001


Chapter 1

AN APPROACH TO MINE VENTILATION BASED ON THE AERODYNAMIC POTENTIAL OF VENTILATING AIR TREATED AS A MIXTURE OF DRY AIR, WATER VAPOUR AND LIQUID WATER DROPLETS

H. Bystroń

Central Mining Institute, Katowice, Poland

ABSTRACT

The purpose of the paper was to verify an approach to mine ventilation based on the aerodynamic potential when adopting the thermodynamic approach by Barenbrug (Barenbrug, 1974) as a criterion of truth. The conformity of energy and power balances in both approaches has been ascertained. Nevertheless, there considerable differences occurred between energies and powers lost to remove water vapour. The cause of these differences is explained.

KEYWORDS

Aerodynamic potential, local and main natural ventilating energies, lost energies and powers, energy and power balances for ventilation system


INTRODUCTION

The purpose of the paper was the verification of an approach to mine ventilation based on the aerodynamic potential when adopting a thermodynamic approach (Barenbrug, 1974) as a criterion of truth. On this way it is possible to verify the formula, by the use of which the mechanical energy expended to achieve the removal of water vapour has been determined. This is motivated by the need of economical yet safe mine ventilation.

AERODYNAMIC POTENTIAL OF VENTILATING AIR TREATED AS A MIXTURE

The aerodynamic potential, , J/(kg dry air), is determined by the formula (Bystroń, 2000 b, c):

0x01 graphic
(1)

where: p, Pa, * corrected pressure; ps, Pa, and vas, m3/(kg dry air) - pressure and apparent specific volume in the isentropic flow, determined respectively by use of the following formulae:

0x01 graphic
, 0x01 graphic
(2), (3)

0x01 graphic
(4)

where: subscript )1 indicates, that the given quantity concerns the cross-section 1 of the top of the downcast shaft; = 1.4 - the isentropic exponent; g, m/s2 - local gravitational acceleration; z, m, - elevation above sea level; w, m/s - average velocity; va, m3/(kg dry air) and X, kg/(kg dry air) - apparent specific volume in the polytropic flow and moisture content respectively - determined by the following formulae (Hemp, 1989; Mc. Pherson, 1993):

0x01 graphic
, 0x01 graphic
(5), (6)

0x01 graphic
(7)

In accordance with the defined aims of the paper, we start from the measured parameters: elevation, z, m, corrected pressure, p, Pa, and the dry-bulb and wet-bulb temperatures of ventilating air, t, t', 0C - respectively (Table 1) with reference to 20 measuring stations (Figure 1) and gravitational acceleration, g = 9.79 m/s2 - taken from the thermodynamic approach (Barenbrug, 1974).

Using the appropriate data from the Table 1, we calculate by use of the formulae (1) to (7) respectively the aerodynamic potential, , and the parameters: pp, X, va, W, ps, vas and , (Table 1) concerning the measuring stations from 1 to 20 in the ventilation system (Figure 1).

0x01 graphic

Figure 1. Line diagram of the mine ventilation system

DROP OF THE AERODYNAMIC POTENTIAL, MASS OF LIQUID WATER DROPLETS AND TECHNICAL WORKS IN THE POLYTROPIC AND ISENTROPIC FLOWS

The drop of the aerodynamic potential, δ, J/(kg dry air), in the branch d-w of the ventilation system is determined by the formula:

δ = d * w (8)

where the subscripts )d and )w indicate, that the given quantity (parameter) concerns the inflow cross-section d and outflow cross-section w respectively of the branch d-w.

The mass of liquid water droplets, mW, kg/(kg dry air), is determined by use of the formula (Ochęduszko, 1974):

mW = Xd * Xw (9)

in which the condition Xd > Xw is sustained.


Table 1. Parameters of ventilating air at measuring stations (Figure 1)

Sta-tion

Corrected

Temperatures

Elevation above sea level

Partial water vapour pressure

Moisture
content

Apparent specific volume

Numerical quantity

Pres-sure

Apparent specific volume

Aero-dynamic potential

pressure

Dry-bulb

Wet-bulb

in the polytropic flow

in isentropic

flow

p

t

t'

z

pp

X

va

W

ps

vas

No.

