Frage 1
Frage
A dual shaft gas turbine has the following advantages
1. flexability in system configuration 2. lower first cost
3. smaller starting motors 4. higher operating pressures
Frage 2
Frage
A gas turbine that uses an intercooler during compression
Antworten
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has it located prior to compression
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is located after the compressor but before the combustor
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has a higher power output at the turbine
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requires a larger starting motor
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all of the above
Frage 3
Frage
Intercoolers are used on a gas turbine compressors to:
Antworten
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reduce the specific volume of the air
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increase the dewpoint of the air
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remove the moisture from the air
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increase the combustor efficiency
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increase compressor life
Frage 4
Frage
A reheater in a gas turbine cycle will:
1. compress more air 2. allow for smaller turbine blades
3. allow for a smaller combustor 4. improve the cycle efficiency
5. will require less air for the same turbine output
Antworten
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2,3,4
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4,5
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1,3,5
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2,4
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1,2,3,4,5
Frage 5
Frage
A regenerator in a gas turbine cycle is also referred to as:
Antworten
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heat exchanger
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cyclone
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duct burner
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intercooler
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safety device
Frage 6
Frage
A gas turbine
1. is a hot air engine 2. has a pressure ratio of 30 - 1
3. always use axial air compressors 4. uses a lower density working medium
Frage 7
Frage
The flow of air and shaft speed of a gas turbine are fairly constant which results in _____________power outputs per unit weight.
Antworten
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constant
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very high
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proportional
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comparable
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efficient
Frage 8
Frage
A gas turbine is designed with the simplicity of a/an ________ and the advantages of a ______________.
Antworten
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steam turbine, internal combustion engine
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air compressor, diesel engine
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steam engine, locomotive boiler
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fuel cell, wind turbine
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rocket ship, airplane
Frage 9
Frage
In a gas turbine cycle the phrase Total energy Arrangement means:
Antworten
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it is a closed cycle system therefore all energy is contained within the system
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the system is based on purely theoretical calculations if all the energy was accounted for in the system
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the turbine provides all the necessary forms of energy
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the exhaust gases from the GT are passed through a HRSG to produce steam
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the gas turbine uses exhaust gas from a boiler as combustion air for the combustor
Frage 10
Frage
A gas turbine arrangement employing the total energy arrangement may be used to provide
1. air conditioning
2. heating
3. electricity
4. cool drinking water
Antworten
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1,2,3
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2,3,4
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1,2,4
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1,2,3,4
Frage 11
Frage
The disadvantage of a closed cycle gas turbine include:
1. higher initial cost 2. more space is required
3. more cooling water needed 4. more components needed
Antworten
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1,2,3
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2,3,4
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1,3,4
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1,2,4
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1,2,3,4
Frage 12
Frage
The regenerator in a gas turbine system gets its heat from:
Frage 13
Frage
Regenerator disadvantages include
1. pressure drop 2. temperature drop
3. fouling of heating surfaces 4. needs a large heating surface
Antworten
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1,2,3
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2,3,4
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1,3,4
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1,2,4
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1,2,3,4
Frage 14
Frage
using an intercooler in a gas turbine system will
1. create more power
2. lowers the airs specific volume
3. raise the 2nd stage air temp
4. drop some moisture from the air
Antworten
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1,2,3
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2,3,4
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1,3,4
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1,2,3,4
-
1,2,4
Frage 15
Frage
initial ignition in a gas turbine combustor is accomplished using
Frage 16
Frage
The function of the combustor is to
Antworten
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burn fuel with excess air
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increase the kinetic energy of the working fluid
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increase the compressed air pressure
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lower NOx emmisions
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increase the airs specific volume
Frage 17
Frage
The _________ on a gas turbine can be driven by the load turbine
Antworten
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starting motor
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aux oil system
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combustor
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air compressor
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power turbine
Frage 18
Frage
A gas turbine compressor may be ________ by design
Antworten
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axial or reciprocating
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screw or radial
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impulse or reaction
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radial or axial
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all of the above
Frage 19
Frage
Axial air compressor blades are commonly made from
1. aluminum
2. brass
3. titanium
4. stainless steel
Frage 20
Frage
Gas turbine casings are usually made from:
Frage 21
Frage
The compressor in a gas turbine has to pressurize the air to supply:
Antworten
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air to cool the turbine
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air for expansion in the turbine
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air for combustion and further expansion through the turbine
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air to the combustor for cooling
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air to provide exhaust gas for a HRSG
Frage 22
Frage
The compressor in a gas turbine system uses up to _________ of the energy supplied by the fuel