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Aviation History
1952
1952 - 1235.PDF
Flight, 2 May 1952 A BURNING PROBLEM ui(z won1 COMBUSTION CHAMBER ion sheet metal work designed and manufactured by us to ensure high efficiency combustion in aircraft gas turbines. Patent flow system gives high rates of heat release and even- temperature distribution at turbine. JOSEPH LUCAS (GAS TURBINE EQUIPMENT) LTD. BIRMINGHAM 28 AND BURNLEY, ENGLAND
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