Pa

0C

0C

m

Pa

kg/kg d. air

m3/kg d. air

-

Pa

m3/kg d.air

J/kg d. air

1

84,193

25.8

14.7

1,575.8

1,070

0.008006

1.032333

1.000000

84,193

1.032333

0

2

99,254

22.6

21.0

112.8

2,384

0.015303

0.876346

1.047460

99,028

0.919341

208

3

100,426

22.5

21.5

9.6

2,498

0.015869

0.866594

1.050808

100,140

0.912036

261

4

98,831

25.9

25.5

116.3

3,236

0.021056

0.897950

1.047346

98,990

0.919590

-146

5

98,831

22.6

21.8

116.3

2,560

0.016537

0.881800

1.047346

98,990

0.919590

-146

6

98,831

24.2

23.7

116.3

2,897

0.018784

0.889691

1.047346

98,990

0.919590

-146

7

95,519

26.7

26.0

360.0

3,317

0.022373

0.933480

1.039441

96,400

0.937175

-825

8

93,724

27.8

27.2

365.2

3,569

0.024625

0.958184

1.039272

96,345

0.937555

-2,457

9

84,000

25.6

14.7

1,595.9

1,082

0.008118

1.034196

0.999348

84,001

1.034018

-1

10

98,763

21.0

20.8

126.2

2,443

0.015773

0.876584

1.047025

98,884

0.920295

-111

11

99,941

21.5

21.3

22.0

2,519

0.016082

0.868145

1.050405

100,006

0.912909

-59

12

98,146

26.6

26.4

128.9

3,427

0.022506

0.908378

1.046938

98,855

0.920488

-653

13

98,146

21.4

21.3

128.9

2,526

0.016428

0.884201

1.046938

98,855

0.920488

-653

14

98,146

24.0

23.9

128.9

2,958

0.019330

0.896060

1.046938

98,855

0.920488

-653

15

95,034

26.6

25.4

361.2

3,169

0.021455

0.936594

1.039402

96,387

0.937263

-1,268

16

93,724

27.4

26.3

365.2

3,353

0.023080

0.954624

1.039272

96,345

0.937555

-2,457

17

93,724

27.6

26.8

365.2

3,474

0.023939

0.956532

1.039272

96,345

0.937555

-2,457

18

81,362

22.2

22.2

1,576.7

2,675

0.021144

1.077399

0.999971

84,184

1.032409

-2,914

19

84,184

23.4

23.4

1576.7

2,877

0.022006

1.046914

0.999971

84,184

1.032409

0

20

84,184

25.7

14.7

1576.7

1,076

0.008049

1.032168

0.999971

84,184

1.032409

0

Table 2. Parameters of ventilating air in branches and meshes: 1, 2 , 3 and 4 of ventilation system (Figure 1)

Branch

Aerody-namic

Mass of liquid

Polytropic

Technical work

in flow

Local na-tural ven-

Energy lost to remove:

