The paper presents a methodology of forming a system of geometric constraints in helicopter design. The methodology is based on the synthesis of the requirements in terms of ensuring operation on marine vessels, transportability, and capacity of the cargo (transport) cabin of the helicopter. The universality of this approach allows to adapt the formed system of geometrical constraints to helicopters of different purposes, both to newly developed and modernised helicopters. This methodology allows to define general geometrical characteristics of the helicopter, nomenclature of units requiring simplification of mounting and dismounting procedure of separate units and reduction of their inspection and maintenance periodicity, as well as configuration of helicopter ground and deck service facilities and recommended places of their installation.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Geometric constraints system formation for helicopter construction


    Beteiligte:
    Dergachev A.N. (Autor:in) / Klychnikova M.V. (Autor:in)


    Erscheinungsdatum :

    2023




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Unbekannt




    Geometric Modelling of Helicopter Ammunitions Vulnerability

    Volodko, A. M. / Gorshkov, V. A. | British Library Conference Proceedings | 1996


    Soviet Helicopter Construction

    A. M. Izakson | NTIS | 1966


    Helicopter close-order formation keeping system

    Evans, H.J. | Engineering Index Backfile | 1966


    Application of CAD System in Geometric Modeling for Helicopter Preliminary Design

    Xu, L. J. / Shen, M. S. | British Library Online Contents | 1992


    Design of helicopter rotors to noise constraints

    Schaeffer, E. G. / Sternfeld, H., Jr. | NTRS | 1978