Octahedral aircraft

An aircraft and octahedron technology, applied in the field of aircraft, can solve problems such as propeller damage, aircraft crash, and easy collision with the outside world, and achieve the effects of low aerodynamic noise, good use safety, and strong replaceability

Pending Publication Date: 2017-07-07
SHENYANG INST OF AUTOMATION - CHINESE ACAD OF SCI
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Most of these existing aircraft propellers are exposed outside the fuselage, which is easy to co

Method used

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Examples

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Example Embodiment

[0028] The present invention will be described in further detail below in conjunction with the accompanying drawings.

[0029] like Figures 1 to 3 As shown, the present invention includes an upper casing 1, a camera module 2, a switch 3, a balance weight assembly 4, a circuit support frame upper cover 5, a main circuit board 9, a circuit support frame 11, a ducted fan module assembly 12, a middle casing Body 15, battery 16 and lower casing 17, wherein the upper casing 1, the middle casing 15 and the lower casing 17 are connected in sequence to form an octahedral cavity, and the connection between the upper casing 1 and the middle casing 15 and the middle casing The connection between the shell 15 and the lower shell 17 adopts the cooperation of grooves and bosses. The holes provided around the upper and lower ends of the middle shell 15 are equipped with wire screw sleeves. Screws connect the upper casing 1 , the middle casing 15 and the lower casing 17 together. The balance w

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PUM

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Abstract

The invention relates to aircrafts, in particular to an octahedral aircraft. The octahedral aircraft comprises an upper shell body, a middle shell body, a lower shell body, counterweight assemblies, a circuit supporting frame upper cover, a main circuit board, a circuit supporting frame, ducted fan assemblies and a battery, wherein the upper shell body, the middle shell body and the lower shell body are sequentially connected to form an octahedral cavity; and the counterweight assemblies, the circuit supporting frame upper cover, the main circuit board, the circuit supporting frame, the ducted fan assemblies and the battery are contained in the octahedral cavity. The upper shell body and the lower shell body are each provided with at least one ducted fan assembly. The circuit supporting frame is installed on the middle shell body and contains the main circuit board installed on the middle shell body. The circuit supporting frame upper cover is arranged at the top of the circuit supporting frame. The multiple counterweight assemblies are uniformly distributed on the circuit supporting frame upper cover. The ducted fan assemblies installed on the middle shell body are arranged on the periphery of the circuit supporting frame in the front, back, left and right directions. The battery is installed on the middle shell body and connected with the main circuit board. All the ducted fan assemblies are connected with the main circuit board. The upper shell body is provided with a switch connected with the main circuit board. The octahedral aircraft is novel in structure, flexible in control and suitable for the flight monitoring service in a space station cabin.

Description

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Claims

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Application Information

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Owner SHENYANG INST OF AUTOMATION - CHINESE ACAD OF SCI
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