To provide a miniaturized rotorcraft capable of maintaining or improving the estimation accuracy of the altitude of the rotorcraft.SOLUTION: The rotorcraft according to the present disclosure comprises a body part forming an airframe of the rotorcraft, a rotor supported by the body part, an atmospheric pressure sensor supported by part of the body part and comprising air-introducing holes, and a long hollow member in which an opening at one end is connected to the air-introducing holes and an opening at the other end is open.SELECTED DRAWING: Figure 1

    【課題】小型化された回転翼機の高度の推定精度を維持または向上させることが可能な回転翼機を提供すること。【解決手段】本開示に係る回転翼機は、前記回転翼機の機体を構成する本体部と、前記本体部に支持される回転翼と、前記本体部の一部に支持され、大気導入孔を備える気圧センサと、長尺状の中空部材であって、一端の開口部が前記大気導入孔と接続され、他端の開口部が開放された中空部材と、を備える。【選択図】 図1


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    Titel :

    ROTORCRAFT


    Weitere Titelangaben:

    回転翼機


    Beteiligte:
    TAKAHASHI EIJI (Autor:in)

    Erscheinungsdatum :

    15.04.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Japanisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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