To meet requirements for turboprop engines T.P./60 and T.P./90, suitable for club, executive and agricultural aircraft, were developed by Rover Gas Turbines Ltd; two engines are similar featuring single shaft turbine propeller engine with single stage centrifugal compressor, one combustion chamber, single stage turbine and shaft power outlet through reduction gear to propeller; propeller blade roots are retained by ball thrust bearings and pitch movements synchronized by bevel gears. (See also Aircraft Eng v 33 n 385 Mar 1961 p 67)
Turboprops for light aircraft
Oil Engine Gas Turbine
Oil Engine and Gas Turbine ; 29 , n 332
1961
Aufsatz (Zeitschrift)
Englisch
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Emerald Group Publishing | 1961
Engineering Index Backfile | 1961
Engineering Index Backfile | 1955
|Commercial Aircraft Directory . Regional jets and turboprops listed
Online Contents | 2000
Online Contents | 1995
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