PROBLEM TO BE SOLVED: To provide an improved spacer tube for a power transmission device of a rotary wing aircraft.SOLUTION: A spacer tube 1 for a power transmission device of a rotary wing aircraft includes a plurality of mutually-connected linear truncated cone ring parts 2 which each have a meandering cross-sectional shape and which each have a base bottom area 3 and a top part area 4.SELECTED DRAWING: Figure 1

    【課題】回転翼航空機の動力伝達装置のための、改良されたスペーサチューブを提供する。【解決手段】回転翼航空機の動力伝達装置のためのスペーサチューブ1に関し、スペーサチューブ1は、蛇行する断面形状を備え、及び、基底領域3及び頂部領域4を有する、複数の互いに接続された直線の円錐台リング部分2から構成されている。【選択図】図1


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    SPACER TUBE FOR POWER TRANSMISSION DEVICE OF ROTARY WING AIRCRAFT


    Weitere Titelangaben:

    回転翼航空機の動力伝達装置のためのスペーサチューブ


    Beteiligte:
    MICHAEL PLATZER (Autor:in) / MARTIN MEUNIER (Autor:in) / MARTIN KUEHNE (Autor:in)

    Erscheinungsdatum :

    2016-04-04


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Japanisch


    Klassifikation :

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



    ELECTROMAGNETIC POWER TRANSMISSION FOR A ROTARY-WING AIRCRAFT OR A FIXED-WING AIRCRAFT

    CHANTRIAUX ERIC / CHRETIEN PASCAL | Europäisches Patentamt | 2019

    Freier Zugriff

    Electromagnetic power transmission for a rotary-wing aircraft or a fixed-wing aircraft

    CHANTRIAUX ERIC / CHRETIEN PASCAL | Europäisches Patentamt | 2017

    Freier Zugriff

    HYBRID POWER ROTARY WING AIRCRAFT

    LUYKS LEO J | Europäisches Patentamt | 2016

    Freier Zugriff


    Hybrid power rotary wing aircraft

    LUYKS LEO J | Europäisches Patentamt | 2016

    Freier Zugriff