Usable energy

Frictional

Mass flow

Aerody-namic

potential drop

water droplets

exponent

polytro-
pic

isentro-
pic

tilating energy

water vapour

liquid water droplets

of fan station

energy loss

of dry air

resistance

-

δ

mW

n

lt

lts

en

lP

lW

eu

qf

0x01 graphic

R

d * w

J/kg d. air

kg/kg d. air

-

J/kg d. air

J/kg d. air

J/kg d. air

J/kg d. air

J/kg d. air

J/kg d. air

J/kg d. air

kg d. air/s

m2/kg2 d. air

1-2

-208

0

1.004608

-14,309

-14,645

336

-52

0

0

180

241

0.003099

2-3

-53

0

1.048977

-1,021

-1,071

50

-8

0

0

5

120

0.000347

2-5

354

0

0.688371

372

389

-17

0

0

0

343

121

0.023427

3-4

407

0

0.450415

1,407

1,460

-53

11

0

0

340

120

0.023611

6-7

679

0

0.709469

3,018

3,086

-68

30

0

0

581

241

0.010003

7-8

1,632

0

0.726281

1,698

1,704

-6

1

0

0

1,625

241

0.027978

9-10

110

0

0.979191

-14,041

-14,393

352

-57

0

0

519

195

0.013649

10-11

-52

0

1.225708

-1,027

-1,080

53

-8

0

0

9

94

0.001019

10-13

542

0

0.724296

543

570

-27

0

0

0

515

101

0.050485

11-12

594

0

0.400072

1,594

1,650

-56

12

0

0

526

94

0.059529

14-15

615

0

0.728289

2,851

2,912

-61

28

0

0

526

195

0.013833

15-16

1,189

0

0.727989

1,239

1,246

-7

1

0

0

1,181

195

0.031059

17-18

457

0.002795

1.188712

12,539

12,424

115

156

17

0

399

436

0.002099

18-19

-2,914

0

1.187903

-2,997

-2,949

-48

0

0

2,997

35

436

0.000184

20-1

0

0

-0.666995

-9

-9

0

0

0

0

0

0

0

20-9

1

0.000069

1.114825

190

190

0

0

0

0

1

0

0

Mesh 1 (1,2,5,6,7,8,17,18,19,20,1): 0

312

0

312

135

17

2,997

3,157

436

0.017407

Mesh 2 (1,2,3,4,6,7,8,17,18,19,20,1): 0

326

0

326

138

17

2,997

3,168

436

0.017481

Mesh 3 (9,10,13,14,15,16,17,18,19,20,9): 0

324

0

324

128

17

2,997

3,176

436

0.017470

Mesh 4 (9,10,11,12,14,15,16,17,18,19,20,9): 0

348

0

348

132

17

2,997

3,196

436

0.017596


Both technical works in the polytropic flow, lt, and in the isentropic flow, lts, J/(kg dry air), are determined respectively by the formulae (Bystroń, 2000 c):

0x01 graphic
(10)

0x01 graphic
(11)

where n - polytropic exponent:

0x01 graphic
(12)

Using the data from the Table 1, respectively, we have calculated by the use of the formulae (8) to (12) the parameters δ, mW , n, lt and lts (Table 2) concerning the branches d-w of the ventilation system (Figure 1).

MECHANICAL ENERGY LOSSES, USABLE ENERGY OF the FAN STATION

The local natural ventilating energy, en, J/(kg dry air ), generated in the branch d-w, is determined by:

en = lt * lts (13)

Both mechanical energies, lW , lP, J/(kg dry air), lost to remove liquid water droplets and water vapour are determined by use of the following formulae (Bystroń, 2000 b, c):

− in case of a downcast shaft or dip-heading (0x01 graphic
)

0x01 graphic
(14)

0x01 graphic
(15)

− in case of a up-cast shaft or incline (0x01 graphic
)

0x01 graphic
   (16)

0x01 graphic
(17)

The usable energy, eu, J/(kg dry air ), of the fan station d-w is determined by the formula:

0x01 graphic

(18)

The frictional mechanical energy loss, 0x01 graphic
, J/(kg dry air), in the branch d-w with (eu > 0) or without the fan station (eu = 0), is given by the formula:

0x01 graphic
= δ + en * lP * lW + eu (19)

Using the appropriate data from Tables 1 and 2, we have calculated the parameters en, lW, lP, eu and qf respectively, by use of the formulae (13) to (19)
(Table 2).

The aerodynamic resistance, R, m2/(kg2 dry air), of the branch d-w of the ventilation system is determined by:

0x01 graphic
(20)

where 0x01 graphic
, (kg dry air)/s, - mass flow along the branch. The aerodynamic resistance, R, m2/(kg2 dry air), of the mesh enclosing the surface atmosphere is determined by equivalent formulae:

0x01 graphic
(21), (22)

where , (kg dry air)/s - mass flow through the main fan station.

In Table 2 are specified mass flows, 0x01 graphic
, (kg dry air)/s, (Barenbrug, 1974) as well as aerodynamic resistances, R, of branches or meshes - calculated respectively by use of the formulae (20) and (21) or (20) and (22).

MAIN NATURAL VENTILATING ENERGY, RESULTANT CHARACTERISTICS OF THE VENTILATION SYSTEM

The natural ventilating energy, , J/(kg dry air), generated in the mesh j containing the surface atmosphere is determined by the expression:

= , i = 1,2,...,Nj

where: i - number of the branch d-w, Nj - amount of all branches in the mesh j.

