Technical features of BS 75 which has by-pass ratio of 1.75 to 1, maximum sea level thrust of 7550 lb and is suitable for twin engined short to medium range airliners of 50,000 lb all-up-weight, or 4-engined airliners of 70,000 to 90,000 lb all-up-weight; fan system and design, h-p compressor, and combustion system; BS 75 has 2 separate 2-stage turbines, one drives fan by means of shaft which is coaxial with that of h-p system; h-p shaft is mounted upon 2 bearings and 1-p shaft on 3; fuel consumption; military potential.
Bristol siddeley BS 75 turbofan
Aircraft Eng
Aircraft Engineering ; 34 , n 401
1962
Aufsatz (Zeitschrift)
Englisch
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