UNMANNED AIRCRAFT AND CONTROL METHOD THEREOF

Title:

UNMANNED AIRCRAFT AND CONTROL METHOD THEREOF

Document Type and Number:

Japanese Patent JP2022150020

Kind Code:

A

Abstract:

To provide an unmanned aircraft which is easily downsized and has high flight performance.SOLUTION: An unmanned aircraft having a kite wing 2 attached at a predetermined angle relative to an aircraft body 1 comprises: front edge pipes 23, 24 that are arranged in bilateral symmetry and turnably provided about a front side portion, relative to an airframe main shaft 10 of the kite wing 2; and propellers 121, 122, 131, 132 disposed on the airframe body 1. The kite wing 2 is flexible and supported by the front edge pipes 23, 24, and opened and closed according to turning of the front edge pipes 23, 24. At least one propeller is arranged to be positioned inside the kite wing 2, in plan view of the kite wing 2 in a fully open state.SELECTED DRAWING: Figure 2

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Inventors:

NONAMI KENZO
SUZUKI SATOSHI
MIYAKE NORIHISA

Application Number:

JP2021052412A

Publication Date:

October 07, 2022

Filing Date:

March 25, 2021

Export Citation:

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Assignee:

ADVANCED ROBOTICS FOUND

International Classes:

B64C27/26; B64C27/08; B64C31/032; B64C39/02

Attorney, Agent or Firm:

Atsushi Ito

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