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Combined flight vehicle generating greater lift force

A combined aircraft and lift technology, applied in the aviation field, can solve problems such as difficulty in development, and achieve the effects of easy production, easy mass production, and increased positive pressure power.

Active Publication Date: 2014-02-26
朱晓义
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

It is necessary to find a greater source of lift and to completely change the structure of traditional aircraft, otherwise it will be difficult to achieve further development

Method used

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  • Combined flight vehicle generating greater lift force
  • Combined flight vehicle generating greater lift force
  • Combined flight vehicle generating greater lift force

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Embodiment Construction

[0027] In order to describe the technical content, structural features, achieved goals and effects of the present invention in detail, the following will be described in detail in conjunction with the embodiments and accompanying drawings.

[0028] First summarize the technical scheme of the present invention as a whole:

[0029] 1. The aircraft of Embodiments 1 to 7 has a plurality of inlets on the shell and communicates with the fluid passages. Under the action of the huge suction of the engine, the high-speed fluid in the fluid passages passes around each carrying cabin, so that each carrying cabin Generate lift and extend to the aircraft shell connected with it to form a high-speed fluid layer located in the upper half of the aircraft and a low-speed fluid layer located in the lower half. The difference in flow velocity between the fluid layers produces greater lift.

[0030] 2. The eighth embodiment is that a plurality of carrying compartments are combined into an aircraf...

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Abstract

The invention discloses a combined flight vehicle generating greater lift force. The combined flight vehicle comprises a shell body and an engine, the surface of the shell body is provided with a plurality of importing ports for importing airflow, the shell body is internally provided with a fluid channel communicated with the outside through the importing ports, and the interior of the shell body is separated into at least two independent carrying capsules by the fluid channel; an air suction port of the engine is communicated with the importing ports through the fluid channel, and an exhaust port of the engine is communicated with the outside. The combined flight vehicle has the beneficial effects that a suction force of the engine allows a high-speed flowing fluid in the fluid channel to pass around the periphery of each carrying capsule at a high speed and be communicated with the upper half part shell body of the plane for together forming a high-speed fluid layer, and a pressure difference is produced between the high-speed flowing fluid and the low-flow-speed fluid in the lower half part shell body and in a natural state, so that lift force is produced in each carrying capsule, and thus the lift force is produced in the flight vehicle.

Description

technical field [0001] The invention relates to the field of aviation, in particular to a combined aircraft generating greater lift. Background technique [0002] Now some fixed-wing aircraft, such as passenger planes, transport planes, bombers, fighter jets, unmanned aerial vehicles, etc., because the fuselage is a closed whole, and the path length between the arc surface and the plane of the upper and lower surfaces of the wing is not much different, so the The traditional aircraft structure with wings as the only source of lift and a closed fuselage has hardly changed in more than a hundred years, and has become a shackle for the development of the aviation industry. It is necessary to find a greater source of lift and to completely change the structure of traditional aircraft, otherwise it will be difficult to obtain further development. [0003] The inventor has obtained more than ten invention patents in this field, among which the Chinese invention patent No. 2011100...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C39/00B64C3/14
Inventor 朱晓义
Owner 朱晓义
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