A quarter-scale turbine model is tested under a head of \(10.8 \mathrm{~m}\). The full-scale turbine is required to work under a head of \(30 \mathrm{~m}\) and to run at \(44.86 \mathrm{rad} \cdot \mathrm{s}^{-1}(7.14 \mathrm{rev} / \mathrm{s}) .\) At what speed must the model be run? If it develops \(100 \mathrm{~kW}\) and uses water at \(1.085 \mathrm{~m}^{3} \cdot \mathrm{s}^{-1}\) at this speed, what power will be obtained from the full-scale turbine, its efficiency being \(3 \%\) better than that of the model? What is the power specific speed of the full-scale, turbine?

Short Answer

Expert verified
The model must be run at approximately 26.94 rad/s. The full-scale turbine will develop approximately 18347.875 kW, and its power specific speed is approximately 0.602 rad·s⁻¹·(m³/s)¹/²·(m)⁻⁵/⁴.

Step by step solution

01

- Determine the model speed

Using the similarity laws for turbines, we can find the speed of the model. The relation is: \[ \frac{N_m}{N_f} = \frac{\text{(Head of Model)}^{1/2}}{\text{(Head of Full Scale)}^{1/2}} \] where \( N_m \) is the model speed, and \( N_f \) is the full-scale speed. Thus, \[ \frac{N_m}{44.86} = \frac{(10.8)^{1/2}}{(30)^{1/2}} \] Solving for \( N_m \) gives us: \[ N_m = 44.86 \times \frac{(10.8)^{1/2}}{(30)^{1/2}} \] \[ N_m = 44.86 \times \frac{3.29}{5.48} \] \[ N_m \approx 26.94 \text{ rad} \cdot \text{s}^{-1} \]
02

- Calculate the power scale factor

The power developed by the turbine scales with the ratio of the heads and the cube of the linear scale. Since the model is quarter-scale, the scale factor for linear dimensions is \( \frac{1}{4} \). The power scale factor is given by: \[ \frac{P_m}{P_f} = \frac{(Head_{model}) \times (Linear Scale)^2}{(Head_{full}) \times (Linear Scale)^5} \] Simplifying the ratio \[ \frac{P_m}{P_f} = \frac{(10.8) \times (1/4)^2}{(30) \times (1/4)^5} \] \[ \frac{P_m}{P_f} = \frac{10.8 \times 1/16}{30 \times 1/1024} \] \[ P_f = P_m \times \frac{30 \times 1/1024}{10.8 \times 1/16} \] \[ P_f = 100 \text{kW} \times \frac{30 \times 1024}{10.8 \times 16} \] \[ P_f \approx 17812.5 \text{kW} \]
03

- Adjust for efficiency

The efficiency of the full-scale turbine is 3% better than the model. If we denote the model's efficiency as \( \text{Eff}_{m} \), then the full-scale efficiency is \( \text{Eff}_{f} = \text{Eff}_{m} + 0.03 \). If the developed power without efficiency adjustments is \( 17812.5 \text{ kW} \), then the final power output of the full-scale turbine is: \[ \text{Power}_{final} = 17812.5 \times (1 + 0.03) \] \[ \text{Power}_{final} = 17812.5 \times 1.03 \] \[ \text{Power}_{final} \approx 18347.875 \text{kW} \]
04

- Determine the power specific speed

The power specific speed (n_s) of the turbine is given by: \[ n_s = N \times \frac{Q^{1/2}}{H^{5/4}} \] where \( N \) is the rotational speed of the turbine, \( Q \) is the volume flow rate, and \( H \) is the head. We need to find this for the full-scale turbine: \[ n_s = 44.86 \times \frac{(1.085)^{1/2}}{(30)^{5/4}} \] \[ n_s = 44.86 \times \frac{(1.041)}{(77.46)} \] \[ n_s \approx 0.602 \text{ rad} \cdot \text{s}^{-1} \cdot \text{(m}^3\text{/s)}^{1/2} \cdot \text{(m)}^{-5/4} \]

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Key Concepts

These are the key concepts you need to understand to accurately answer the question.

similarity laws for turbines
The similarity laws, or affinity laws, are essential for understanding how models of turbines relate to their full-scale counterparts. These laws help us predict the performance of a full-scale turbine based on tests conducted on a scaled-down model. These laws assume geometric and dynamic similitude between the model and the prototype.

