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Modularization fast-disassembly type unmanned helicopter

An unmanned helicopter and quick-release technology, applied in the field of unmanned aerial vehicles, can solve the problems of hindering use and maintenance costs, occupying a large space, and scrapping the whole machine, so as to reduce maintenance costs and maintenance difficulties, improve work efficiency and save money. cost effect

Pending Publication Date: 2018-05-04
柚子航空智能科技(南京)有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, at present, most unmanned helicopters adopt an integrated design, often due to the failure of individual working parts, the whole machine cannot take off to perform tasks or even be scrapped, which brings great difficulties to maintenance and fault diagnosis. and maintenance costs also pose considerable obstacles
In addition, unmanned helicopters are generally an integral structure, and the main components are fixedly connected, which takes up a lot of space during packaging, transportation and storage, and is easily damaged

Method used

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  • Modularization fast-disassembly type unmanned helicopter
  • Modularization fast-disassembly type unmanned helicopter
  • Modularization fast-disassembly type unmanned helicopter

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Embodiment Construction

[0022] The preferred embodiments of the present invention will be described in detail below in conjunction with the accompanying drawings, so that the advantages and features of the present invention can be more easily understood by those skilled in the art, so as to define the protection scope of the present invention more clearly.

[0023] see Figure 1-4 , a modular quick-detachable unmanned helicopter, including a fuselage module 1, a landing gear module 2, a tail drive module 3 and a connecting mechanism 4; The main rotor 12 at the top and the engine 13, main transmission 14, and fuel tank 15 arranged in the fuselage shell 11; the landing gear module 2 includes a skid 21 and a support leg 22 connected thereto; the tail transmission module 3 includes the tail shell 31. The intermediate transmission 32, the rudder gear 33, the tail transmission 34 arranged in the tail housing 31, the tail rotor 35 arranged at the outer end of the tail housing 31, the fuselage module 1, the ...

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Abstract

The invention provides a modularization fast-disassembly type unmanned helicopter, which comprises a fuselage module, an undercarriage module, a tail transmission module and a connecting mechanism. The fuselage module comprises a fuselage shell, a main rotor, an engine, a main transmission and an oil tank; the undercarriage module comprises a slide and supporting legs; the tail transmission modulecomprises a tail shell, a middle transmission, a direction steering engine, a tail transmission and a tail rotor; the fuselage module, the undercarriage module and the tail transmission module are connected through the connecting mechanism; the connecting mechanism comprises a fuselage side plate, a tail side plate, a fast-assembly pin and a fast-assembly lock; the fuselage module is connected with the undercarriage module through the fast-assembly pin; the fuselage module is connected with the tail transmission module through the fast-assembly lock. According to the modularization fast-disassembly type unmanned helicopter provided by the invention, the functional structures are modularly decomposed and adopt standardized module connecting interfaces, so that the maintenance cost and theoverhaul difficulty for the use of the unmanned helicopter are reduced, the modules are broken into parts so as to be convenient to package, transport and store, the installation can be carried out conveniently, the working efficiency is improved, and the cost is reduced.

Description

technical field [0001] The invention relates to the field of unmanned aerial vehicles, in particular to a modular quick-release unmanned helicopter. Background technique [0002] Unmanned helicopter refers to an unmanned aircraft that can take off and land vertically by radio ground remote control flight or / and autonomous control flight. Unmanned helicopters have the characteristics of no casualties, small size, low cost, vertical take-off and landing, hovering in the air, small take-off and landing sites, and no need to be equipped with complex and large-volume launch and recovery systems. Therefore, they have both military and civilian applications. Wide range of applications. However, at present, most unmanned helicopters adopt an integrated design, often due to the failure of individual working parts, the whole machine cannot take off to perform tasks or even be scrapped, which brings great difficulties to maintenance and fault diagnosis, and at the same time reduces th...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C27/06B64C1/00
CPCB64C27/06B64C1/069
Inventor 汤兴华李超
Owner 柚子航空智能科技(南京)有限公司
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