Zusammenfassung der Ressource
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A gas turbine compressor is usually
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The compressor on the gas turbine
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can be driven by the load turbine
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is always of the axial type
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is always a multi-staged compressor
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is always independently driven
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is always a reciprocating type
Frage 3
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The combustion chamber of a gas turbine
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increases the pressure of the compressed air
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is heated between the load turbine and the compression turbine
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burns fuel with excess air
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is water cooled
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rotates at shaft speed
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Many typical steam plant auxiliaries are eliminated with a gas turbine due to its
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Gas turbines are very popular where
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noise does not present a problem
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water is scarce
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industrial sites are small and in congested areas
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thermal pollution is of major concern
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natural gas is plentiful
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gas turbines are ideal when considering
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A two shaft gas turbine
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has the load turbine downstream from the compressor turbine
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has the first turbine drive the prop on a turbo-prop engine
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is always an open cycle type
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is always a closed cycle type
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does not require a starting motor
Frage 8
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A gas turbine is not self-starting. It must be rotated at _________ of its maximum speed before fuel is turned on
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10% to 30 %
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15% to 30 %
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20% to 30 %
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25% to 30 %
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25% to 50%
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Early gas turbines were handicapped by
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metal not being able to withstand high speed centrifugal forces
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the inability to get enough air into the combustion chamber
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metals not standing the high temperatures involved
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their high operating speeds
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their inadequate power capability
Frage 10
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The temperature to which the air can be raised at the turbine inlet is
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an indication of a units power
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directly related to the units size
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a function of the air compressor input
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an indication of the units efficiency
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important for proper compressor performance
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The low installation cost of a gas turbine is
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due to cheap materials in the blades
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due to short fuel lines
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because no fuel pump is required
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because no electrical wiring is required
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because less auxillary equipment is needed