Approach taken by Westland Aircraft Ltd to prevent many defects persisting through development period and causing unreliability in service; summary of Wessex Mk. 1 helicopter development program with regard to transmission, controls, rotors and mechanisms, and complete aircraft shows importance of development testing; growth of overhaul period begins with experience accumulated by strip examination of number of components on completion of initial overhaul period; average achieved life and mean time between failures; establishment of failure probability requirement.


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    Titel :

    Engineering reliability of shaft-driven helicopters


    Weitere Titelangaben:

    Roy Aeronautical Soc -- J


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    1963


    Format / Umfang :

    14 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Shaft Gas Turbines For Helicopters

    Krebs, R. P. / Blaschke, T. C. / Miller, W. S. | SAE Technical Papers | 1956


    Matching the Characteristics of Helicopters and Shaft-Turbines

    Meyers, D.N. / Ciolkosz, Z.M. | SAE Technical Papers | 1954


    CHARACTERISTICS OF THE TWO-SHAFT GAS TURBINE IN HELICOPTERS

    ANDERSON, WILLIAM B. | SAE Technical Papers | 1953


    Helicopters in civil engineering

    Hammond, R. | Engineering Index Backfile | 1957


    Research requirements to improve reliability of civil helicopters

    Dougherty, J. J., III / Barrett, L. D. | NTRS | 1978