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Modularized compound multi-rotor hybrid power aircraft

An aircraft and composite technology, applied in the field of modular composite multi-rotor hybrid aircraft, can solve the problem that fixed-wing aircraft cannot take off and land vertically during flight time

Inactive Publication Date: 2016-10-05
范磊
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The present invention combines the flight advantages of the multi-rotor aircraft with the advantages of the fixed-wing aircraft due to the realization of the compound flight mode, and overcomes the problems of multi-rotor aircraft's flight time, load, flight speed and fixed-wing aircraft's inability to take off and land vertically.

Method used

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  • Modularized compound multi-rotor hybrid power aircraft
  • Modularized compound multi-rotor hybrid power aircraft
  • Modularized compound multi-rotor hybrid power aircraft

Examples

Experimental program
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Embodiment Construction

[0042] Lift module assembly: The lift module is composed of core modules, groups (see figure 1 ) assembled. After the folding connecting pipe module 7 is packed into the equidistant two ends of the upper hole of the side frame module 5, fasten with the fastener module 13, and the folding module 6 is installed at the two ends, and the rotating module 6 is installed at the other end of the folding module 6. The arm tube module 8, the rotor mounting frame module 4 is respectively installed at the two ends of the rotary arm tube module 8, the rotor module 1 is respectively installed at the upper end of the rotor mounting frame module 4, and the reinforced positioning tube module 9 is respectively inserted into the rotor mounting frame from both ends The module 4 and the connecting frame module 5 are fastened through the lower holes to form a single-rotor lift module 14 . See figure 2 Install two rotor modules 1 at the bottom of the two rotor mounting frame modules 4 of the sing...

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Abstract

The invention relates to a modularized serial manufacturing method for a multi-rotor aircraft and a compound multi-rotor hybrid power aircraft. According to the invention, the multi-rotor aircraft is rapidly assembled from core modules and module groups; and composite power units are additionally installed so as to assemble compound multi-rotor hybrid power aircraft module groups. The aircraft module groups can independently fly as independent aircrafts and can be assembled in parallel into larger aircrafts with different types.

Description

technical field [0001] The invention relates to a method for modularly assembling a multi-rotor aircraft and a composite multi-rotor hybrid aircraft. The core module and module are used to quickly assemble the multi-rotor aircraft, and the composite multi-rotor hybrid aircraft module is assembled by adding a compound power device. These aircraft modules are not only independent aircraft that can fly independently, but also aircraft modules that are assembled in parallel with larger aircraft of different types. Background technique [0002] Aircraft have been invented for more than 100 years and have greatly facilitated human transportation. From the flight mode, it can be divided into: helicopters, fixed-wing aircraft, autogyro aircraft, and composite aircraft. A composite aircraft that can take off and land vertically like a helicopter and fly at high speed and efficiently like an airplane has been the focus of aviation research for a long time. There are different types...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C27/08B64C27/10B64C27/22B64D27/02
Inventor 范磊
Owner 范磊