The heat drop in fixed and moving blades are 15 kJ/kg and 30 kJ/kg, respectively in an impulse reaction turbine stage. The degree of reaction for this stage will be:
2/3
An impulse reaction turbine is a type of thermal turbine that extracts energy from a fluid by both impulse and reaction principles. In such a turbine, the working fluid, typically steam or gas, undergoes an enthalpy (heat) drop in both the stationary (fixed) blades and the rotating (moving) blades. The problem asks us to determine the degree of reaction for a specific turbine stage given the individual heat drop values for the fixed and moving blades.
The heat drop in a turbine stage refers to the total decrease in the enthalpy of the working fluid as it passes through that stage. This energy conversion drives the turbine rotor. The total heat drop within a stage is divided between two main components:
The degree of reaction (R) is a fundamental parameter in turbine design that quantifies the proportion of the total enthalpy drop (or static heat drop) that takes place within the moving blades, relative to the total enthalpy drop across the entire stage. It helps classify turbines and understand their operating characteristics. For an impulse reaction turbine, the degree of reaction is defined as:
\[ \text{Degree of Reaction (R)} = \frac{\text{Heat drop in moving blades}}{\text{Total heat drop in the stage}} \]
The total heat drop for the entire stage is the sum of the heat drops in both the fixed and moving blades:
\[ \text{Total heat drop in the stage} = \text{Heat drop in fixed blades} + \text{Heat drop in moving blades} \]
To find the degree of reaction for this impulse reaction turbine stage, we will use the provided heat drop values:
First, we calculate the total heat drop for the entire turbine stage:
\[ \text{Total heat drop in the stage} = 15 \, \text{kJ/kg} \, (\text{fixed blades}) + 30 \, \text{kJ/kg} \, (\text{moving blades}) \]
\[ \text{Total heat drop in the stage} = 45 \, \text{kJ/kg} \]
Now, we can substitute the calculated total heat drop and the given heat drop in moving blades into the formula for the degree of reaction:
\[ \text{R} = \frac{\text{Heat drop in moving blades}}{\text{Total heat drop in the stage}} \]
\[ \text{R} = \frac{30 \, \text{kJ/kg}}{45 \, \text{kJ/kg}} \]
To simplify the fraction, we find the greatest common divisor of 30 and 45, which is 15:
\[ \text{R} = \frac{30 \div 15}{45 \div 15} = \frac{2}{3} \]
The calculated degree of reaction for this impulse reaction turbine stage is \(\frac{2}{3}\).
This result implies that two-thirds of the total enthalpy drop in this particular turbine stage occurs within the moving blades, highlighting the significant reactive nature of this turbine stage.
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