Naval missions require aircraft of moderate speeds operating at moderate altitudes; this indicates continuing need for shaft-power turbine engines; significant variations, combinations, and configurations available in engines under development in range of shaft horsepowers from about 50 to 16,000; problem areas include component compatibility, reduction gearbox reliability, torquemeter adequacy, droop, and propellers. (see also abstract in SAE -- J v 68 n 6 June 1960 p 128-9)
Trends in navy turboprop/turboshaft engine developments
SAE -- Paper
SAE Meeting ; 1960
1960
14 pages
Conference paper
English
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