For gas turbines compressors used are
A.Reciprocating type
B.Centrifugal type
C.Axial flow type
D.Lobe type
E.Sliding vane type
A.Reciprocating type
B.Centrifugal type
C.Axial flow type
D.Lobe type
E.Sliding vane type
A.Higher
B.Lower
C.Not affected
D.Fluctuating
E.Depends on load
A.Sand cast
B.Die cast
C.Turned from bar stock
D.Forged
E.Cold headed
A.The fuel emits vapours at a rate which produces an inflammable mixture with air
B.The fuel spontaneously ignites
C.The fuel ignites with clearly visible flash
D.The fuel ignites without a park
E.Fuel vaporises at the prescribed rate
A.Valve opens
B.Valve closes after opening
C.Valve opens initially
D.Valve spring pressure is adjusted
E.None of the above
A.IHP
B.BHP
C.IHP-BHP
D.Friction horse power
E.Friction horse power at cranking r.p.m
A.Reduces heat loss in exhaust
B.permits use of higher compression ratio
C.Improves thermal efficiency
D.Permits use of fuels of inferior quality
E.None of the above
A.1.68
B.1.41
C.1.35
D.1.135
A.Lower altitudes
B.Higher altitude
C.Low speeds
D.High speeds
E.None of the above
A.Thermal efficiency improves
B.The output of turbine increases
C.Work done by compressor reduces
D.The ratio compressor compressor work/turbine output decreases
E.None of the above