runway, it comprises the runway body that is boat-shaped (the front end is a triangular tip, the rear end is a flat end), and the runway body is made up of four runway monomers 1 side by side, which are respectively the first runway The monomer 1a, the second raceway monomer 1b, the third raceway monomer 1c and the fourth raceway monomer 1d, the first raceway monomer 1a and the second raceway monomer 1b are movably connected by the first connecting piece 2a, the second The second raceway monomer 1b and the third raceway monomer 1c are flexibly connected through the second connecting piece 2b, and the third raceway monomer 1c and the fourth ...

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Abstract

The invention discloses an aircraft electromagnetic runway. The aircraft electromagnetic runway comprises a runway body; the runway body consists of a plurality of runway single bodies; the adjacent runway single bodies are movably connected through a connecting piece; an electromagnetic circuit is arranged at the top end of each runway single body; a controller as well as a power supply and a driving device which are connected with the controller are arranged in each runway single body; the power supply is connected with the electromagnetic circuit; and the driving device is used for providing power for the runway single bodies. The electromagnetic runway is placed at a position with certain depth below the horizontal plane during use; the electromagnetic circuit is arranged on the runway, so that a mutual repulsion force is generated to retard collision between an aircraft and water surface when the aircraft is close to the water surface, and a mutual attraction force is generated toshorten the sliding distance of the aircraft when the aircraft lands on the water surface and slides forwards; the runway has a small occupied area and safe landing of the aircraft is guaranteed; andthe electromagnetic runway can be driven to different places to use, the electromagnetic runway can adjust the own width and area according to requirements, and flexibility and practicability are high.

Description

technical field [0001] The invention relates to the technical field of aircraft runways, in particular to an electromagnetic runway for aircraft on water. Background technique [0002] There are now seaplanes used for maritime patrol, anti-submarine, rescue and sports, tourism, commuting, aerial photography, etc., whose take-off and landing are all carried out on water. Correspondingly, it is necessary to set up special take-off and landing runways on the water, among which the landing runway is more demanding, because a little carelessness will cause an accident under the huge impact force. [0003] In addition, various types of aircraft, such as airplanes, sometimes encounter forced landings due to malfunctions, bird strikes, or hijackings during flight. A considerable part of the accidents occurred when there was no land for emergency landings, so they had to choose the sea. The plane was forced to land, but there were no special landing facilities on the sea surface, wh...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B63B35/53B63B35/52E01C9/00
CPCB63B35/52B63B35/53E01C9/00
Inventor 万可
Owner 合肥凯石投资咨询有限公司
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