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Combined and detached airplane

A technology of combining and disassembling aircrafts, which is applied in the field of aircrafts, can solve problems such as inability to combine and disassemble, and achieve the effect of increasing passenger capacity and increasing flight distance

Inactive Publication Date: 2014-01-15
李沛霖
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] In order to solve the shortcomings that the aircraft cannot be combined and disassembled during flight, the invention provides a combined and disassembled aircraft. The sub-machines of the aircraft can not only be combined with the main machine to load passengers and cargo, but also can be disassembled in time in the air according to the needs. , which can not only avoid air accidents in time, but also can disperse and land in different regions. It is safe, convenient and practical. It is a breakthrough design in aircraft design

Method used

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  • Combined and detached airplane
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Embodiment Construction

[0014] exist figure 1 Among them, the combination decomposes the aircraft, including: a main engine 10 and a sub-machine 9; the aircraft has a main engine 10 with a platform 8 on its back, wings 3 are provided on both sides of the main engine 10, and a horizontal empennage 5 and a vertical empennage 4 are provided at the tail of the main engine; The abdomen of 10 is provided with fuel tank, and fuel oil is housed in the fuel tank; On the platform 8 of main engine back, be provided with automatic hook, catapult and several sub-machines 9 are housed, automatic hook, catapult and main engine fuel tank are connected with platform respectively. Several loaded sub-machines 9 are matched and connected; when needed, the automatic hook, catapult and fuel tank can be automatically unhooked, ejected and cut off fuel; the sub-machines are respectively provided with a sub-machine cab 2 and a passenger and cargo compartment.

[0015] The sub-machine wings 6 and the sub-machine horizontal t...

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PUM

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Abstract

The invention relates to a combined and detached airplane. The airplane is provided with a main cabin with the back provided with a platform, the two sides of the main cabin are provided with wings, and the tail of the main cabin is provided with a horizontal tail wing and a vertical tail wing. An oil tank is arranged on the belly part of the main cabin, and fuel oil is arranged in the oil tank. An automatic hook, an ejector and a plurality of auxiliary cabins are arranged on the platform of the back of the main cabin, and the automatic hook, the ejector and the oil tank of the main cabin are connected with the auxiliary cabins on the platform respectively. When need exists, the automatic hook can automatically disengage, the ejector can automatically carry out ejection and the oil tank can automatically carry out fuel cut. Auxiliary cabin wings and auxiliary cabin horizontal tail wings can be respectively folded upwards from the wing root connecting position. The auxiliary cabins of the airplane can be separated from and combined with the main cabin, the passenger capacity of the airplane can be increased due to the fact that the auxiliary cabins carry passengers, and the auxiliary cabins can be fast separated from the main cabin as soon as possible for escaping when the air crash happens. In the process of executing a task, the airplane can be fast detached to carry out different tasks. The main cabin and the auxiliary cabins of the airplane can store engine oil, and therefore the flying range of the airplane is increased.

Description

technical field [0001] The invention relates to an aircraft, in particular to a combined and disassembled aircraft with a sub-machine and a sub-machine and a main machine that can be decomposed and combined. Background technique [0002] At present, military aircraft or civil aircraft are a complete and independent whole, which cannot be assembled and disassembled in time during flight, and cannot be disassembled and avoided in time when encountering some air accidents; when flying to different regions in the same direction, Also can't decompose landing, also must look for other means of transportation to disperse again after landing in an area. Contents of the invention [0003] In order to solve the shortcomings that the aircraft cannot be combined and disassembled during flight, the invention provides a combined and disassembled aircraft. The sub-machines of the aircraft can not only be combined with the main machine to load passengers and cargo, but also can be disass...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D5/00
Inventor 李沛霖张柯鑫
Owner 李沛霖
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