Gas turbines for power generation are normally used To supply base load requirements To supply peak load requirements In emergency To enable start thermal power plant TRUE ANSWER : ? YOUR ANSWER : ?
A large clearance volume in a reciprocating compressor results in Increased volume flow rate Lower delivery pressure Lower suction pressure Reduced volume flow rate TRUE ANSWER : ? YOUR ANSWER : ?
In a turbo jet engine, subsequent to heat addition to compressed air, to get the power output, the working substance is expanded in Exit nozzle, which is a constant volume process Turbine blades, which is essentially an isentropic process Turbine blades, which is a constant volume process Exit nozzle, which is essentially an isentropic process TRUE ANSWER : ? YOUR ANSWER : ?
The stagnation pressure rise in a centrifugal compressor takes place In the impeller only In the diffuser only In the diffuser and impeller In the inlet guide vanes only TRUE ANSWER : ? YOUR ANSWER : ?
Isothermal compression efficiency can be attained by running the compressor At very slow speed At average speed At zero speed At very high speed TRUE ANSWER : ? YOUR ANSWER : ?
In the axial flow gas turbine, the work ratio is the ratio of Actual total head temperature drop to the isentropic total head drop from total head inlet to static head outlet Output and input Compressor work and turbine work Actual compressor work and theoretical compressor work TRUE ANSWER : ? YOUR ANSWER : ?
The compressor capacity is defined as the Actual volume of the air delivered by the compressor when reduced to normal temperature and pressure conditions Volume of air sucked by the compressor during its suction stroke None of these Volume of air delivered by the compressor TRUE ANSWER : ? YOUR ANSWER : ?
Inter-cooling in gas turbine results in Increase in net output but decrease in thermal efficiency Increase in thermal efficiency but decrease in net output Decrease in both thermal efficiency and net output Increase in both thermal efficiency and net output TRUE ANSWER : ? YOUR ANSWER : ?
The ratio of the increase in pressure in rotor blades to total increase in pressure in the stage is called Degree of reaction Pressure ratio Pressure coefficient Slip factor TRUE ANSWER : ? YOUR ANSWER : ?
Gas turbine as compared to internal combustion engine All of the listed here Has more efficiency Can be driven at a very high speed Produces uniform torque TRUE ANSWER : ? YOUR ANSWER : ?