Carbon fiber multi-rotor unmanned aircraft fuselage and method for manufacturing the same

A technology of a multi-rotor unmanned aerial vehicle and a manufacturing method, applied in the field of unmanned aerial vehicles, can solve the problems of complex structure, inconvenient use and high cost, and achieve the effects of smooth operation, reduced use cost and reduced energy consumption

Active Publication Date: 2015-04-08
常州神鹰碳塑复合材料有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0007] The purpose of the present invention is to overcome the disadvantages of complex structure, heavy weight, inconvenient use and high cost of the UAV fuselage in the prior art, and provide a carbon fiber multi-rotor UAV fuselage and manufacturin...

Method used

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  • Carbon fiber multi-rotor unmanned aircraft fuselage and method for manufacturing the same
  • Carbon fiber multi-rotor unmanned aircraft fuselage and method for manufacturing the same
  • Carbon fiber multi-rotor unmanned aircraft fuselage and method for manufacturing the same

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Embodiment

[0042] Such as figure 1 , figure 2 and image 3 As shown, a kind of carbon fiber multi-rotor unmanned aerial vehicle fuselage of the present embodiment comprises central compartment, rotor arm 3 and motor compartment 4, and central compartment comprises central compartment upper cover 1 and central compartment cabin body 2 that are fixed together, The central cabin upper cover 1 and the central cabin body 2 are fixedly connected by bolts 8, specifically, as Figure 6 and Figure 7 As shown, the bolt 8 is a special bolt, one end is processed with an external thread, and the other end is processed with an internal thread. When connecting, one end with an external thread passes through the threaded hole on the central cabin upper cover 1 and the central cabin body 2 to secure the two together; the end with an internal thread passes through the bottom of the central cabin body 2 screw thread connection. In the present embodiment, the middle part of the central cabin body 2 i...

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Abstract

The invention discloses a carbon fiber multi-rotor unmanned aircraft fuselage and a method for manufacturing the same, and belongs to the technical field of unmanned aircraft devices. The fuselage comprises a center compartment, rotor arms and a motor compartment, wherein the center compartment comprises a center compartment upper cover and a center compartment body which are fixedly connected, a device plate is fixed in the middle of the center compartment body, one end of each rotor arm is connected with the motor compartment, the other end of the rotor arm extends between the device plate and a bottom plate in the center compartment body, and the ends of the rotor arms are connected with the device plate and the bottom plate by connection pieces. The structure of the fuselage is simple, the design scheme is reasonable and smart, the least manufacturing raw materials are used to ensure lightest quality of the fuselage, and enough structure strength and good using performance of the fuselage can be guaranteed.

Description

technical field [0001] The invention relates to an unmanned aerial vehicle, more specifically, to a carbon fiber multi-rotor unmanned aerial vehicle body and a manufacturing method. Background technique [0002] In the operation of transmission lines, it is often necessary to quickly find and confirm fault points and dangerous points within several spans. However, in the case of undulating terrain or vertical and horizontal river ditches, using existing inspection methods not only has high work intensity, but also low work efficiency, and may even cause delays in inspection time and inaccurate results. Therefore, it is possible to quickly, simply and accurately find fault points and dangerous points; it can realize multi-angle and all-round observation, troubleshoot hidden or potential defect faults, and timely grasp the operation status of transmission line equipment. An important issue facing the department. [0003] Condor series products are new unmanned aerial vehicle...

Claims

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Application Information

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IPC IPC(8): B64C1/00B64C27/08
Inventor 唐许施刘生王明珠王宏亮许太尚
Owner 常州神鹰碳塑复合材料有限公司
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