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It has been proposed to use the thermal gradient of the ocean to drive a heat engine. Suppose that at a certain location the water temperature is 22°Cat the ocean surface and 4°Cat the ocean floor.

(a) What is the maximum possible efficiency of an engine operating between these two temperatures?

(b) If the engine is to produce 1GWof electrical power, what minimum volume of water must be processed (to suck out the heat) in every second?

Short Answer

Expert verified

a) Maximum possible efficiency of an engine is 6.1%

b) Minimum volume of water that must be processed in every second to produce1GWof electrical power is86m3·s-1

Step by step solution

01

Part (a) - Step 1: To find

The maximum possible efficiency of heat engine.

02

Part (a) - Step 2: Explanation

Given:

The temperature of hot reservoir =22°C

The temperature of cold reservoir =4°C

Formula:

The expression for the efficiency of heat engine is as follows:

emax=1-TcTh

Here, Tcis temperature of cold reservoir

This temperature of hot reservoir.

Calculation:

The temperature of hot reservoir Kelvin is:

role="math" localid="1648159148570" Th=273+22=295KTc=273+4=277K

Now Substituting the values of Tcand Thin the above expression

emax=1-277K295K=0.061=6.1\%

Hence, the maximum possible efficiency of heat engine is6.1%

03

Part (b) - Step 3: To find

Minimum volume of water that must be processed in every second to produce1GWof electrical power.

04

Part (b) - Step 4 : Explanation

Since the temperature of ocean water drops as the engine extracts heat from it, the engine's efficiency varies.

The temperature differential between the cold and hot reservoirs would be as follows:

22°C-4°C=18°C

The temperature difference between the cold and warm water is equivalent to half of the temperature difference at equilibrium.

That is

ΔT=18°C2=9°C

The average temperature of reservoirs is 18°Cand 9°CThus, the efficiency of heat engine is

e=1-(9+273)K(18+273)K=0.0309=3.09%

The heat energy removed from each kilogram of the warm water is

Qc=mCwΔT

Where,

mis mass of the water,

Cwis the specific heat of water, and

ΔTis change in temperature.

Now Substitute the values of ΔTand Cwrespectively

Qm=4186J/kg°C9°C=37.674×103J/kg

But, the efficiency of the engine is 3.09%.

05

Part (b) - Step 5: Calculation

Thus, the heat energy produced per kilograms is as follows:

=1.164×104J/kg

The work done per each second is called its power.

P=Wt

Here, t is the time interval.

Substitute 1GWfor P

Wt=1GW109W1GWWt=109WWt=109J⋅s−1

Thus, the total mass of the water per second is as follows:

mt=109J·s-11.164×104J·kg-1=8.6×104kg·s-1

The total amount of water in cubic meters per second is

8.6×104kg·s-110-3m31kg=86m3·s-1

Hence the total amount of water in cubic meters per second would be

86m3·s-1.

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Most popular questions from this chapter

A power plant produces1GWof electricity, at an efficiency of 40%(typical of today's coal-fired plants).

(a) At what rate does this plant expel waste heat into its environment?

(b) Assume first that the cold reservoir for this plant is a river whose flow rate is 100m3/s.By how much will the temperature of the river increase?

(c) To avoid this "thermal pollution" of the river, the plant could instead be cooled by evaporation of river water. (This is more expensive, but in some areas it is environmentally preferable.) At what rate must the water evaporate? What fraction of the river must be evaporated?

The ingenious Stirling engine is a true heat engine that absorbs heat from an external source. The working substance can be air or any other gas. The engine consists of two cylinders with pistons, one in thermal contact with each reservoir (see Figure 4.7). The pistons are connected to a crankshaft in a complicated way that we'll ignore and let the engineers worry about. Between the two cylinders is a passageway where the gas flows past a regenerator: a temporary heat reservoir, typically made of wire mesh, whose temperature varies

gradually from the hot side to the cold side. The heat capacity of the regenerator is very large, so its temperature is affected very little by the gas flowing past. The four steps of the engine's (idealized) cycle are as follows:
i. Power stroke. While in the hot cylinder at temperature Th, the gas absorbs heat and expands isothermally, pushing the hot piston outward. The piston in the cold cylinder remains at rest, all the way inward as shown in the figure.
ii. Transfer to the cold cylinder. The hot piston moves in while the cold piston moves out, transferring the gas to the cold cylinder at constant volume. While on its way, the gas flows past the regenerator, giving up heat and cooling to Tc.
iii. Compression stroke. The cold piston moves in, isothermally compressing the gas back to its original volume as the gas gives up heat to the cold reservoir. The hot piston remains at rest, all the way in.
iv. Transfer to hot cylinder. The cold piston moves the rest of the way in while the hot piston moves out, transferring the gas back to the hot cylinder at constant volume. While on its way, the gas flows past the regenerator, absorbing heat until it is again at Th.

