Design and development of a cold air turbine

Sridhara, K and Thunga, KS (1974) Design and development of a cold air turbine. Technical Report. National Aerospace Laboratories, Bangalore,India.

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    Abstract

    A high speed drive unit with a continuosly variable speed power characteristics is a necessary tool for testing protype compressors and fans and high speed bearings.Such a drive unit is a special purpose machine and is generally not available in the normal range of compressed air is already available at National Aeronautical Laboratory,it was decided to develop a compact cold gas turbine of jet engines was available from the Airforce disposal stock which formed the basis for the design of the turbine

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: High speed drive;Protype compressors;Industrial electric machine
    Subjects: ENGINEERING > Engineering (General)
    Division/Department: Propulsion Division, Propulsion Division
    Depositing User: shankar sk nadoor
    Date Deposited: 14 Nov 2006
    Last Modified: 24 May 2010 09:53
    URI: http://nal-ir.nal.res.in/id/eprint/3399

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