Turbo power pack - Phase I

Murthy, MVA and Thunga, KS and Murthy, SJK (1989) Turbo power pack - Phase I. Project Report. National Aerospace Laboratories, Bangalore.

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    A compact turbo power pack was designed for application i n underwater propulsion . The turbo power pack designed consists of a high pressure ratio supersonic partial admission impulse turbine coupled to a reduction gear box to reduce the turbine shaft speed to the level of the shaft speeds of the contrarotating propellers . The possible configurations of the turbine and gear box were studied to optimise the system and the design parameters . The report presents the details of the final configuration of the system .

    Item Type: Proj.Doc/Technical Report (Project Report)
    Uncontrolled Keywords: Supersonic turbine, Propulsion, Reduction gear box
    Subjects: AERONAUTICS > Aircraft Propulsion and Power
    Division/Department: Propulsion Division, Propulsion Division, Propulsion Division
    Depositing User: Ms Indrani V
    Date Deposited: 09 Oct 2012 13:58
    Last Modified: 09 Oct 2012 13:58
    URI: http://nal-ir.nal.res.in/id/eprint/11075

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