GAS%20TURBINE%20POWER%20PLANTS - PowerPoint PPT Presentation

About This Presentation
Title:

GAS%20TURBINE%20POWER%20PLANTS

Description:

GAS POWER PLANTS IN INDIA. THE MAIN COMPONENTS OF A GAS ... The air at high pressure from the compressor is led to the combustion chamber via the regenerator.In the ... – PowerPoint PPT presentation

Number of Views:364
Avg rating:3.0/5.0
Slides: 26
Provided by: 123se66
Category:

less

Transcript and Presenter's Notes

Title: GAS%20TURBINE%20POWER%20PLANTS


1
GAS TURBINE POWER PLANTS
BY ABHISHIEK PAWAR - 0815002 ANIL NAIR -
0815012 ANIRUDDHA SAWANT - 0815013 ANJALI DESAI
- 0815014
2
INTRODUCTION
  • A generating station which employs gas turbine as
    the prime mover for the generation of electrical
    energy is known as a gas turbine power plant.
  • In a gas turnine power plant,air is used as the
    working fluid.The air is compressed by the
    compressor is lead to the combustion chamber
    where heat is added to air,thus raising its
    temperature.Heat is added to the compressed air
    either by burning fuel in the chamber or by the
    use of air heaters.The hot and high pressure air
    from the combustion chamber is then passed to the
    gas turbine where it expands and does the
    mechanical work.The gas turbine drives the
    alternator which converts the mechanical energy
    into electrical energy.

3
SIMPLE GAS TURBINE CYCLE
4
AIR STANDARD BRAYTON CYCLE
1 - 2    Isentropic compression2 - 3    Constant
pressure heat addition3 - 4    Isentropic
expansion4 - 1    Constant pressure heat removal
P-V Diagram
T-S Diagram
5
SIMPLE GAS TURBINE LAYOUT
FRONT VIEW
TOP VIEW
6
FUELS
  • One further advantage of gas turbines is their
    fuel flexibility. They can be adapted to use
    almost any flammable gas or light distillate
    petroleum products such as gasoline (petrol),
    diesel and kerosene (paraffin) which happen to be
    available locally, though natural gas is the most
    commonly used fuel. Crude and other heavy oils
    and can also be used to fuel gas turbines if they
    are first heated to reduce their viscosity to a
    level suitable for burning in the turbine
    combustion chambers.

7
ADVANTAGES
  • It is simple in design as compared to steam power
    station since no boilers and their auxiliaries
    are required
  • it is much smaller in size as compared to steam
    power station of same capacity.This is expected
    since gas turbine power plant doesnot require
    boiler,feed water arrangements etc
  • The initial and operating costs are much lower
    than that of equivalent steam power station
  • It requires comparatively less water as no
    condenser is used
  • The maintenance charges are quite small
  • Gas turbines are much simpler in construction and
    operation than steam turbines
  • It can be started quickly from cold conditions
  • There are no standby losses.However,in a steam
    power station,these losses occur because boiler
    is kept in operation even when the steam turbine
    is supplying no load

8
DISADVANTAGES
  • There is a problem for starting the unit.It is
    because before starting the turbine,the
    compressor has to be operated for which power is
    required from some external source.However once
    the unit starts,the external power is not needed
    as the turbine itself supplies necessary power to
    the compressor.
  • Since a greater part of the power developed by
    the turbine is used in driving the compressor,the
    net output is low
  • The overall efficiency of such plants is
    low(about 20) because of the exhaust gases from
    the turbine contain sufficient heat
  • The temperature of combustion chamber is quite
    high(3000 deg.F)so that its life is comparatively
    reduced

9
GAS POWER PLANTS IN INDIA
10
THE MAIN COMPONENTS OF A GAS TURBINE POWER PLANT
  • COMPRESSOR
  • TURBINE
  • HEAT EXCHANGER
  • INTERCOOLER

11
(No Transcript)
12
(No Transcript)
13
COMPRESSOR
  • The compressor sucks in air form the atmosphere
    and compresses it to pressures in the range of 15
    to 20 bar. The compressor consists of a number of
    rows of blades mounted on a shaft. This is
    something like a series of fans placed one after
    the other. The pressurized air from the first row
    is further pressurized in the second row and so
    on. Stationary vanes between each of the blade
    rows guide the air flow from one section to the
    next section. The shaft is connected and rotates
    along with the main gas turbine.

14
TURBINE
  • The turbine does the main work of energy
    conversion. The turbine portion also consists of
    rows of blades fixed to the shaft. Stationary
    guide vanes direct the gases to the next set of
    blades. The kinetic energy of the hot gases
    impacting on the blades rotates the blades and
    the shaft. The blades and vanes are made of
    special alloys and designs that can withstand the
    very high temperature gas. The exhaust gases then
    exit to exhaust system through the diffuser. The
    gas temperature leaving the Turbine is in the
    range of 500 to 550 C.

15
HEAT EXCHANGER
  • Two kinds of heat exchangers are used
  • a) Recuperators and b)Regenerators
  • In recuperative type, the air and hot gases are
    made to flow in counter direction as the effect
    of counter-flow gives high average temperature
    difference causing the higher heat flow.

16
HEAT EXCHANGER
  • The regenerator type heat exchanger consists of a
    heat conducting member which is exposed
    alternately to the hot exhaust gases and the
    cooler compressed air. It absorbs heat from hot
    gases and gives it up when exposed to the air.
    The heat capacity member is made of a metallic
    mesh or matrix which is rotated slowly (40-60
    rpm) and continuously exposed to hot and cold air.

17
(iii)Combustion Chamber The air at high pressure
from the compressor is led to the combustion
chamber via the regenerator.In the combustion
chamber,heat is added to the air by burning oil .
The oil is injected through the burner into the
chamber at high pressure ensure atomization of
oil and its through mixing with air . The result
is that the chamber attains a very high
temperature(about 3000F).The combustion gases are
suitably cooled to 1300F to 1500F then delivered
to gas turbine.
18
INTERCOOLER
  • An intercooler is generally used in a gas turbine
    power plant when the pressure ratio used is
    sufficiently large and the compression is
    completed with two or more stages
  • A cross flow type intercooler is generally
    preferred for effective heat transfer

19
URAN GAS TURBINE POWER PLANT
20
  • It is the first gas-run electricity plant in asia
  • This power station has got first air cooled
    condensor in asia.
  • It consists of nine units overall
  • UNIT 1 was commisioned in February 1982
  • The plant can be brought to full speed in 3
    minutes and at full load in 8 minutes

21
Total Capacity of Station.852 MW GT        
3 x 60 MW                    GT         4 x
108 MW                    WHRP  2 x 120 MW
22
  • The plant is located close to ONGC Uran terminal
    where the gas separation is done
  • A 220 kV sub-station has been established which
    connects the station to the state 220 kV network
  • A pipeline of 30 cm diameter and 6 km long from
    ONGC terminal to gas turbine station is completed
    in 1982 to supply the gas separated at ONGC
    terminal

23
(No Transcript)
24
REFERENCES
25
THANK YOU
Write a Comment
User Comments (0)
About PowerShow.com