Aircraft takeoff

专利名称：Aircraft takeoff

发明人：ペイジ，マーク，アラン,マッキー，マシュー，ロ

バート,ゴッドラスキー，ロバート，アンソニー

申请号：JP2020501421申请日：20180321公开号：JP2020511365A公开日：20200416

专利附图：

摘要：Aircraft used in fixed airflow flight and rotary wing flight modes are providedwhile retaining the horizontal fuselage.The aircraft may include fuselage, wings, rotorsand multiple engines.The rotor may have a wing attachment assembly further comprisinga rotary support.The rotary portion can have a central support portion and a wing, and aplurality of engines are attached to the rotary portion.In a rotating wing flight mode, therotating portion can rotate around the longitudinal axis of the rotor providing lift for theaircraft, as well as the rotor of the helicopter.In the fixed wing flight mode, the rotaryportion does not rotate around the vertical axis of the rotor, and applies the lift to the

aircraft similarly to the conventional aircraft.The same engine as supplying torque topower the rotor in a rotating wing flight mode also provides power to the aircraft in afixed wing flight mode.

申请人：デザイン テクノロジーズ インコーポレイテッド

地址：アメリカ合衆国 カリフォルニア州 ９２６１８，アーヴァイン，ヴァンダービルト １１

国籍：US

代理人：伊東 忠重,伊東 忠彦,大貫 進介

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