(a) Draw a PV diagram for this idealized Stirling cycle.
(b) Forget about the regenerator for the moment. Then, during step 2, the gas will give up heat to the cold reservoir instead of to the regenerator; during step 4 , the gas will absorb heat from the hot reservoir. Calculate the efficiency of the engine in this case, assuming that the gas is ideal. Express your answer in terms of the temperature ratio Tc / Th and the compression ratio (the ratio of the maximum and minimum volumes). Show that the efficiency is less than that of a Carnot engine operating between the same temperatures. Work out a numerical example.
(c) Now put the regenerator back. Argue that, if it works perfectly, the efficiency of a Stirling engine is the same as that of a Carnot engine.
(d) Discuss, in some detail, the various advantages and disadvantages of a Stirling engine, compared to other engines.

Prove that if you had a refrigerator whose COP was better than the ideal value (4.9), you could hook it up to an ordinary Carnot engine to make an engine that produces no waste heat.

Consider an ideal Hampson-Linde cycle in which no heat is lost to the environment.

(a) Argue that the combination of the throttling valve and the heat exchanger is a constant-enthalpy device, so that the total enthalpy of the fluid coming out of this combination is the same as the enthalpy of the fluid going in.

(b) Let xbe the fraction of the fluid that liquefies on each pass through the cycle. Show that

x=Hout-HinHout-Hliq,

where Hinis the enthalpy of each mole of compressed gas that goes into the heat exchanger, Houtis the enthalpy of each mole of low-pressure gas that comes out of the heat exchanger, and Hliqis the enthalpy of each mole of liquid produced.

(c) Use the data in Table 4.5to calculate the fraction of nitrogen liquefied on each pass through a Hampson-Linde cycle operating between 1 bar and 100 bars, with an input temperature of 300K. Assume that the heat exchanger works perfectly, so the temperature of the low-pressure gas coming out of it is the same as the temperature of the high-pressure gas going in. Repeat the calculation for an input temperature of 200K.

To get more than an infinitesimal amount of work out of a Carnot engine, we would have to keep the temperature of its working substance below that of the hot reservoir and above that of the cold reservoir by non-infinitesimal amounts. Consider, then, a Carnot cycle in which the working substance is at temperatureThwas it absorbs heat from the hot reservoir, and at temperatureTcwas it expels heat to the cold reservoir. Under most circumstances the rates of heat transfer will be directly proportional to the temperature differences:

QhΔt=KTh-ThwandQcΔt=KTcw-Tc

I've assumed here for simplicity that the constants of proportionality Kare the same for both of these processes. Let us also assume that both processes take the

same amount of time, so theΔt''s are the same in both of these equations.*

aAssuming that no new entropy is created during the cycle except during the two heat transfer processes, derive an equation that relates the four temperaturesTh,Tc,Thwand Tcw

bAssuming that the time required for the two adiabatic steps is negligible, write down an expression for the power (work per unit time) output of this engine. Use the first and second laws to write the power entirely in terms of the four temperatures (and the constant K), then eliminateTcwusing the result of part a.

cWhen the cost of building an engine is much greater than the cost of fuel (as is often the case), it is desirable to optimize the engine for maximum power output, not maximum efficiency. Show that, for fixed Thand Tc, the expression you found in part bhas a maximum value at Thw=12Th+ThTc. (Hint: You'll have to solve a quadratic equation.) Find the correspondingTcw.

dShow that the efficiency of this engine is 1-Tc/ThEvaluate this efficiency numerically for a typical coal-fired steam turbine with Th=600°CandTc=25°C, and compare to the ideal Carnot efficiency for this temperature range. Which value is closer to the actual efficiency, about 40%, of a real coal-burning power plant?

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