In order to make better decisions during advanced development of turbine engines, life cycle cost (LCC) methodologies must adequately reflect the impact of engine design decisions on the total system LCC. Two applications of Teledyne CAE's APSICOST Methodology are presented herein. These demonstrate the integrated nature of turbine engine LCC analyses with total aircraft system LCC.It is recommended that a joint airframe/propulsion/government effort be undertaken to standardize methods for reflecting aircraft system LCC impacts in turbine engine advanced development activities.


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    Titel :

    Applying Design-To-Life Cycle Cost Methods During Engine Advanced Development


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Wiltse, D. E. (Autor:in) / Apel, J. R. (Autor:in)

    Kongress:

    Aerospace Meeting ; 1978



    Erscheinungsdatum :

    01.02.1978




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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    Tegarden, F. W. / Shoemaker, W. W. | SAE Technical Papers | 1978


    Life Cycle Cost in Preliminary Engine Design

    Vernon, John | SAE Technical Papers | 1978


    Engine life cycle cost

    SININGER, W. | AIAA | 1976



    Engine life cycle cost considerations during the validation phase

    GIBSON, J. / COLLINS, D. / CONLEY, C. | AIAA | 1975