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Novel aircraft carrier-based aircraft catapult system

A carrier-based aircraft and aircraft carrier technology, applied in the direction of launch/drag transmission, etc., to achieve the effect of low cost, low cost, and saving training costs

Inactive Publication Date: 2019-07-09
侯力宇
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

For the purpose of carrier-based aircraft ejection, the main purpose is to minimize the fuel consumption of the carrier-based aircraft and ensure that the carrier-based aircraft uses a short-distance take-off runway to take off when the carrier-based aircraft is full of fuel and ammunition. Using the short-distance runway can allow two carrier-based aircraft to take off with full fuel and bombs at the same time, while ensuring that the two carrier-based aircraft with full fuel and bombs take off, without making changes to the ski-jump aircraft carrier and the catapult carrier-based aircraft, the present invention The device applies an external force to the carrier-based aircraft to obtain additional thrust without changing the motor of the catapult-type carrier-based aircraft, so that the carrier-based aircraft can use a short-distance runway to take off when it is full of fuel and ammunition. , and can eject fixed-wing carrier-based aircraft

Method used

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  • Novel aircraft carrier-based aircraft catapult system
  • Novel aircraft carrier-based aircraft catapult system
  • Novel aircraft carrier-based aircraft catapult system

Examples

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Embodiment Construction

[0038] The specific working mode of the present invention is illustrated below through examples.

[0039] The process of the embodiment of the present invention is as attached figure 1 , the system components modules of the embodiment of the present invention are as attached figure 2 , when the embodiment of the present invention is in use, it is under the body of the catapult J-15, and the 203 bowstring hooks the towing rod of the carrier-based aircraft. The present invention includes 201 control part, 202 electric motor, 203 bowstring, 204 storage part, 206 synchronizing device , 207 brake part, 208 wheel, 209 traction rope, each part is as follows:

[0040] 1.201 control part, used to control several other parts, the main functions are as follows:

[0041] Start, start the 202 motor under manual control, make the 202 motor enter the afterburner state, release the 207 brake part, and the 203 bowstring starts to drag the carrier aircraft to accelerate take-off through the ...

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PUM

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Abstract

The invention discloses a novel aircraft carrier-based aircraft catapult system. A carrier-based aircraft take-off power-assisted system does not need to modify an existing ski-jump aircraft carrier deck, and an existing catapult-assisted take-off carrier-based aircraft does not need to be modified, so that an aircraft carrier deck is not damaged, a catapult-assisted take-off carrier-based aircraft body is not caused, and the catapult-assisted take-off carrier-based aircraft achieves full-oil fully-loaded take-off of the catapult-assisted take-off carrier-based aircraft is achieved at low costby using ski-jump aircraft carrier short-distance take-off. The overall combat force of the ski-jump aircraft carrier and the take-off efficiency of the carrier-based aircraft are improved, take-offsorties and risks for executing tasks are reduced, and the number of pilots on the carrier-based aircraft is reduced.

Description

technical field [0001] The invention relates to a novel carrier-based aircraft ejection system, in particular to an ejection-type carrier-based aircraft take-off ejection system for a ski-jump aircraft carrier. Background technique [0002] The Liaoning ship and our country subsequently built a new generation of ski-jump aircraft carriers that are undergoing sea trials. The country has invested about 100 billion yuan in each aircraft carrier. The delivery capability of the carrier-based aircraft is determined by the delivery capability of the carrier-based aircraft, which is mainly related to the dispatch efficiency of the carrier-based aircraft, the loading capacity of each aircraft, fuel and flight radius. It can take off with full fuel and full bombs, and the take-off runway uses a short-distance runway, and the carrier-based aircraft takes off with high efficiency; the Liaoning ship and China's new domestic aircraft carrier can use long-distance runways to achieve carrie...

Claims

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Application Information

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IPC IPC(8): B64F1/06
CPCB64F1/06
Inventor 侯力宇
Owner 侯力宇
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