The main natural ventilating energy, , J/(kg dry air), in a mine ventilation subsystem or a system with one fan station is determined by the expression (Bystroń, 2000 a):

= , j = 1,2,...,M (23)

where: M -the number of all meshes j. On the basis of Table 2 and expression (23) we record for the ventilation system (Figure 1):

= (312, 326, 324, 348) =

= 312 J/(kg dry air ) (24)

0x01 graphic

Figure 2. Resultant characteristics of network and characteristics of main natural ventilating energy, 0x01 graphic
=
= idem = 312 in the ventilation system (Figure 1)

The mesh, in which the main natural ventilating energy is generated, is termed the main mesh of the ventilation system. The aerodynamic resistance of the main mesh, R, m2/(kg2 dry air), is determined by the expression:

, j = 1, 2,..., M (25)

On the basis of Table 2 and expression (25) we record for the ventilation system (Figure 1):

(0.017407, 0.017481, 0.017470, 0.017596) =

= 0.017407 m2/(kg2 dry air) (26)

The aerodynamic resistance of the main mesh is the resistance of the ventilation system.

The equation of the resultant characteristics of the ventilation network as the element of the ventilation system (Figure 1) has the form (Bystroń, 2000 b):

(27)

where: , (kg dry air)/s - mass flow of dry air, R, m2/(kg2 dry air), - aerodynamic resistance determined by (26).

In Figure 2 are plotted the characteristics of the main natural ventilating energy as described by the equation:

= idem = 312 J/(kg dry air) (28)

and the resultant characteristics of the ventilation network by the equation (27), where the point R (Figure 2) of the equilibrium of the ventilation system (Figure 1) is determined by the co-ordinates: : = 436 (kg dry air)/s , euR = eu = 2,997 J/(kg dry air).

In Figure 3 are plotted: isentrope 1-2s described by the equation0x01 graphic
, where p1 = 84,193 Pa, 0x01 graphic
= 1.032333 m3/(kg dry air) (Table 1) and the natural ventilating energy: local = 336 and main = 312 J/(kg dry air) (Table 2).

ENERGY BALANCE

The energy balances both for the ventilation system and for the main mesh 1 (1,2,5,6,7,8,17,18,19,20,1) (Figure 1) are exactly the same. In the fourth line down from the top of Table 2 the elements of these balances expressed in J/(kg dry air) are given; namely:

The sum of available energies, eu + = 3,309, is equal to the sum of lost mechanical energies, = 3,309. Thus the energy balance: eu + =

is exactly satisfied.

0x01 graphic

Figure 3. Local natural ventilating energy, 0x01 graphic
= 336, in the branch 1-2 and main natural ventilating energy, 0x01 graphic
= 312, in the ventilation system (Figure 1)

Table 3. Comparison of energy balances for the ventilation system (Figure 1)

Approach to mine ventilation:

Barenbrug

Author

Differ-rence,

per cent

Usable energy of fan station, eu

2,998

2,997

- 0.03

Main natural ventilating energy, 0x01 graphic

311

312

0.32

Sum of usable energies, eu + 0x01 graphic

3,309

3,309

0.00

Frictional loss of mechanical energy,
0x01 graphic

3,141

3,157

0.51

Mechanical energies lost to remove:
- water vapour, 0x01 graphic

(151)

135

-10.60

- liquid water droplets, 0x01 graphic

(17)

17

0.00

Sum of these energies,

0x01 graphic

168

152

- 9.52

Sum of lost mechanical energies,

0x01 graphic

3,309

3,309

0.00

In Table 3 the energy balances determined in the thermodynamic approach (Barenbrug, 1974) and the author's approach based on the above-mentioned aerodynamic potential are presented. These balances are identic. Nevertheless, there occur the considerable differences between the following elements of these balances, i. e. between:

We underline, that the energies = (151) and = (17) (Table 3) have not been given in the above-mentioned Barenbrug's work, but they have been presented in the work (Hemp, 1986).

POWER BALANCE

The usable power, Nn, of the local natural ventilating energy and the usable power, Nu, of the main fan station, the frictional power loss, Nf, the powers, NP and NW, lost to remove water vapour and liquid water droplets - expressed in W - are determined respectively by use of the formulae (Barenbrug, 1974):

0x01 graphic
,0x01 graphic
,

which concern the branches d-w of the ventilation system (Figure 1) with adequate parameters: en, lP, lW, qf and eu as well as with the mass flow , (kg dry air)/s.

