Recognizing need for simple turbine power plant that would be efficient with moderate flying speed, Bristol Aeroplane Co have been experimenting with gas turbine drives for normal type of propeller, and outcome is 2000-hp Theseus I engine, which has dry weight of 2310 lb and installed weight of very little more, there being no liquid coolant and only one small cooler for lubricating oil. (See also Engineering v 161 n 4175 Jan 18 1946 p 56; Flight v 48 n 1928 Dec 6 1945 p 597-9; Aeroplane v 69 n 1802 Dec 7 1945 p 657-8; Mech World v 119 n 3080 Jan 11 1946 p 29; Aircraft Production v 8 n 87 Jan 1946 p 19-20)


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    Title :

    Gas-turbine propeller drive for aircraft


    Additional title:

    Can Aviation


    Published in:

    Publication date :

    1946


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




    Gas-turbine propeller drive for aircraft

    Engineering Index Backfile | 1945


    Gas-turbine propeller drive for aircraft

    Engineering Index Backfile | 1946


    Gas-turbine propeller drive for aircraft

    Engineering Index Backfile | 1946


    Gas-turbine propeller drive for aircraft

    Engineering Index Backfile | 1946


    Gas-turbine propeller drive for aircraft

    Engineering Index Backfile | 1945