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IGT PO1.1 GAS TURBINE CYCLES AND COMPONENTS

Authored by Wardhyana Yahya

Engineering

Vocational training

Used 5+ times

IGT PO1.1 GAS TURBINE CYCLES AND COMPONENTS
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17 questions

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1.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

Which of the following best describes a rotodynamic machine?

A device that converts electrical energy into mechanical energy.

A mechanism that converts the energy of a moving fluid into the energy of a rotating shaft.

An apparatus that stores kinetic energy in a rotating drum.

A system that converts solar energy into electrical power.

2.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

What is the primary mechanism by which a rotodynamic machine operates?

Conversion of potential energy to kinetic energy.

Transfer of heat energy to mechanical energy.

Transfer of energy between a moving fluid and a rotating shaft.

Conversion of mechanical energy to electrical energy.

3.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

In a turbine, how is energy transferred from the fluid to the rotor?

The fluid increases its velocity as it passes through the rotor, gaining energy.

The rotor's speed decreases due to the fluid's tangential force, causing energy loss.

The fluid's tangential momentum decreases as it imparts a tangential force on the rotor, transferring energy to the rotor.

The fluid's energy is entirely converted into heat as it exits the rotor.

4.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

In a fan, pump, or compressor, what role does the impeller play?

It reduces the tangential momentum of the fluid, transferring energy from the fluid to the rotor.

It increases the tangential momentum of the fluid, transferring energy from the rotor to the fluid.

It stores mechanical energy to be later used for fluid movement.

It converts electrical energy directly into fluid motion.

5.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

Which of the following statements is TRUE about aero derivative gas turbines?

They are specifically designed for base load operation.

They can produce full power within three minutes after start up.

They have a lower capital cost per kilowatt installed compared to industrial gas turbines.

They can produce a maximum output of more than 260 MW.

6.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

What is a key difference between aero derivative and industrial gas turbines?

Aero derivative turbines are more suitable for base load operation than industrial turbines.

Industrial turbines have a higher capital cost per kilowatt installed than aero derivative turbines.

Aero derivative turbines are modified aircraft jet engines, while industrial turbines are designed specifically for stationary power generation.

Industrial turbines can produce full power within three minutes, while aero derivative turbines take longer.

7.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

Why are industrial gas turbines considered suitable for base load operation?

They can produce full power very quickly after startup.

They have a lower maximum output compared to aero derivative turbines.

They have a lower capital cost per kilowatt installed and more robust construction.

They are derived from aircraft jet engines and can reach full power in less than 10 minutes.

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