Using the Figure 1, the appropriate data from the Table 2 and the above-mentioned formulae we have calculated the powers specified in Table 4. In the lines from 2 to 5 from below of this table the following sums of powers are specified concerning the meshes from 1 to 4 of the ventilation system (Figure 1).

In the last line of Table 4 the elements of the power balance for this ventilation system, expressed in kW, are given; namely:

The sum of usable power, Nu + = 1,448.805 is equal to the sum of lost powers 0x01 graphic
NW ) =
= 1,448.805. Thus the power balance:

Nu + =

is exactly in equilibrium.

Table 4. Power balance for the ventilation system (Figure 1)

Branch

Power of local nat.

Power lost
to remove:

Frictional

Usable power

ventilating energy

Water vapour

Liquid water droplets

power loss

of fan station

d-w

Nn

NP

NW

Nf

Nu

1-2

80.976

-12.532

0

43.380

0

2-3

6.000

-0.960

0

0.600

0

2-5

-2.057

0

0

40.777

0

3-4

-6.360

1.320

0

41.160

0

6-7

-16.388

7.230

0

140.021

0

7-8

-1.446

0.241

0

391.625

0

9-10

68.640

-11.115

0

101.205

0

10-11

4.982

-0.752

0

0.846

0

10-13

-2.727

0

0

52.015

0

11-12

-5.264

1.128

0

49.444

0

14-15

-12.090

5.460

0

102.570

0

15-16

-1.365

0.195

0

230.295

0

17-18

50.140

68.016

7.412

173.964

0

18-19

-20.928

0

0

15.260

1306.692

20-1

0

0

0

0

0

20-9

0

0

0

0.195

0

Mesh 1:

90.297

62.955

7.412

805.027

1,306.692

Mesh 2:

91.994

56.085

7.412

806.010

1,306.692

Mesh 3:

81.670

62.556

7.412

675.504

1,306.692

Mesh 4:

84.115

62.932

7.412

673.779

1,306.692

System:

142.113

58.231

7.412

1,383.162

1,306.692

In Table 5 the power balances and their component elements as determined by the thermodynamic approach (Barenbrug, 1974) and the author's approach based on the aerodynamic potential are given. These balances are identical in practice.

Nevertheless, considerable differences occur between the following elements of these balances, i. e. between:

We stress, that the powers = (65.088) and = (7.412) (Table 5) have not been given in the work (Barenbrug, 1974). Based on Tables 3, 4 and 5 we have: = (7.412) and =0x01 graphic
+
+ NW) - = 72.5 - (7.412) = (65.088).

Table 5. Comparison of power balances for the ventilation system (Figure 1)

Approach to mine ventilation:

Baren-brug

Author

Differ-rence,

per cent

Usable power of fan station, Nu

1,307.1

1,306.692

0.03

Power of main natural ventilating

energy, Nn

141.8

142.113

0.22

Sum of usable powers, Nu + Nn

1,448.9

1,448.805

- 0.01

Sum of frictional power losses, 0x01 graphic

1,376.4

1,383.162

0.49

Sum of power lost to remove:
- water vapour, 0x01 graphic

(65.088)

58.231

-10.53

- liquid water droplets, 0x01 graphic

(7.412)

7.412

0.00

Sum of both lost powers, 0x01 graphic

72.5

65.643

- 9.46

Sum of all lost powers,

0x01 graphic

1,448.9

1,448.805

- 0.01

ADDITIONAL QUESTIONS AND CONCLUSIONS

In order to recognise the reason for the appearance of the considerable above-mentioned differences we present the following consideration:

In case of the approach based on the aerodynamic potential - acting in accordance with the work (Bystroń, 2000 b) - we proceed from the relationship:

0x01 graphic
0x01 graphic

0x01 graphic

(Ochęduszko, 1974). When performing the necessary transformations we obtain:

0x01 graphic
(29), (30)

From matching both relations (29) and (30), the expression 0x01 graphic
(where 0x01 graphic
, J/kg,) and the equation of motion 0x01 graphic
results the following form of the last equation:

0x01 graphic
(31)

Dividing both sides by the following form of Poisson's equation: 0x01 graphic
0x01 graphic
, we derive the expression 0x01 graphic
. Comparison of the right side of this expression and relationship (30) results in:

