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Multipurpose attack and transportation integrated aircraft

An aircraft, multi-purpose technology, applied in the field of aircraft, to achieve the effect of large combat radius, lasting firepower, and strong precision strike capability

Pending Publication Date: 2021-11-05
尚之灏
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The analysis found that the above three attack aircraft have obvious shortcomings, and we need more advanced attack aircraft

Method used

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  • Multipurpose attack and transportation integrated aircraft
  • Multipurpose attack and transportation integrated aircraft
  • Multipurpose attack and transportation integrated aircraft

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0031] Such as Figures 1 to 4 As shown, the multi-purpose attack and transportation integrated aircraft includes the aircraft body. The upper part of the aircraft body is sequentially provided with a cockpit 1, a fuel tank 2, an air intake 3, and an engine 4. The aircraft body is equipped with a drone, and the lower part of the aircraft body is installed. There are radar 5 and avionics equipment 6, and radar 5 and avionics equipment 6 are positioned at the lower part of cockpit 1, and aircraft body has modular accommodation cabin body 7, and accommodation cabin body 7 can accommodate precision guided missile (not shown in the figure), At least one of combat personnel, ground combat equipment (not shown in the figure), and containers (not shown in the figure), the drone can guide precision guided missiles, and guided missiles include air-to-air missiles, air-to-ground missiles, cruise missiles, Anti-ship missiles, anti-radiation missiles, the aircraft body is 18 meters long, 4...

Embodiment 2

[0046] Such as figure 1 , 5 As shown in and 6, on the basis of Embodiment 1, the bottom of the aircraft body has a second installation groove 15, and the unmanned aerial vehicle 9 is installed in the second installation groove 15, and the bottom of the second installation groove 15 has two flip doors 16. The two reversing doors 16 can be turned over relative to the second installation groove 15 to realize the opening or closing of the second installation groove 15, and the turning directions of the two reversing doors 16 are opposite; the two opposite side walls 17 of the second installation groove 15 are both A hydraulic drive device 18 is installed, and the output shaft 19 ends of the hydraulic drive device 18 all have a limit arc pressure plate 20, and the limit arc pressure plate 20 on both sides is used to top the fuselage of the unmanned aerial vehicle 9 and inspect it tightly. Form a limit, the limit arc pressure plate 20 is compatible with the body of the unmanned aer...

Embodiment 3

[0048] On the basis of Embodiment 1 or 2, the reconnaissance UAV 8 is configured as a flexible frequency transceiver, and the flexible frequency transceiver is configured to selectively change the communication frequency of the flexible frequency transceiver, and the flexible frequency transceiver is configured to communicate with The aircraft body communicates with the unmanned aerial vehicle 9 for reconnaissance and strike, and the communication frequency between the unmanned aerial vehicle 8 for reconnaissance and the unmanned aerial vehicle 9 for reconnaissance and strike can be changed.

[0049] As a communication relay station, the reconnaissance UAV 8 can change the frequency between the reconnaissance UAV 8-aircraft body, the reconnaissance UAV 8-reconnaissance and strike integrated UAV 9, and is used to protect the smooth communication when it is subject to electronic interference. Thereby guide the unmanned aerial vehicle 9 fixed-point removal target of inspecting and...

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Abstract

The invention relates to a multipurpose attack and transportation integrated aircraft which is characterized by comprising an aircraft body, a cabin, an oil tank, an air inlet channel and an engine are sequentially arranged in the upper portion of the aircraft body from front to back, an unmanned aerial vehicle is installed on the aircraft body, a radar and avionics equipment are installed in the lower portion of the aircraft body, and are located in the lower portion of the cabin, the aircraft body is provided with a modularized containing cabin body, the containing cabin body can contain at least one of precise guidance missiles, combat personnel, ground combat equipment and containers, and the unmanned aerial vehicle can guide the precise guidance missiles. The aircraft is high in accurate strike capacity, lasting in firepower and large in combat radius, does not need a nose to aim at and launch ammunition, can be guided by the unmanned aerial vehicle to launch outside a ground fire network, accurately hit a target and is large in ammunition loading amount, so that long pressing time is achieved, and the aircraft has combat and tactical transportation capacity due to the containing cabin.

Description

technical field [0001] The present disclosure relates to the technical field of aircraft, in particular to a multi-purpose attack and transport integrated aircraft. Background technique [0002] From the First World War to the present, there are three basic tasks of ground attack aircraft - attacking armored targets, attacking mobile personnel and attacking buildings and positions. The main scenes are all low-intensity in the air and high-intensity on the ground. [0003] At present, there are many types of aircraft that can be used as attack aircraft, such as A-10 type low-to-medium value subsonic combat attack aircraft, unmanned aerial vehicles, and armed helicopters. Among them, armed helicopters are traditional close-range large-scale land combat weapons. , the intensity of the armed helicopter is low, the suppression time and survivability are not very good, it needs to fight at close range, the combat radius is extremely low, the intensity of the reconnaissance and st...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D7/00B64D7/08
CPCB64D7/00B64D7/08
Inventor 尚之灏
Owner 尚之灏
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