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Aviation History
1954
1954 - 0162.PDF
Flight, 15 January 1954 JV<?. 3. Petrol at 2,000 p.s.i. flows from these fuel-pump components—of selected materials and finishes down to 2 micro-inches. Lubricated only by the fuel, these reciprocating and rotating parts operate at speeds up to 4,000 r.p.m. FUEL AND COMBUSTION SYSTEMS FOR GAS TURBINE ENGINES JOSEPH LUCAS (GAS TURBINE EQUIPMENT) LTD., BIRMINGHAM & BURNLEY
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