**Turbomachinery**" topic of the "

**Fluid Mechanics & Hydraulics**" subject.

## Turbomachinery

Turbomachine is defined as a device in which energy transfer takes place between a flowing fluid and a rotating element resulting in a change of pressure and momentum of the fluid. Energy is transferred into or out of the turbomachine mechanically by means of input/output shafts.

**Principal Parts of a Turbo Machine**

- Rotating element consisting of a rotor on which are mounted blades.
- A stationary element in the form of guide blades, nozzles, etc.
- Input/output shafts.
- Housing

Schematic cross sectional view of a steam turbine showing the principal parts of a turbomachine.

**Functions:**

- The rotor functions to absorb/deliver energy to the flowing fluid.
- The stator is a stationary element which may be of many types:-
- Guide blades which function to direct the flowing fluid in such a way that energy transfer is maximized.
- Nozzles which function to convert pressure energy of the fluid to kinetic energy
- Diffusers which function to convert kinetic energy to pressure energy of the fluid.

- The input /output shafts function to deliver/receive mechanical energy to or from the machine.
- The housing is a protective enclosure which also functions to provide a path of flowing fluid. While a rotor & input /output shaft are essential parts of all turbo machines, the stator & the housing are optional.

**Classification of Turbo Machines:**

- According to the nature of energy transfer:
- Power generating turbo machines: In this, energy is transferred from the flowing fluid to the rotor. Hence, enthalpy of the flowing fluid decreases as it flows across. There is a need for an output shaft.
- Ex: Hydraulic turbines such as Francis turbine, Pelton wheel turbine, Kaplan turbine, steam turbine such as De-Laval turbine, Parsons Turbine etc, Gas turbines etc,
- Power absorbing Turbo machines: In this, energy is transferred from the rotor to the flowing fluid. The enthalpy of the fluid increases as it flows there is a need for an input shaft.
- Ex: Centrifugal pump, Compressor, blower, fan etc,
- Power transmitting turbo machines: In this energy is transferred from one rotor to another by means of a flowing fluid. There is a need for an input / output shafts. The transfer of energy occurs due to fluid action.
- Ex: Hydraulic coupling, torque converter etc,

**Schematic representation of different types of turbo machine based on fluid flow:**

- Axial flow fan.
- Radial outward flow fan.
- Mixed flow hydraulic turbine.

**Based on the type of fluid flow:**- Tangential flow in which fluid flows tangential to the rotor Ex: Pelton wheel etc,
- Axial flow in which the fluid flows more or less parallel to the axes of the shafts /rotors. Ex: Kaplan turbine, Axial flow compressor.
- Radial flow in which fluid flows along the radius of the rotor this is again classified as:
- Radially inward flow. Ex: Old fancies turbine.
- Radially outward flow. Ex: Centrifugal Pump

- Mixed flow which involves radius entry & axial exit or vise-versa. Ex: Modern francises turbine & Centrifugal Pump

**Based on the type of Head:**- High head &low discharge. Ex: Pelton wheel.
- Medium head &medium discharge. Ex: Francis turbine.
- Low head & high discharge. Ex: Kaplan turbine.

**Application of 1 ^{st} & 2^{nd} law of thermodynamics of turbo machines:**

In a turbo machine, the fluctuations in the properties when observed over a period of time are found to be negligible. Hence, a turbo machine may be treated as a steady flow machine with reasonable accuracy & hence, we may apply the steady flow energy equation for the analysis of turbo machine.

Hence we may write

Where, subscript ‘1’ is at the point of entry & subscript ‘2’ is at point of exit.

It is also true that, thermal losses are minimal compared to the amount of work transferred & hence may be neglected. Hence we may write,

Where, h_{02 }& h_{01} are stagnation exit & entry respectively.

w = ∆h_{0.}

In a power generating turbo machine, ∆h_{0} is negative (since h_{02} < h_{01}) & hence w is positive.

On the same line, for a power absorbing turbo machine, ∆h_{0} is positive (since h_{02 }> h_{01}) & hence w is negative.

From the 2^{nd} law of Thermodynamics:

In the above relation, we note that vdp would be a negative quantity for a power generating turbo machine & positive for power absorbing turbo machine.

Hence Tds which is always a positive quantity would reduce the amount of work generated in the former case & increase the work absorbed in the later case.

**Efficiency of a turbo machine:**

Generally, we define 2 types of turbo machine .in case of turbo machine to account for various losses 2 type of efficiency is considered:

- Hydraulic efficiency/isentropic efficiency
- Mechanical efficiency.

**Hydraulic efficiency/isentropic efficiency:**

To account for the energy loss between the fluid & the rotor

2. **Mechanical efficiency:**

To account for the energy loss between the rotor & the shaft.

**Schematic representation of Compression & Expansion process:**

(a) Power absorbing machine. (b) Power generating machine.

**Analysis of Energy Transfer in turbo machines:** Analysis of energy transfer in turbo machines requires a consideration of the kinematics and dynamic factors involved. The factors include changes in the fluid velocity, rotor velocity and the forces caused due to change in the velocity.

We apply Newton’s second law of motion as applicable to rotary movement. i.e., Torque is proportional to the rate of change of angular momentum.

Another important consideration is the treatment of a turbo machine as a steady flow machine.

- This involves following assumptions:
- Mass-flow rate is constant.
- State of fluid at any given point does not change.
- Heat and Work transfer are constant.
- Leakage losses are negligible.
- Same steady mass of fluid flows through all section.

Velocity Components:

Fig. velocity components through a rotor

The fluid enters the rotor with an absolute velocity say V_{1} and leaves with an absolute velocity say V_{2.}

The absolute velocity of the fluid will have components in the axial, radial and tangential direction which may be referred to as V_{a},V_{w} and V_{f }respectively.

The axial components do not participate in the energy transfer but cause a thrust which is borne by the thrust bearings. The radial components also do not participate in the energy transfer but cause a thrust which are borne by the journal bearings. The only components which participate in the energy transfer is the tangential component Vw.

V_{a1} and V_{a2} : Axial components of V_{1} and V_{2} respectively.

V_{f1 }and V_{f2} : Radial components of V_{1} and V_{2 }respectively.

V_{w1} and V_{w2 }: Tangential components of V_{1} and V_{2 }respectively referred to as whirl velocity, flow velocity. Let the rotor move with an angular velocity ω.

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## Comments

write a commentTheanmozhi ThuyamaniJul 31, 2018

Schematic representation of Compression & Expansion processUnable to get this sir.. Please explain it elaborately