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Katena32 [7]
3 years ago
9

15. A cold-chamber die-casting machine operates automatically, supported by two industrial robots.The machine produces two zinc

castings per cycle. One robot ladles molten metal into the chamber each cycle, and the other unloads the two castings from the machine and sprays lubricant onto the die cavities. Cycle time = 0.85 min. Each casting weighs 0.75 lbm, and the gating system weighs 0.40 lbm. The gating system can be recycled to cast more parts. Die cost = $45,000. The total production run = 200,000 pc. Scrap rate = 3%. Assume reliability = 100%. Cost of zinc = $1.05/lbm. Melting temperature of zinc = 787F. Its density = 0.258 lbm/in3 , heat of fusion = 49 Btu/lbm, and specific heat = 0.091 Btu/lbmF (use the same values of density and specific heat for solid and molten zinc). Pouring temperature = 860F. Heat losses account for 35% of the energy used to heat the metal. Cost of power for heating = $0.15/kWh. The cost rate of the die casting machine = $57/hr, and the cost rate of each robot = $18/hr. As part of the operation sequence, the casting is trimmed from the gating system, which is done manually at a labor rate of $20.00/hr. The worker recycles the zinc from the gating system for remelting. Determine (a) unit energy for melting and pouring, (b) total cost per hour to operate the cell, and (c) cost per part

Engineering
2 answers:
MAVERICK [17]3 years ago
5 0

Answer:

a) The unit energy for melting and pouring is 121 Btu/lb

b) The total cost per hour is 368.31/h

c) The cost per part is 2.7/pc

Explanation:

a) The unit energy for melting and pouring is:

U=C_{p} (T_{m,Zn} -T_{0} )+deltaH_{fus}+C_{p}  (T_{p}- T_{0})

If we assume that the surrounding temperature is 70°F

U=0.091(787-70)+49+0.091(860-787)=121Btu/lb

b) The hourly production is:

R=(\frac{number-of-castings}{t_{cycle} } )*(1-scrap-rate)\\R=(\frac{2}{0.85min} *\frac{60min}{1h} )*(1-0.03)=136.9good-parts/h

The total weight of zinc is:

W_{total} =(\frac{number-of-castings}{t_{cycle} } )*(2*weight-of-casting)\\R=(\frac{2}{0.85min} *\frac{60min}{1h} )*(2*0.75)=211.8lb

The total cost of zinc is:

C=W_{total} *cost-of-zinc=211.8*1.05=222.3 $

The total heat transfer is:

Q=(\frac{number-of-castings}{t_{cycle} } )*((2*weight-of-casting)+gating-system-weight)*U\\Q=(\frac{2}{0.85min} *\frac{60min}{1h} )*((2*0.75)+0.4))*121=32462Btu/h=541Btu/min

541 Btu/min = 9.51 kW

The power is:

Power=\frac{Q}{1-Q_{loss} } =\frac{9.51}{1-0.35} =14.6kW

The hourly cost is:

C_{H} =P*cost-of-power-for-heating=14.6*0.15=2.2/h

The cost for die casting is:

C_{d} =cost-rate-of-die-casting+(2*cost-of-each-robot)=57+(2*18)=93/h

The die cost per casting is:

C_{die,casting} =\frac{45000}{200000} =0.225/pc

The hourly rate is:

Hourly-rate=R*C_{d,casting} =136.9*0.225=30.81/h

The total cost per hour is:

C_{total} =C+C_{H} +C_{d} +C_{1} +Hourly-time=222.35+2.2+93+20+30.81=368.31/h

c) The cost per part is:

C_{per part} =\frac{C_{total} }{R} =\frac{368.36}{136.9} =2.7/pc

Softa [21]3 years ago
4 0

Answer:

a. 121 Btu/lb

b. 211.8lb

c. 2.69/pc

Explanation:

See the attachments please

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Astronauts who landed on the moon during the Apollo 15, 16, and 17 missions brought back a large collection of rocks to the eart
stiks02 [169]

Answer: a) W(earth) = 935.62 lbs

b) Mass of rocks in slugs = 29.06 slugs

Explanation:

a) From Newton's law, W = mg. Whether on the moon or on earth. Although, the mass of the rocks everywhere is the same, that is, mass of rocks on the moon = mass of rocks on earth.

W(moon) = mg(moon)

W(moon) = 154 lbs

g(moon) = 5.30 ft/s2

m = W(moon)/g(moon) = 154/5.3 = 29.06 lb.s2/ft

W(earth) = m g(earth)

g(earth) = 32.2 ft/s2

W(earth) = 29.06 × 32.2 = 935.62 lbs.

b) A slug = 1 lb.s2/ft, therefore the mass of the rocks in slugs is 29.06 slugs.

QED!

8 0
3 years ago
An ideal vapor-compression refrigeration cycle that uses refrigerant-134a as its working fluid maintains a condenser at 800 kPa
mote1985 [20]

Answer:

COP = 3.828

W' = 39.18 Kw

Explanation:

From the table A-11 i attached, we can find the entropy for the state 1 at -20°C.

h1 = 238.43 KJ/Kg

s1 = 0.94575 KJ/Kg.K

From table A-12 attached we can do the same for states 3 and 4 but just enthalpy at 800 KPa.

h3 = h4 = hf = 95.47 KJ/Kg

For state 2, we can calculate the enthalpy from table A-13 attached using interpolation at 800 KPa and the condition s2 = s1. We have;

h2 = 275.75 KJ/Kg

The power would be determined from the energy balance in state 1-2 where the mass flow rate will be expressed through the energy balance in state 4-1.

W' = m'(h2 - h1)

W' = Q'_L((h2 - h1)/(h1 - h4))

Where Q'_L = 150 kW

Plugging in the relevant values, we have;

W' = 150((275.75 - 238.43)/(238.43 - 95.47))

W' = 39.18 Kw

Formula foe COP is;

COP = Q'_L/W'

COP = 150/39.18

COP = 3.828

4 0
3 years ago
Determine the speed of sound in air at 400 K. Also determine the Mach number of an aircraft moving in the air at a velocity of 3
Reika [66]

Answer:

\alpha = \sqrt{1.4 *0.287 \frac{KJ}{Kg K}*\frac{1000J}{1KJ} *400 K}= 400.899 m/s

Ma= \frac{310 m/s}{400.899 m/s}= 0.773

Explanation:

For this case we have given the following data:

T= 400 K represent the temperature for the air

v = 310 m/s represent the velocity of the air

k = 1.4 represent the specific heat ratio at the room

R = 0.287 KJ/ Kg K represent the gas constant  for the air

And we want to find the velocity of the air under these conditions.

We can calculate the spped of the sound with the Newton-Laplace Equation given by this equation:

\alpha = \sqrt{\frac{K}{\rho}}=\sqrt{k RT}

Where K = is the Bulk Modulus of air, k is the adiabatic index of air= 1.4, R = the gas constant  for the air, \rho the density of the air and T the temperature in K

So on this case we can replace and we got:

\alpha = \sqrt{1.4 *0.287 \frac{KJ}{Kg K}*\frac{1000J}{1KJ} *400 K}= 400.899 m/s

The Mach number by definition is "a dimensionless quantity representing the ratio of flow velocity past a boundary to the local speed of sound" and is defined as:

Ma=\frac{v}{\alpha}

Where v is the flow velocity and \alpha the volocity of the sound in the medium and if we replace we got:

Ma= \frac{310 m/s}{400.899 m/s}= 0.773

And since the Ma<0.8 we can classify the regime as subsonic.

7 0
3 years ago
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