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22-Mec-B2 Environmental Control in Buildings · May 2013

Question 3 of 8: Two-stage ammonia refrigeration with a direct-contact intercooler (20 marks)

Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)

Notes on this paper

Paper format. Professional Engineers of Ontario / EGBC annual examination, 07-Mec-B2 (now 22-Mec-B2) Environmental Control in Buildings, May 2013 sitting. Three hours, open book. Eight problems of 20 points each; the candidate is instructed to solve five and to nominate which five are to be graded. Psychrometric charts and a pressure–enthalpy diagram for ammonia (R-717) are appended to the paper, and candidates are expected to bring an environmental-control text and steam tables. Instruction 1 invites the candidate to state any interpretation assumptions with the answer — that latitude is used explicitly below where the printed data are redundant.

All eight problems are worked here. Every psychrometric state has been recomputed from the ASHRAE formulation for saturation vapour pressure rather than scaled off a chart, so the numbers are tighter than a graphical solution would be; chart-quality agreement (about ±0.2 K and ±0.0002 kg/kg) is all that an examiner expects.

Reference texts for this subject.

Psychrometric relations used throughout. At barometric pressure $p$, with saturation vapour pressure $p_{ws}(t)$ from the ASHRAE correlation,

$$W = 0.6220\,\frac{\phi\,p_{ws}(t)}{p - \phi\,p_{ws}(t)}, \qquad h = 1.006\,t + W\,(2501 + 1.86\,t)$$

in SI (kJ per kg of dry air), and in the inch-pound system $h = 0.240\,t + W\,(1061 + 0.444\,t)$ Btu per lb of dry air. The thermodynamic wet-bulb temperature is obtained from the adiabatic-saturation equation, which is what a chart's constant-wet-bulb lines represent.

Question 3: Two-stage ammonia refrigeration with a direct-contact intercooler (20 marks)

Question text not reproduced: the examination questions are © Engineers and Geoscientists BC. Open the official past paper (linked at the top of this page) to read the question, then follow the worked solution below.

Given. The two-stage ammonia (R-717) plant of the figure printed with the question, with a direct-contact heat exchanger acting as both flash chamber and de-superheater at the intermediate pressure.

Given data
QuantityValue
Refrigeration capacity30 tons = 360,000 Btu/h = 6000 Btu/min
Evaporator exit, state 1saturated vapour at −20 °F (18.3 psia)
Intermediate pressure (heat exchanger)80 psia
Condenser pressure250 psia
Compressor-2 inlet, state 3saturated vapour at 80 psia
Isentropic efficiency, both stages85%
Expansion-valve inlets, states 5 and 7saturated liquid

Find. the mass-flow ratio $\dot{m}_2/\dot{m}_1$, the power input to each stage in horsepower, and the coefficient of performance.

Condenserheat outComp 2ẆDirect-contactheat exchanger(flash intercooler)Comp 1ẆEvaporator30 tons invalvevalve5634781280 psia in theintercooler;250 psia condenser
The plant, with the state numbering of the figure supplied in the question. Compressor 1 handles the evaporator flow $\dot{m}_1$; compressor 2 handles the whole condenser flow $\dot{m}_2$. The direct-contact heat exchanger receives superheated vapour at 2 and the throttled liquid at 6, and delivers saturated vapour at 3 to compressor 2 and saturated liquid at 7 to the low-stage expansion valve.

Approach. Read the eight enthalpies from the R-717 tables and the supplied p–h diagram, correct both compressions for 85% isentropic efficiency, then get the flow ratio from a combined mass and energy balance on the direct-contact heat exchanger and scale to the 30-ton duty.

