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Work procedure

1. Check water-level in feed-tank 9 (Fig. 6.2) by calibrating tube 10 and, if necessary, refill it.

2. Set a steady-state regime of the pump with partly opening of throttle 7.

3. Measure vacuum PV and pressure PM.

4. Measure time T of calibrating tank 8 being filling.

5. Measure a torque and determine the power at the motor shaft.

6. Put all results of measurement and calculations in table 6.1.

7. Increase pump discharge and follow instructions of items 1, 2, 3, 4 for each position.

8. Determine values , Q, .

9. Plot diagrams HP=(Q), P=(Q), using the received data.

Table 6.1

Number of measurement

1

2

3

4

5

Time for calibrating tank filling T,s

Measured volume of liquid W, m3

Liquid rate Q, m3 /s

Pressure output PP, Pa

Vacuum input PV, Pa

Pump Pressure Head HP, m

Pump Power NP, W

Lever motor balance L, m

Motor Power NM, W

Pump efficiency

Appendix 1

Relation of kinematics viscosity coefficient of fresh water to temperature

Appendix 2

Relation of kinematics viscosity coefficient of AMG-10 oil to temperature

Appendix 3

Volume modulus K, kg/cm2

13.300

13.000

13.000

13.300

-200˚C

0.11

-190˚C

0.45

Vapour pressure pt. mm Hg

+20˚C

90

11.5

60

44

46.4

-160˚C

7

+40˚C

195

27

100

156

135

56.7

-149˚C

21

+60˚C

59

355

352

61.4

t

p1 atm

Kinematic viscosity υ at temperature t, centistokes

-50˚C

2.60

25

5.5

1.250

1.72

6.5

-204˚C

0.297

-20˚C

1.62

8.0

congeals

498

130

0.83

-200˚C

0.257

0˚C

0.93

4.0

2.0

10,100

42

0.70

1.042

-190˚C

0.193

+20˚C

0.73

2.5

1.05

1,100

30

16

0.58

1.52

0.95

-184˚C

0.170

+50˚C

0.54

1.5

1.55

8.3

10

0.38

-175˚C

0.125

+70˚C

1.2

65

7.5

0.30

t

υ cst

Specific gravity δ

0.750

0.800

0.775

0.895

0.885

0.850

1.510

0.790

1.34

1.15

1.25

Liquid

Aviation gasoline . Б95/130

Kerosene T-1

Kerosene T-2

Lubricating oil MC-20

Lubricating oil MK-8

Hydraulic fluid АМГ-10

Nitric acid (98%)

Ethyl alcohol

Hydrogen peroxide (80%)

Liquid oxygen

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