Hypothetical family of "giant" helicopters in which certain design and operational trends are taken to their logical conclusions; achievement may be within reach in near future; three problems facing designer of large helicopter are control of transmission weight, control of blade weight, and achievement of acceptable fuel consumption; turbojet engines offer effective solution. From Helicopter Assn Great Britain -- J v 5 n 4. (See also Flight v 60 n 2236, 2237 Nov 30 1951 p 672-4, Dec 7 p 728-31; Am Helicopter v 26 n 5, 6 Apr 1952 p 6-9, 13, May p 8-12, 14)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Giant helicopter


    Weitere Titelangaben:

    Aeroplane


    Beteiligte:

    Erschienen in:

    Aeroplane ; 81 , n 2106


    Erscheinungsdatum :

    1951


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Giant helicopter

    Fitzwilliams, O.L.L. | Engineering Index Backfile | 1952


    Giant helicopter

    Fitzwilliams, O.L.L. | Engineering Index Backfile | 1951




    Helicopter rotor head, multirotor helicopter, and helicopter

    UEBORI TAKAKAZU / SUZUKI SHUNICHI | Europäisches Patentamt | 2020

    Freier Zugriff