The key relationship used here is: \ \ \(\frac{N_m}{N_f} = \frac{\text{(Head of Model)}^{1/2}}{\text{(Head of Full Scale)}^{1/2}}\) \ \ This formula allows us to determine the rotational speed of the model (\(N_m\)) if we know the rotational speed of the full-scale turbine (\(N_f\)) and the heads under which both are operating.
model speed calculation
To calculate the speed at which a scaled-down model turbine must be run, we use the similarity laws. Given the full-scale turbine operates at a specific head and speed, we can calculate the appropriate model speed. Here's how we do it:

Switching from heads to speeds: \ \ \(N_m = N_f \times \left( \frac{\text{(Head of Model)}^{1/2}}{\text{(Head of Full Scale)}^{1/2}} \right)\) \ \ With a full-scale speed of 44.86 rad/s and heads of 10.8 m (model) and 30 m (full-scale), we substitute and solve: \ \ \(N_m = 44.86 \times \left( \frac{10.8^{1/2}}{30^{1/2}} \right) \) \ \ Simplifying leads to: \ \ \(N_m = 44.86 \times \frac{3.29}{5.48} \approx 26.94 \text{ rad} \cdot \text{s}^{-1}\) \ \ Thus, the model should run at 26.94 rad/s.
power scale factor
The power scale factor helps us to translate the power output from a model turbine to what a full-scale turbine would produce. This scaling takes into account the difference in both the operating head and the size scale. The power scales with the product of the heads and the fifth power of the geometric scale ratio:

Using the formula: \ \ \(\frac{P_m}{P_f} = \frac{\text{(Head of Model)} \times \text{(Linear Scale)}^2}{\text{(Head of Full Scale)} \times \text{(Linear Scale)}^5}\) \ \ Given a quarter-scale model (linear scale = 1/4) and heads: \ \ \(\frac{P_m}{P_f} = \frac{10.8 \times (1/16)}{30 \times (1/1024)}\) \ \ This simplifies further to: \ \ \(P_f = 100 \times \frac{30 \times 1024}{10.8 \times 16} \approx 17812.5 \text{kW}\)
efficiency adjustment
When transferring results from the model to the full-scale turbine, we need to account for any efficiency differences. In our case, the full-scale turbine's efficiency is 3% better than the model’s. Assuming the model develops a power of 17812.5 kW without efficiency adjustments, the formula for the final power is:

\(\text{Power} = P_f \times (1 + 0.03)\) \ \ Substituting gives: \ \ \(\text{Power} = 17812.5 \times 1.03 \) \ \ Which simplifies to roughly: \ \ \(\text{Power } \approx 18347.875 \text{kW}\)
power specific speed
The power specific speed of a turbine (\(n_s\)) is a crucial non-dimensional number that helps in comparing different designs. It combines turbine speed, flow rate, and head. The equation is:

\(n_s = N \times \frac{Q^{1/2}}{H^{5/4}}\) \ \ For the full-scale turbine, using the given full-scale values: \ \ \(n_s = 44.86 \times \frac{(1.085)^{1/2}}{(30)^{5/4}}\) \ \ Upon simplifying, we have: \ \ \(n_s \approx 0.602 \text{ rad} \cdot \text{s}^{-1} \cdot (\text{m}^3/\text{s})^{1/2} \cdot (\text{m})^{-5/4}\)

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Most popular questions from this chapter

A centrifugal pump which runs at \(104.3 \mathrm{rad} \cdot \mathrm{s}^{-1}(16.6 \mathrm{rev} / \mathrm{s})\) is mounted so that its centre is \(2.4 \mathrm{~m}\) above the water level in the suction sump. It delivers water to a point \(19 \mathrm{~m}\) above its centre. For a flow rate of \(Q\left(\mathrm{~m}^{3} \cdot \mathrm{s}^{-1}\right)\) the friction loss in the suction pipe is \(68 Q^{2} \mathrm{~m}\) and that in the delivery pipe is \(650 Q^{2} \mathrm{~m}\). The impeller of the pump is \(350 \mathrm{~mm}\) diameter and the width of the blade passages at outlet is \(18 \mathrm{~mm} .\) The blades themselves occupy \(5 \%\) of the circumference and are backward-facing at \(35^{\circ}\) to the tangent. At inlet the flow is radial and the radial component of velocity remains unchanged through the impeller. Assuming that \(50 \%\) of the velocity head of the water leaving the impeller is converted to pressure head in the volute, and that friction and other losses in the pump, the velocity heads in the suction and delivery pipes and whirl slip are all negligible, calculate the rate of flow and the manometric efficiency of the pump.

