Lecture 7 Flashcards

1
Q

Power cycles are ways of

A

converting an energy transfer in the form of heat into an energy transfer in the form of work

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2
Q

petrol engine

A

otto cycle petrol

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3
Q

diesel engine

A

diesel cycle diesel

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4
Q

jet engine and gas turbine

A

brayton cycle kerosane jet gas/oil for gas

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5
Q

coal power station

nuclear power

A

rankine

rankine

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6
Q

heat sink

A

receives energy in the form of heat

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7
Q

heat engine

A

device that takes energy in the form of heat from a hot reservoir converts it into work engine then reject heat to somewhere that is a lower temperature (heat sink)

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8
Q

a heat engine must

A

work between a high temp and a lower temp

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9
Q

thermal efficiency

A

work out/heat high

where work = heat high - heat low

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10
Q

for heat engine itself entropy

A

stays the same since it always remains teh same internally

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11
Q

maximum thermal efficiency =

A

(Thigh - Tlow)/Thigh

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12
Q

what is maximum thermal efficiency known as

A

Carnot efficiency

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13
Q

since some heat from heat source ends in the heat sink the second law can be stated as

A

it is impossible to construct a system that will operate in a cycle, extract heat from a reservoir and do an equivalent amount of work on the surroundings

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14
Q

heat engine works between

A

heat source and a heat sink

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15
Q

area under the T-s diagram

A

Heat in

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16
Q

why is the work out only the top part of the area under ts diagram

A

area on the bottom part is work in, amount of you to put back in to keep cycle going

17
Q

area encoled by the Ts diagram

A

is the work out for a reversible cycle

18
Q

if cycle goes clockwise on Ts diagram net work is

A

out if it goes anticlockwise net work is inwards - no longer power cycle

19
Q

if cycle goes clockwise on pv diagram net work is

A

out if it goes anticlockwise net work is inwards - no longer power cycle

20
Q

carnot cycle comprises of

A
4 reversible processes (can be air or steam)
open system carnot cylce for air
1 isothermal turbine
2 isentropic turbine
3 isothermal compressor
4 isentropic compressor
21
Q

four processes of the carnot cycle

A

1 isothermal expansion W=Q dH=0
2 isentropic expansion Q=0
3 Isothermal compressor W=Q dH=0
4 isentropic compressor Q=0

22
Q

why does the ts diagram prove the carnot cycle is the most efficient

A

made a box

maximum area for given minimum and maximum temperatures

23
Q

carnot cycle complete cycle is reversible if

A

isothermal expansion and compression are reversible and

the expansion and compression are isentropic

24
Q

issues with making a carnot cycle

A

isentropic is impossible and isothermal costs are huge and extremely difficult to engineer

25
carnot cycle all heat added at
maximum temperature dS=dQ/T make T as large as possible minimise entropy increase
26
carnot principle
Q high/ Q low = Thigh/Tlow
27
given carnot efficiency what would you want to maximise but would struggle to do so
Thigh - Tlow to be as big as possible - issues with operating range of materials T high melting T low freezing
28
Brayton cycle contrains
is an open system containing three reversible processes 1 isentropic compressor 2 isobaric heat addition (combuster) 3 isentropic turbine
29
reversible =
max output
30
no line between 4 and 1
air taken in fresh each time (not quite a cycle)
31
% of turbine power used to drive compressor
1 -(net work / total turbine work)
32
net work
work out of turbine - work needed to drive compressor
33
add in isentropic efficiency
more work into compressor less work out of turbine (though do need to put less heat in is compressor output temp is higher)
34
additional step taken when dealing with isentropic efficiencies
multiply (or divide) isentropic case temperature difference by efficiency to add (or minus) from starting temperature
35
effect of combustor pressure
causes pressure drop across combustor making outlet temperature higher
36
when calculating pressure drop across combustor
compressor same need to calculate need starting pressure for turbine starting temp will remain same
37
compressor outlet pressure =
turbine inlet pressure unless theres pressure drop
38
brayton cycle equations
W/Q=m*cp*(T1-T2) and polytropic equations use polytropic equations to find final temperatures and pressure use isentropic efficiency to correct them calculate heat in and out