To provide a rotary wing flight body capable of solving increase of a self weight overhead due to a drive source provided on each rotary wing, in a rotary wing flight body such as a drone or the like, eliminating non-efficiency of individually designing and producing each size and shape of a rotary wing flight body for coupling and combining respective elements as components for constructing a rotary wing flight body with a target performance.SOLUTION: A rotary wing flight body is configured so that, a rotary wing part 150 for generating lift and driving force and a drive part having a rotary engine which is a drive source of the rotary wing part are modularized, for coupling and combining respective elements in a semi custom manner, according to a target specification request.SELECTED DRAWING: Figure 6
【課題】ドローン等の回転翼飛行体に於いて、回転翼毎に駆動源を有する事による自重オーバーヘッドの増大を解消する。更に多彩なサイズ、形状の回転翼飛行体を個別に設計製造する非効率を排して、部品としての各要素を、結合し組み合わせして目的性能の回転翼飛行体を構築する。【解決手段】揚力、推進力を発生させる回転翼部150と、この駆動源である回転エンジンを有する駆動部をそれぞれモジュール化し、目的仕様要求に応じてセミカスタム的に結合し組み立る。【選択図】図6
ROTARY WING FLIGHT BODY FOR EVERY MODULE
モジュール別回転翼飛行体
2020-09-17
Patent
Electronic Resource
Japanese
IPC: | B64C AEROPLANES , Flugzeuge |
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