  1. Fix the states. All enthalpies are on the usual R-717 datum ($h_f = 0$ at −20 °F is not used; the datum is $h_f = 0$ at −40 °F), read from the saturation table and the appended pressure–enthalpy chart. Saturation temperatures are 44.4 °F at 80 psia and 110.8 °F at 250 psia.
    Ammonia states
    StateCondition$h$ (Btu/lb)$s$ (Btu/lb·R)
    1sat. vapour, −20 °F604.51.4041
    2s80 psia, $s = s_1$691.91.4041
    280 psia, actual707.4—
    3sat. vapour, 80 psia623.31.2934
    4s250 psia, $s = s_3$693.31.2934
    4250 psia, actual705.7—
    5 = 6sat. liquid, 250 psia (throttled)167.8—
    7 = 8sat. liquid, 80 psia (throttled)91.6—
  2. Actual first-stage discharge. The isentropic compression from 18.3 to 80 psia raises the enthalpy by $691.9 - 604.5 = 87.4$ Btu/lb, so $$h_2 = h_1 + \frac{h_{2s} - h_1}{\eta_c} = 604.5 + \frac{87.4}{0.85} = \boxed{707.4\ \text{Btu/lb}}$$ which on the chart is about 186 °F — strongly superheated, and exactly why intercooling is worth the extra hardware.
  3. Actual second-stage discharge. From saturated vapour at 80 psia to 250 psia, $$h_4 = h_3 + \frac{h_{4s} - h_3}{\eta_c} = 623.3 + \frac{693.3 - 623.3}{0.85} = 705.7\ \text{Btu/lb}$$ about 212 °F. Note that de-superheating in the direct-contact exchanger has brought the second stage back to the saturation line, so its discharge is cooler than the first stage's despite the higher pressure.
  4. Mass-flow ratio from the direct-contact heat exchanger. The exchanger is adiabatic and receives $\dot{m}_1$ of superheated vapour at 2 plus $\dot{m}_2$ of throttled two-phase refrigerant at 6; it delivers $\dot{m}_2$ of saturated vapour at 3 and $\dot{m}_1$ of saturated liquid at 7. Energy balance: $$\dot{m}_1 h_2 + \dot{m}_2 h_6 = \dot{m}_2 h_3 + \dot{m}_1 h_7 \;\Rightarrow\; \frac{\dot{m}_2}{\dot{m}_1} = \frac{h_2 - h_7}{h_3 - h_5}$$ Substituting, $$\frac{\dot{m}_2}{\dot{m}_1} = \frac{707.4 - 91.6}{623.3 - 167.8} = \frac{615.8}{455.5} = \boxed{1.352}$$ The high stage carries 35% more refrigerant than the low stage, the extra being the vapour flashed off in the intercooler.
  5. Low-stage mass flow from the 30-ton duty. The refrigerating effect per pound is $h_1 - h_8 = 604.5 - 91.6 = 512.9$ Btu/lb, so $$\dot{m}_1 = \frac{6000}{512.9} = 11.70\ \text{lb/min},\qquad \dot{m}_2 = 1.352 \times 11.70 = 15.82\ \text{lb/min}$$
  6. Power input to each stage. With 1 hp = 42.41 Btu/min, $$\dot{W}_1 = 11.70\,(707.4 - 604.5) = 1204\ \text{Btu/min} = \boxed{28.4\ \text{hp}}$$ and for the high stage $$\dot{W}_2 = 15.82\,(705.7 - 623.3) = 1302\ \text{Btu/min} = \boxed{30.7\ \text{hp}}$$ The two stages are almost equally loaded, which is what a well-chosen intermediate pressure achieves.
  7. Coefficient of performance. $$\text{COP} = \frac{\dot{Q}_{evap}}{\dot{W}_1 + \dot{W}_2} = \frac{6000}{1204 + 1302} = \boxed{2.39}$$ For comparison, a single-stage machine between the same −20 °F and 110.8 °F limits at 85% efficiency lands near 2.0, so the second stage buys roughly a 20% improvement as well as a much cooler discharge.
Final results
QuantityResult
Mass-flow ratio $\dot{m}_2/\dot{m}_1$1.352
Low-stage mass flow11.70 lb/min (0.0884 kg/s)
High-stage mass flow15.82 lb/min (0.1195 kg/s)
Power, compressor 128.4 hp (21.2 kW)
Power, compressor 230.7 hp (22.9 kW)
Total compressor power59.1 hp (44.1 kW)
Coefficient of performance2.39