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What is the Clausius statement of the second law?
It's impossible to construct a heat engine which operates in reverse without a network input from the surroundings
what is the Kelvin-Plank statement of the second law?
It is impossible for any heat engine to receive heat from a single thermal reservoir and to produce an equivalent quantity of work
What is the first law of thermodynamics?
Q12-W12= E2-E1
What is a system?
a fixed quantity of material
What is the difference between control volume and system?
For control volume material crosses the boundary
what is rp for a typical open-cycle gas turbine?
10 to 30
what is the efficiency for a typical open-cycle gas turbine?
20-40%
1-2 compression stroke in a real otto cycle
compression of air and petrol vapour mixture
2-3 in a real otto cycle
spark ignites mixture, increasing pressure
3-4 power stroke in a real otto cycle
expansion of combustion products
4-1 in a real otto cycle
exhaust stroke, induction stroke
why might engine power be less than expected?
air breathed by the engine is at a lower density than the ambient air
1-2 compression in a real open cycle gas turbine engine
compression of air in compressor
2-3 in a real open cycle gas turbine engine
combustion of fuel in chambers, small pressure drop
3-4 expansion in a real open cycle gas turbine engine
expansion of combustion products in turbine
stage 1-2 of the joule cycle (compressor)
isentropic compression
stage 2-3 of the joule cycle (combustor)
isobaric heat addition
stage 3-4 of the joule cycle (turbine)
isentropic expansion
stage 4-1 of the joule cycle
isobaric heat rejection
why is stage 2-3 modelled as isobaric in a diesel cycle?
Combustion is slow compared to the movement of the piston
what happens to joule cycle efficiency when pressure ratio increases?
increases
When is specific net work in the joule cycle a maximum?
at medium pressure ratio
what is the difference between a jet engine and joule cycle?
in a jet engine the turbine provides only enough work to drive the compressor
what is the dew point temperature of a gaseous air/water vapour mixture?
The temperature which corresponds to the saturation temperature at the partial pressure of the water vapour
gibbs-dalton law
Each species in a gas mixture occupies the same volume and has the same temperature as the mixture
What's the worst COP for a refrigerator?
0
What's the worst COP for a heat pump?
1
Steps 1-2 of VCR (compressor)
Isentropic compression
steps 2-3 of VCR (condenser)
isobaric condensation
Steps 3-4 of VCR (valve)
Valve
steps 4-1 of VCR (evaporator)
Isobaric evaporation
how does Q being negative affect entropy?
Decreases entropy
how does Q being positive affect entropy?
Increases entropy
why are two stage cascade cycles used?
to improve COP
heat pump pros
Low CO2 emissions, low running costs
heat pump cons
High capital costs, efficiency drop in cold temperature
how do air source heat pumps work?
Use heat from the outside to heat an indoor space
how do ground source heat pumps work?
Absorb heat from the ground
Pros of ground source heat pumps
high COP
cons of ground source heat pumps
expensive
Two conditions to liquify a gas
Reach temp below Tcrit and a state under the saturation line
two methods to liquify a gas
High pressure, three stage cascade refrigeration plant
what is the linde process?
gas is compressed, cooled and throttled
why is gas behaviour real in the linde process?
Throttling has to cause a temperature drop
Turbomachine definition
A device that transfers energy between a rotor and a fluid due to dynamic action
What two ways can turbomachines be classified?
Fluid type, flow direction
What does a turbomachine stage consist of?
Rotor row, stator row
When is stagnation enthalpy constant?
Any process that doesn't involve heat or work transfer
Condition needed to define a stagnation state
Isentropic process
How do internal irreversibilities affect stagnation pressure?
Reduce stagnation pressure
What is the requirement for a real gas to be liquefied by throttling in a Linde process?
the Joule-Thomson coefficient must be greater than 0
what is the absolute reference frame in turbomachinery?
fixed in relation to stator
what is the relative reference frame in turbomachinery?
fixed in relation to the rotor
Reaction definition
the ratio of static enthalpy change between in rotor to stagnation enthalpy change in stage
pros of impulse turbine
smaller tip leakage
pros of reaction turbine
smaller friction loss
cons of impulse turbine
higher friction loss
cons of reaction turbine
Higher tip leakage
why are many stages for a reaction turbine in a compressor needed for an effective pressure ratio?
If the reaction is too high it can cause boundary layer separation