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Aircraft carrier carrier-bearing and land-aviation fixed wing aircraft take-off method

An aircraft take-off and fixed-wing technology, which is applied to the launch/tug transmission device and other directions, can solve the problems of inability to complete the flight operation, complicated control, and high cost, and achieves reduction of design, R&D, manufacturing, training and maintenance costs and safety factors. High, simple construction effect

Inactive Publication Date: 2016-10-26
匡仲平
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Its disadvantages are: it is impossible to get rid of the high dependence on the taxi take-off runway, and it is expensive, complex in structure, cumbersome in operation, extremely difficult and dangerous, and its core technology is monopolized by developed countries, difficult to obtain, and controlled by others...
Once the airport runway is damaged, it may not be possible to complete the take-off operation

Method used

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Embodiment Construction

[0030] The carrier-borne and land-flight fixed-wing aircraft take-off method described in this combined invention is unlocked by the steam ejection force, electromagnetic ejection force, especially the spring ejection force, respectively with the engine thrust and binding of the aircraft carrier-mounted and land-flight fixed-wing aircraft Resistance composition;

[0031] The take-off method of carrier-borne and land aviation fixed-wing aircraft described in this combination invention adds spring ejection on the basis of existing steam ejection and electromagnetic ejection;

[0032] The take-off method of carrier-based and land aviation fixed-wing aircraft described in this combination invention is realized by docking and combining various types of ejection devices, especially spring ejection devices, aircraft carrier-borne and land aviation fixed-wing aircraft engines and binding unlocking devices. A technical feature effect that is superior to the sum of the above individual ...

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PUM

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Abstract

The invention provides an aircraft carrier carrier-bearing and land-aviation fixed wing aircraft take-off method and relates to improvement and innovation of aircraft carrier carrier-bearing and land lift-off fixed wing aircraft take-off technical methods. Force is composed of steam catapulting force, electromagnetic catapulting force, especially spring catapulting force and thrust of an engine and binding and unlocking resistance of an aircraft carrier carrier-bearing and land-aviation fixed wing aircraft, and spring catapulting with the compression and stretching reset functions is added on the basis of the existing steam catapulting and electromagnetic catapulting. The method is characterized in that various types of catapulting devices especially the spring catapulting device are combined with the engine and the bonding and unlocking device of the aircraft carrier carrier-bearing and land-aviation fixed wing aircraft in a butt joint manner, accumulation is collected and stored and synchronously released instantly to generate extreme specific impulse, and the method is used for achieving the technical feature effect more superior to the sum of the above single technical feature effects. The take-off manner of the fixed wing aircraft used for aircraft carrier carrier-bearing and land lift-off is changed into a launching take-off manner from a sliding take-off manner under the working condition that no sliding runway is needed, and multi-craft multi-line quick and direct take-off and lift-off at the same time period are achieved.

Description

technical field [0001] The invention relates to the improvement and innovation of aircraft carrier-borne fixed-wing aircraft and other take-off technical methods of land-launched fixed-wing aircraft. Background technique [0002] At present, the existing technical solutions are limited to improving the aircraft to launch and fly through the clamping device. Although all functions are used to bind and unlock the catapult, and finally launch the aircraft, the single structure leads to energy storage and energy gathering. Insufficient, which in turn may cause the key technical problem that the release energy is not enough to drive the carrier-based and land aviation fixed-wing aircraft with relatively large take-off weight to realize the improvement from taxi take-off to launch and flight. [0003] At present, the more advanced take-off methods of carrier-based fixed-wing aircraft are simple steam bomb catapult take-off or electromagnetic catapult take-off. Its disadvantages a...

Claims

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Application Information

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IPC IPC(8): B64F1/06
CPCB64F1/06
Inventor 匡仲平
Owner 匡仲平
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