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Design scheme of framework structure

A design scheme and frame structure technology, applied to fuselage frames, aircraft, vertical take-off and landing aircraft, etc., can solve the problems of vertical take-off and landing performance that are difficult to integrate, and achieve the effect of improving maneuverability and good aerodynamic layout

Inactive Publication Date: 2015-01-14
鲍小福
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] At present, most of the fixed-wing aircraft in the prior art adopt a bird-shaped fuselage design, which is difficult to integrate in terms of vertical take-off and landing performance. Although some aircraft can perform vertical take-off and vertical landing operations, their aerodynamic layout To be further improved

Method used

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example 1

[0018] Example 1: If figure 1 , figure 2 , image 3 , Figure 4 As shown, a shell / body 1 is characterized in that: inside the shell / body 1, on the basis of the center point / line, there are longitudinal pipes 2 and horizontal pipes 3 perpendicular to each other. It communicates with the outer space of the body 1, and the two ends of the longitudinal 2 and transverse 3 pipes perpendicular to each other are connected to form a body by the body tube 4. On the body 4, the center of the body 1 is taken as a point, There are vertical pipes 5 symmetrically arranged, and the nozzles at both ends of the vertical pipes 5 communicate with the outer space of the body 1, and inside the body 1, with the center as the point, there are vertical pipes 6 symmetrically arranged , the lower end nozzle of the vertical pipe 6 communicates with the external space of the body 1, the upper end of the pipe 6 is provided with a pipe plug 61, and the shell / body 1 is provided with various openings 7, r...

example 2

[0026] Example 2: This example is the control of the aircraft. The vertical pipe 2 and the horizontal pipe 3 are vertically connected to each other and the ten / field-shaped pipe is the direction sense of front, rear, left and right. The operating table in the operating room, program operation; start; all the electric propellers / fans on the vertical pipe 2, horizontal pipe 3, and vertical pipe 5 start to run at low speed, and the self-check system shows that everything is normal. The program operation enters into the suspension stop program; the information processor automatically handles the rotation of all electric propellers / fans at the lower end of the vertical pipe 5, and automatically adjusts the speed of the electric propeller fan at the upper end of the vertical pipe 5 to maintain the hovering balance of the aircraft. The piston element / vertical landing frame retracted in the device body 1 in the vertical pipeline 6 li is operated. After the aircraft is suspended in the...

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Abstract

The invention discloses a design scheme of a framework structure. The design scheme can be applied to an aircraft, and the aircraft can take off and land vertically and can move front and back as well as left and right like a cross; the operability of the aircraft is improved. The aircraft can take a flying saucer shape, a cuboid shape, a streamline shape, a cone shape, a shuttle shape, a pipe shape and the like and is good in pneumatic arrangement; by the adoption of full-motor operation, the aircraft can fly in the air and sail and sink in the sea; furthermore, emission of waste gas to an atmosphere and an ocean environment is reduced, so that the framework structure has environment-friendly and pollution-free effects and can be applied to civil use and military use.

Description

Technical field: [0001] The invention relates to frame structure design technology. Background technique: [0002] At present, most of the fixed-wing aircraft in the prior art adopt a bird-shaped fuselage design, which is difficult to integrate in terms of vertical take-off and landing performance. Although some aircraft can perform vertical take-off and vertical landing operations, their aerodynamic layout There is room for further improvement. Invention content: [0003] The technical problem to be solved by the present invention is to provide a frame structure design scheme with more reasonable structural strength and aerodynamics in view of the above-mentioned existing technical status of aircraft. [0004] The technical solution adopted by the present invention to solve the technical problem of the above-mentioned frame structure is: a shell / body, the inside of which is connected together by stacked pipes, including ribs and bulkhead panels, characterized in that the...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C29/00B64C1/06
Inventor 鲍小福
Owner 鲍小福
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