Module combined type manufacturing method for four-axis aircraft and four-axis aircraft

A four-axis aircraft, combined technology, applied in the direction of aircraft, aircraft parts, rotorcraft, etc., can solve the problems of easy connection, increase of overall weight, complicated disassembly and assembly, etc., so that it is easy to avoid problems and increase the overall weight , the effect of high overall strength

Active Publication Date: 2015-12-16
广东凯登智能科技有限公司
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, due to the high cost of manufacturing, use, and maintenance, it has not yet been widely popularized.
[0003] Because of the complex structure and tight connection of each part of the traditional aircraft, they are all integrated, and basically cannot be disassembled after assembly
This traditional one-piece aircraft, once any parts are damaged, will lead to the overall scrapping, even if it is sent for repair, it is difficult to disassemble and repair
[0004] Or, after a long period of use, some parts of...

Method used

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  • Module combined type manufacturing method for four-axis aircraft and four-axis aircraft
  • Module combined type manufacturing method for four-axis aircraft and four-axis aircraft
  • Module combined type manufacturing method for four-axis aircraft and four-axis aircraft

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Embodiment Construction

[0045] see Figures 1 to 15 , the modular combined manufacturing method of quadcopter provided by the present invention, comprises the following steps:

[0046] 1) Install a battery module 1, which is in the shape of a cuboid, with a first contact female socket 11 at the rear and a first buckle 12 at the bottom;

[0047] 2) Install a camera module 2, which is in the shape of a cuboid, with a camera 23 at the front, a second contact female socket 21 at the rear, and a second buckle 22 at the bottom;

[0048] 3) Install the height-fixing and infrared anti-collision module 3, and the bottom of the height-fixing and infrared anti-collision module 3 is provided with a third buckle 32 and a third contact female socket 31;

[0049] 4) Set the aircraft frame module 4, the four-axis aircraft frame module 4 includes a main body 41, an X-shaped flight shaft 42 protruding from the main body 41, and four X-shaped flight shafts respectively The propeller power group 43 at the end; the mai...

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Abstract

The invention discloses a module combined type manufacturing method for a four-axis aircraft. The module combined type manufacturing method includes the following steps: (1) a battery module is arranged and is in a cuboid shape, a first contact type female socket is arranged at the back position, and a first buckle is arranged at the bottom; (2) a camera shooting module is arranged and is in a cuboid shape, a camera is arranged on the front portion, a second contact type female socket is arranged at the back position, and a second buckle is arranged at the bottom; (3) a height determining and infrared anti-collision module is arranged, and a third buckle and a third contact type female socket are arranged at the bottom of the height determining and infrared anti-collision module; (4) an aircraft rack module is arranged, and the four-axis aircraft rack module comprises a body part, a flight shaft outwards extending from the body part and propeller power sets arranged at the four ends of the X-shaped flight shaft respectively; and (5) all the modules are assembled in a combined manner through detachable plug-in or buckling mechanisms. The invention further discloses the module combined type four-axis aircraft for implementing the method.

Description

technical field [0001] The invention relates to the structure of an aircraft, in particular to a modular combined manufacturing method of a four-axis aircraft and the four-axis aircraft. Background technique [0002] With the development of remote-controlled unmanned aerial vehicle technology, a large number of various aircraft technologies have emerged, and their applications are becoming more and more extensive. However, due to reasons such as high manufacturing, use, and maintenance costs, it has not yet been widely popularized. [0003] Because of the complex structure and tight connection of various parts of traditional aircraft, they are all integrated, and basically cannot be disassembled after assembly. Once this traditional integrated aircraft is damaged, it will be scrapped as a whole. Even if it is sent for repair, it is difficult to disassemble and repair. [0004] Or, after a long period of use, some parts of the aircraft need to be replaced. Due to the compli...

Claims

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Application Information

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IPC IPC(8): B64C27/08B64C1/00B64D47/08B64D47/00B64D27/24
Inventor 蔡强
Owner 广东凯登智能科技有限公司
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