22-Mec-B2 Environmental Control in Buildings · May 2018
Question 4 of 8: Ground-water heat pump with R-134a (20 marks)
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. Eight problems, three hours, open book.
Problem 1 carries 30 marks, Problem 2 carries 10 marks and Problems 3 to 8
carry 20 marks each; candidates answer any five, and indicate their choice on
the cover of the first workbook. Psychrometric charts (SI and inch-pound) and
an R-134a pressure–enthalpy diagram are appended to the paper.
All eight problems are solved below, because the set as a whole
is the study resource.
Reference texts.
ASHRAE, Handbook — Fundamentals (2021): Ch.1 psychrometrics,
Ch.16 ventilation and infiltration, Ch.18 heating and cooling load
calculations, Ch.21 duct design, Ch.26 heat, air and moisture transmission.
McQuiston, Parker and Spitler, Heating, Ventilating and Air
Conditioning: Analysis and Design, 6th ed. — loads, psychrometric
processes, duct and air distribution design.
W. P. Jones, Air Conditioning Engineering, 5th ed. — the
percentage-saturation convention, apparatus dew point and coil by-pass factor,
face-and-by-pass plant.
Shan K. Wang, Handbook of Air Conditioning and Refrigeration, 2nd
ed. — single-duct reheat and VAV systems, discriminator (zone-demand)
control.
ASHRAE Standard 55-2023, Thermal Environmental Conditions for Human
Occupancy; ASHRAE Standard 62.1-2022, Ventilation for Acceptable
Indoor Air Quality.
National Building Code of Canada 2020 and NRCan / Environment and Climate
Change Canada climatic design data for the Canadian design conditions used in
Problems 5 and 7.
Check: two readings taken from the printed
paper.
(1) The length label on the Problem 6 duct sketch is printed as
“L1 = =100 ft == 6ft”. The equation editor
has dropped the symbols after each equals sign; the pattern
“something = something = 100 ft” and
“something = something = 6 ft” means four named
lengths in two equal pairs, and the sketch shows exactly four duct runs. The
solution therefore takes L1 = L2 = 100 ft
(plenum to tee, and tee to elbow) and L3 = L4 =
6 ft (the two drops to the ceiling diffusers), and states the reading
as an assumption under cover-page instruction 1. Only the pressure totals in
parts (c) and (d) depend on it; the duct diameters in part (a) do not.
(2) Problem 1 gives the outdoor air as “percentage saturation
50 %” but the room as “RH 50 %”. These are different
quantities and the difference is deliberate: percentage saturation is
$\mu = W/W_{s}$, relative humidity is $\phi = p_{w}/p_{ws}$. At 26 °C
the 50 % saturation state is 50.8 % RH, so treating them as
interchangeable shifts the outdoor humidity ratio by about
0.2 g/kg.
Question 4: Ground-water heat pump with R-134a (20 marks)
Given. A simple vapour-compression cycle whose two
saturation temperatures are fixed by the source approach and the stated delivery
pressure.
Given data, Problem 4
Quantity
Symbol
Value
Refrigerant
—
R-134a
Ground-water temperature
tw
4 °C
Evaporator approach
Δt
14 K
Compressor delivery pressure
p2
1.0164 MPa
Air volume flow delivered
V
0.8 m³/s at 35 °C, atmospheric
Air temperature rise over the condenser
—
6 °C → 35 °C
Compressor speed, action
N
300 rpm, single acting
Volumetric efficiency
ηvol
0.85
Combined compressor / motor efficiency
ηo
0.87
Electricity tariff
—
0.10 $/kWh
Find. (a) the coefficient of performance, (b) the
refrigerant mass flow, (c) the compressor swept volume in cm³, and (d) the
hourly running cost against direct electric resistance heating.
Approach. The two saturation temperatures fix all four cycle
states; the air-side duty then fixes the mass flow, the suction specific volume
fixes the swept volume, and the compressor work divided by the drive efficiency
gives the electrical demand to be priced.
Problem 4: the vapour-compression heat pump. Ground water at 4 °C feeds the evaporator; the condenser is the heater battery in the supply-air duct.
Fix the two saturation temperatures. The evaporator must sit
14 K below the ground water for heat to cross:
$$t_{1} = t_{w} - \Delta t = 4 - 14 = -10\ ^\circ\text{C}
\quad\Longrightarrow\quad p_{1} = 200.6\ \text{kPa}$$
and the delivery pressure is the condensing pressure, which for R-134a
corresponds to
$$p_{2} = 1.0164\ \text{MPa} \quad\Longrightarrow\quad
t_{\text{cond}} = 40.0\ ^\circ\text{C}$$
That the stated pressure lands exactly on a round 40 °C is the
paper's way of confirming the reading; a condensing temperature 5 K
above the 35 °C air leaving the coil is also physically necessary, so
the data are self-consistent.
Read the four cycle states. State 1 is dry saturated vapour
at $-10\ ^\circ\text{C}$; 1–2 is isentropic compression to 1.0164 MPa;
state 3 is saturated liquid at 40 °C because there is no undercooling;
and 3–4 is a throttle at constant enthalpy.
Cycle state points (IIR datum: h = 200 kJ/kg for saturated liquid at 0 °C)
State
Condition
p, MPa
t, °C
h, kJ/kg
s, kJ/kg·K
1
dry saturated vapour
0.2006
-10.0
392.7
1.7334
2
superheated discharge
1.0164
46.3
426.5
1.7334
3
saturated liquid
1.0164
40.0
256.4
1.1900
4
wet, after the throttle
0.2006
-10.0
256.4
dryness 0.338
The suction specific volume, needed in part (c), is
$v_{1} = 0.09959\ \text{m}^{3}/\text{kg}$.
