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Multi-rotor craft capable of transforming combination

A multi-rotor aircraft and flight control module technology, applied in the field of aircraft, can solve the problems of inconvenient carrying, single load, and inflexible combination of multi-rotor aircraft

Active Publication Date: 2016-02-24
GUANGZHOU INST OF GEOGRAPHY GUANGDONG ACAD OF SCI
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The purpose of the present invention is to provide a deformable combined multi-rotor aircraft, which aims to solve the problems that the existing multi-rotor aircraft combination is not flexible enough, inconvenient to carry, single load, and unable to meet the needs of different occasions

Method used

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  • Multi-rotor craft capable of transforming combination
  • Multi-rotor craft capable of transforming combination
  • Multi-rotor craft capable of transforming combination

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Embodiment Construction

[0024] In order to make the object, technical solution and advantages of the present invention more clear, the present invention will be further described in detail below in conjunction with the examples. It should be understood that the specific embodiments described here are only used to explain the present invention, not to limit the present invention.

[0025] The application principle of the present invention will be further described below in conjunction with the accompanying drawings.

[0026] see Figure 1-Figure 7 :

[0027] Two or three arms are installed on the fuselage of a deformable combined multi-rotor aircraft according to an embodiment of the present invention, specifically including an electronic governor 1, a motor 2, a propeller 3, a GPS antenna 4, and a flight control module 5. Wireless image transmission module 6, wireless digital transmission module 7, remote control receiving module 8, remote control, polymer lithium battery mount 9, sensor mount 10, ...

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Abstract

The invention discloses a multi-rotor craft capable of transforming combination. Two arms or three arms are installed on a machine body. The arms are connected with the machine body through screws. An electronic speed regulator is installed on each arm. Motors are installed at two ends of each arm. The motor is loaded with a propeller. A flight control module, a wireless image transmission module, a wireless digital transmission module and a remote control reception module are installed at the upper part of the central position of the machine body. A sensor is mounted at the bottom of the central position of the machine body. An undercarriage is installed at two sides of the bottom of the machine body. A polymer lithium battery is mounted on the undercarriage. The multi-rotor craft can be transformed into a four-rotor or a six-rotor structure to meet requirements of different situations. The four-rotor structure meets the small-load requirement and is light and flexible. The six-rotor structure is stable, achieves large load and can be loaded with single-lens reflex cameras and heavy sensors.

Description

technical field [0001] The invention belongs to the field of aircraft, in particular to a deformable combined multi-rotor aircraft. Background technique [0002] The four-rotor aircraft can meet the requirements of small loads, and is characterized by lightness and flexibility; the six-rotor aircraft is characterized by stability, large loads, and can be equipped with SLR and heavy sensors; [0003] The existing combination of multi-rotor aircraft is not flexible enough, it is inconvenient to carry, and the load is single, which cannot meet the needs of different occasions. Contents of the invention [0004] The purpose of the present invention is to provide a deformable combined multi-rotor aircraft, which aims to solve the problems that the existing multi-rotor aircrafts are not flexible enough to be combined, inconvenient to carry, have a single load, and cannot meet the needs of different occasions. [0005] The present invention is achieved in this way. Two or three ...

Claims

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Application Information

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IPC IPC(8): B64C27/08B64C27/32
CPCB64C27/08B64C27/32
Inventor 唐光良黄光庆林志文
Owner GUANGZHOU INST OF GEOGRAPHY GUANGDONG ACAD OF SCI
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