Aircraft and control method of aircraft

专利名称：Aircraft and control method of aircraft发明人：鈴木 陽一申请号：JP2019107576申请日：20190610公开号：JP2019167104A公开日：20191003

专利附图：

摘要：In a rotary wing machine having a plurality of motors, a load is concentrated ona specific motor when a straight running posture is frequently used. The rotary wingmachine includes a propeller, a motor that rotates the propeller, an arm portion thatsupports the motor, and a detection unit that detects at least the state of the motor,

and according to a forward operation from an operator. A control method of a rotarywing machine that displays at least a front or rear direction indication display in the firsthorizontal direction in a first pattern, based on the state detected by the detection unit,from the operator The moving direction of the rotary wing machine according to theforward operation is changed to a second horizontal direction different from the firsthorizontal direction, and at least the front or rear direction indication display in thesecond horizontal direction is displayed in a second pattern. And control the rotorcraft.[Selection] Figure 1

申请人：株式会社エアロネクスト,株式会社ＤＲＯＮＥ ｉＰＬＡＢ

地址：東京都渋谷区恵比寿西二丁目３番５号,東京都渋谷区恵比寿西二丁目３番５号

国籍：JP,JP

代理人：特許業務法人 ｉＰＬＡＢ Ｓｔａｒｔｕｐｓ

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