The compressor turbine spun at up to 68, 000 rpm while the output turbine spun at up to 65, 000 rpm.
2.
The design included eight Armstrong Siddeley Viper turbojet engines, a very large centre rotor / impeller with Lundstrom compressor turbines, with the cockpit mounted in the top / centre.
3.
The subsequent technical investigation indicated that there was poor quality control in the assembly of the compressor turbine, leading to failure of the complete unit after several compressor blades separated.
4.
In the late 1980s, GE also proposed a much larger turboprop, the T407 / GLC38, with a five-stage axial / one-stage centrifugal mixed-flow compressor; an annular combustor with 15 burners; a two-stage compressor turbine; a three-stage power turbine; and max takeoff power of 6, 000 shp ( 4, 475 kW ).
5.
The initial " T700-GE-700 " is an ungeared free-turbine turboshaft, with a five-stage axial / one-stage centrifugal mixed-flow compressor, featuring one-piece " blisk " axial stages, with the inlet guide vanes and first two stator stages variable; an annular combustion chamber with central fuel injection to improve combustion and reduce smoke; a two-stage compressor turbine; and a two-stage free power turbine with tip-shrouded blades.
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