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 Oil Engine and Gas Turbine v 29 n 332 June 1961 p 74)
Turboprops for light aircraft
Aircraft Eng
Aircraft Engineering ; 33 , n 385
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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