0x01 graphic

From this relationship and the equation of energy for the isentropic flow: 0x01 graphic
, we obtain:

0x01 graphic
(32)

As a result of subtraction by sides of the following equation of local natural ventilating energy: den +
+ va dp * vas dp = 0 from the equation of motion (31) we have:

0x01 graphic
(33)

Subtracting equation (32) from equation (33) and matching of the expression obtained with the equation: d = vas (dp * dps ), we obtain (Bystroń 2000 b):

0x01 graphic

The first element of the right side of this equation we equate to the sum (dlP + dlW). This results in:

dlP + dlW 0x01 graphic
(34)

In case of a downcast shaft or dip-heading (zd zw) - where, in accordance with the classical theory (Ochęduszko, 1974), water vapour condensation does not take place - one obtains lW = 0, dlW = 0 (Barenbrug, 1974, Hemp, 1989). From the integration of the equation (34) assuming that dlW = 0 formula (15) results.

In case of a upcast shaft or incline (zd < zw) we rearrange the first factor of the right side of equation (34) as follows:

0x01 graphic

On the basis of this expression, formula (9) and equation (34), as well as on the basis of the above-mentioned theory, we can write:

0x01 graphic
,

0x01 graphic

The integrals of these equations are formulae (16) and (17) respectively.

In case of the thermodynamic approach (Barenbrug, 1974) on the basis of the work (Hemp, 1989) and relation: a = 0x01 graphic
(Xd * Xw ) and r = X , we obtain:

0x01 graphic
(35)

0x01 graphic
(36)

If we assume, that the ventilating air velocities are negligibly low, wd = 0, ww = 0, then from formula (16) will result (36). This does not influence formulae (15), (17) and (35).

According to the above consideration we conclude, that expression (35) is the reason for the above-
-mentioned considerable differences between energies and powers expended to remove water vapour as well as water vapour and liquid water droplets.

This work was sponsored by the Committee
of Scientific Research, Warsaw

REFERENCES

Barenbrug, A. W. T.,1974, ”The Thermodynamic Approach to Mine Ventilation,” Chapter 12. The Ventilation of South African Gold Mines. Mine Vent. Soc. of South Africa. Cape Town, pp. 244-265

Bystroń, H., 2000 a, ”The Main and Booster Natural Ventilating Energies in the Mine Ventilation Network,” (in Polish), Archives of Mining Sciences, Vol. 45, No 2, pp. 171-198

Bystroń, H., 2000 b, “ Aerodynamic Potential of Ventilating Air in Difficult Thermic Condition Mine,” (in Polish), Przegląd Górniczy, No 10, pp. 1-11

Bystroń, H., 2000 c, “Basic Parameters of Ventilation Subsystem in the Light of Aerodynamic Potential and Assumptions Concerning Ventilating Air,” (in Polish), Mechanizacja i Automatyzacja Górnictwa, No 11, pp. 5-17

Hemp, R., 1989, “The Thermodynamic Aspects of Mine Airflow,” Chapter 2. Environmental Engineering in South African Mines. The Mine Vent. Soc. of South Africa, pp. 29-48

McPherson, M. J., 1993, “Mine Ventilation Thermodynamics,” Chapter 8. Subsurface Ventilation and Environmental Engineering. Chapman & Hall, London, pp. 241-281

Ochęduszko, S., 1974, “Moist Gases,” Chapter 29. Applied Thermodynamics (in Polish). Wydaw. Nauk. Techn., Warsaw, pp. 266-278

2

I SZKOŁA AEROLOGII GÓRNICZEJ 1999

5

8

PROCEEDINGS OF THE 7TH INTERNATIONAL MINE VENTILATION CONGRESS

7

AN APPROACH TO MINE VENTILATION BASED ON THE AERODYNAMIC



Wyszukiwarka

Podobne podstrony:
001 Istota Marketingu i otoczenie
3616 001
001
2980 001
I wojna swiatowa i Rosja 001
001
gruzlica 001
BVSOI 3 001 E en
1119155152 001
P27 001
2012 11 22 Document 001
Access to History 001 Gas Attack! The Canadians at Ypres, 1915
0718 001
p08 001
Ir 1 (R 1) 001 002 Okładka
001 prawo
001
Kr 001 Dwa podstawowe modele
2977 001

więcej podobnych podstron