Part (a) — the coefficient of performance. For a heat
pump the useful output is the condenser duty and the input is the compression
work:
$$\text{COP}_{hp} = \frac{h_{2} - h_{3}}{h_{2} - h_{1}}
= \frac{426.5 - 256.4}{426.5 - 392.7} = \frac{170.08}{33.81}
= \boxed{5.03}$$
As a sanity check the reversed-Carnot limit between the same two saturation
temperatures is
$T_{\text{cond}}/(T_{\text{cond}} - T_{\text{evap}}) = 313.15/50 = 6.26$, so the
cycle achieves 80 % of the ideal — high, but that is what a
throttle-only, no-superheat cycle over a 50 K lift should give.
Get the air-side duty the condenser has to meet. The
volume flow is quoted at the delivery state, so the density is evaluated there:
$$\rho = \frac{p}{R\,T} = \frac{101\,325}{287.0 \times 308.15}
= 1.1455\ \text{kg/m}^{3},\qquad
\dot{m}_{a} = 0.8 \times 1.1455 = 0.9164\ \text{kg/s}$$
$$\dot{Q}_{\text{cond}} = \dot{m}_{a}\,c_{p}\,(t_{\text{out}} - t_{\text{in}})
= 0.9164 \times 1.005 \times (35 - 6) = \boxed{26.71\ \text{kW}}$$
If instead the 0.8 m³/s were read at the 6 °C inlet the duty
would be 29.5 kW, 10 % higher; the delivery reading is taken because
the question states the air is delivered at 35 °C at that
rate.
Part (b) — refrigerant mass flow. Every kilogram of
refrigerant rejects $h_{2} - h_{3}$ in the condenser, so
$$\dot{m}_{r} = \frac{\dot{Q}_{\text{cond}}}{h_{2} - h_{3}}
= \frac{26.71}{170.08} = \boxed{0.157\ \text{kg/s}} \;(9.42\ \text{kg/min})$$
Part (c) — swept volume of the compressor. The
volumetric efficiency relates the induced volume to the volume swept per
revolution; single acting means one induction stroke per revolution:
$$\dot{V}_{1} = \dot{m}_{r}\,v_{1} = 0.157 \times 0.09959
= 0.01564\ \text{m}^{3}/\text{s}$$
$$V_{\text{swept}} = \frac{\dot{V}_{1}}{\eta_{\text{vol}}\,(N/60)}
= \frac{0.01564}{0.85 \times 5.0} = 3.680 \times 10^{-3}\ \text{m}^{3}
= \boxed{3{,}680\ \text{cm}^{3}}$$
A 3.7 litre displacement is large, but at only 300 rev/min it is what
a slow-speed reciprocating machine of this duty needs — for reference,
a bore and stroke of about 165 mm on a single cylinder.
Part (d) — the running cost. The shaft work follows
from the same mass flow, and the drive efficiency converts it to electrical
demand:
$$\dot{W}_{\text{shaft}} = \dot{m}_{r}\,(h_{2} - h_{1})
= 0.157 \times 33.81 = 5.31\ \text{kW}, \qquad
\dot{W}_{\text{elec}} = \frac{5.31}{0.87} = 6.10\ \text{kW}$$
$$\text{cost}_{hp} = 6.10\ \text{kW} \times 0.10\ \frac{\$}{\text{kWh}}
\times 1\ \text{h} = \boxed{\$0.61\ \text{per hour}}$$
Part (d) — compare with electric radiators, and comment.
Resistance heating delivers the same 26.71 kW of heat for 26.71 kW of
electricity:
$$\text{cost}_{\text{resistance}} = 26.71 \times 0.10
= \boxed{\$2.67\ \text{per hour}}$$
so the heat pump saves $2.06 per hour, 77 % of the bill, and the
comparison is properly made on the overall coefficient of performance
$\dot{Q}/\dot{W}_{\text{elec}} = 26.71/6.10 = 4.38$, not the 5.03 of the
refrigeration cycle alone — the drive losses are real and have to be
carried. Three qualifications belong with that number. First, it is an
instantaneous figure at one operating point; a seasonal average is lower,
because the load falls as the source stays fixed and the machine cycles.
Second, the advantage here rests on a ground-water source at a steady
4 °C, which is exactly why ground-coupled machines are specified in
Canadian climates: an air-source unit at a Canadian heating design temperature
would be operating near its low-ambient cut-out with resistance back-up carrying
the coldest hours at a COP of 1. Third, the capital cost of the well, the
ground loop and a 3.7 litre compressor is very much larger than that of
radiators, so the economic case is a life-cycle one; at a saving of
$2.06 per hour of full-load operation and, say, 2,000 equivalent
full-load hours a year, the annual saving is about $4,100 and a simple
payback follows directly from the installed-cost difference. On the
environmental side the answer depends on the grid: on the largely hydro-electric
grids of British Columbia, Manitoba and Quebec the heat pump is unambiguously
better on both energy and carbon, whereas on a fossil-heavy grid the primary
energy comparison has to include the generating and transmission efficiency
before the same conclusion can be drawn.
[Figure not reproduced: Problem 4: the cycle on the R-134a p-h diagram appended to the examination paper. 1-2 is isentropic compression, 2-3 de-superheating and condensation with no undercooling, 3-4 the throttle, 4-1 evaporation to dry saturated vapour. See the official exam paper.]