Reliable heavy-life helicopter with economical range and pay-load can be constructed with current technology and manufacturing facilities; influence of vehicle size on its power plant, and integrated trends of power plant, transmission system, and rotor system are used to show interplay of benefits, and penalties as aircraft size increases; operational and human factors aspects of use of large rotors are discussed to show how they influence application of large helicopters for military and civilian uses; findings of 20-ton-payload study are extrapolated to predict 50-ton vehicle possessing several important design features still in conceptual or development stages.


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    Titel :

    Large crane helicopter


    Weitere Titelangaben:

    ASME -- Paper


    Beteiligte:

    Kongress:

    ASME Meeting Tran-5 ; 1967 Cranes



    Erscheinungsdatum :

    1967


    Format / Umfang :

    13 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Sikorsky crane helicopter

    Michel, P.L. | Engineering Index Backfile | 1962


    Twin-engine helicopter crane

    Coleman, F. | Engineering Index Backfile | 1958


    Hot cycle flying crane helicopter

    Nay, H.O. / Sullivan, R.J. | Engineering Index Backfile | 1963


    Igor Sikorsky Defines the Crane Helicopter

    McKenna, John A. | AIAA | 2010


    Comparison Between Helicopter and Cable Crane in Logging Operation

    M. Manzone / P. Balsari | DOAJ | 2017

    Freier Zugriff