Consider the following statements: 1. The distinguishing features of a radial flow reaction turbine are – (i) only a part of the total head of water is converted into velocity head before it reaches the runner and (ii) the flow through water completely fills all the passages in the runner. 2. Kaplan turbine is essentially a propeller working in reverse, and its blades are so mounted that all the blade angles can be adjusted simultaneously by means of suitable gearing even as the machine is in operation 3. A draft tube is pipe of gradually increasing cross-sectional area which must be airtight, and under all conditions of operation, its lower end must be submerged below the level of the discharged water in the tailrace. Which of the above statements are correct?
Consider the following statements: 1. The distinguishing features of a radial flow reaction turbine are – (i) only a part of the total head of water is converted into velocity head before it reaches the runner and (ii) the flow through water completely fills all the passages in the runner. 2. Kaplan turbine is essentially a propeller working in reverse, and its blades are so mounted that all the blade angles can be adjusted simultaneously by means of suitable gearing even as the machine is in operation 3. A draft tube is pipe of gradually increasing cross-sectional area which must be airtight, and under all conditions of operation, its lower end must be submerged below the level of the discharged water in the tailrace. Which of the above statements are correct? Correct Answer 1, 2 and 3
Reaction Turbine:
- The principal feature of a reaction turbine that distinguishes it from an impulse turbine is that only a part of the total head available at the inlet to the turbine is converted to velocity head, before the runner is reached.
- Also, in the reaction turbines the working fluid, instead of engaging only one or two blades, completely fills the passages in the runner.
- The pressure or static head of the fluid changes gradually as it passes through the runner along with the change in its kinetic energy based on absolute velocity due to the impulse action between the fluid and the runner.
- The pressure at the exit of the runner of a reaction turbine is generally less than atmospheric pressure, so the water at exit cannot be directly discharged to the tail race. The draft tube is a conduit which connects the runner exit to the tail race. The primary function of the draft tube is to reduce the velocity of the discharged water to minimize the loss of kinetic energy at the outlet. This permits the turbine to be set above the tail water without any appreciable drop of available head.
Axial flow reaction turbine:
An axial flow turbine is a turbine in which the water flows parallel to the axis of the rotation of the shaft.
A reaction turbine is a turbine in which the head at the inlet is sum of the pressure energy and kinetic energy and during the flow of water through the runner a part of pressure energy is converted into kinetic energy.
The shaft of the turbine is vertical in axial flow reaction turbine.
There are two important types of axial flow reaction turbine:
1. Kaplan Turbine:
When the vanes on the hub are adjustable, then the turbine is known as Kaplan turbine.
2. Propeller Turbine:
When the vanes on the hub are not adjustable, then the turbine is known as propeller turbine.
Draft Tube: The draft tube is a conduit that connects the runner exit to the tailrace where the water is being finally discharged from the turbine. It is used with reaction turbines only.
The draft tube has two purposes as follows
i) It permits a negative or suction head to be established at the runner exit, thus making it possible to install the turbine above the tailrace level without loss head.
ii) It converts a large proportion of velocity energy rejected from the runner into useful pressure energy.
A draft tube is made divergent so as to reduce the velocity at the outlet to a minimum. Therefore, a draft tube is basically a diffuser and should be designed properly with the angle between the walls of the tube to be limited to about 8 degrees so as to prevent the flow separation from the wall and to reduce accordingly the loss of energy in the tube.
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