In a hydro-electric scheme a number of Pelton wheels are to be used under the following conditions: total output required \(30 \mathrm{MW} ;\) gross head \(245 \mathrm{~m} ;\) speed \(39.27 \mathrm{rad} \cdot \mathrm{s}^{-1}\) \(\left(6.25\right.\) rev/s); 2 jets per wheel; \(C_{\mathrm{Y}}\) of nozzles \(0.97 ;\) maximum overall efficiency (based on conditions immediately before the nozzles) \(81.5 \% ;\) power specific speed for one jet not to exceed \(0.138\) rad \((0.022\) rev); head lost to friction in pipe-line not to exceed \(12 \mathrm{~m} .\) Calculate \((a)\) the number of wheels required, (b) the diameters of the jets and wheels, (c) the hydraulic efficiency, if the blades deflect the water through \(165^{\circ}\) and reduce its relative velocity by \(15 \%,(d)\) the percentage of the input power that remains as kinetic energy of the water at discharge.

A vertical-shaft Francis turbine, with an overall efficiency of \(90 \%\), runs at \(44.86 \mathrm{rad} \cdot \mathrm{s}^{-1}(7.14 \mathrm{rev} / \mathrm{s})\) with a water discharge of \(15.5 \mathrm{~m}^{3} \cdot \mathrm{s}^{-1} .\) The velocity at the inlet of the spiral casing is \(8.5 \mathrm{~m} \cdot \mathrm{s}^{-1}\) and the pressure head at this point is \(240 \mathrm{~m}\), the centre-line of the casing inlet being \(3 \mathrm{~m}\) above the tail-water level. The diameter of the runner at inlet is \(2.23 \mathrm{~m}\) and the width at inlet is \(300 \mathrm{~mm}\). The hydraulic efficiency is \(93 \%\). Determine \((a)\) the output power, \((b)\) the power specific speed, ( \(c\) ) the guide vane angle, \((d)\) the runner blade angle at inlet, (e) the percentage of the net head which is kinetic at entry to the runner. Assume that there is no whirl at outlet from the runner and neglect the thickness of the blades.

A centrifugal fan, for which a number of interchangeable impellers are available, is to supply air at \(4.5 \mathrm{~m}^{3} \cdot \mathrm{s}^{-1}\) to a ventilating duct at a head of \(100 \mathrm{~mm}\) water gauge. For all the impellers the outer diameter is \(500 \mathrm{~mm}\), the breadth \(180 \mathrm{~mm}\) and the blade thickness negligible. The fan runs at \(188.5 \mathrm{rad} \cdot \mathrm{s}^{-1}\) ( \(\left.30 \mathrm{rev} / \mathrm{s}\right)\). Assuming that the conversion of velocity head to pressure head in the volute is counterbalanced by the friction losses there and in the impeller, that there is no whirl at inlet and that the air density is constant at \(1.23 \mathrm{~kg} \cdot \mathrm{m}^{-3}\), determine the most suitable outlet angle of the blades. (Neglect whirl slip.)

The impeller of a centrifugal pump has an outer diameter of \(250 \mathrm{~mm}\) and an effective outlet area of \(17000 \mathrm{~mm}^{2} .\) The outlet blade angle is \(32^{\circ} .\) The diameters of suction and discharge openings are \(150 \mathrm{~mm}\) and \(125 \mathrm{~mm}\) respectively. At \(152 \mathrm{rad} \cdot \mathrm{s}^{-1}(24.2 \mathrm{rev} / \mathrm{s})\) and discharge \(0.03 \mathrm{~m}^{3} \cdot \mathrm{s}^{-1}\) the pressure heads at suction and discharge openings were respectively \(4.5 \mathrm{~m}\) below and \(13.3 \mathrm{~m}\) above atmospheric pressure, the measurement points being at the same level. The shaft power was \(7.76 \mathrm{~kW}\). Water enters the impeller without shock or whirl. Assuming that the true outlet whirl component is \(70 \%\) of the ideal, determine the overall efficiency and the manometric efficiency based on the true whirl component.

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