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Irreversible Flow from Turbine Exit to Condenser P M V Subbarao Professor Mechanical Engineering Department I I T Delhi Irreversibilities due to Closed Cycle Policy …..

Irreversible Flow from Turbine Exit to Condenser P M V Subbarao Professor Mechanical Engineering Department I I T Delhi Irreversibilities due to Closed

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Page 1: Irreversible Flow from Turbine Exit to Condenser P M V Subbarao Professor Mechanical Engineering Department I I T Delhi Irreversibilities due to Closed

Irreversible Flow from Turbine Exit to Condenser

P M V Subbarao Professor

Mechanical Engineering DepartmentI I T Delhi

Irreversibilities due to Closed Cycle Policy …..

Page 2: Irreversible Flow from Turbine Exit to Condenser P M V Subbarao Professor Mechanical Engineering Department I I T Delhi Irreversibilities due to Closed

The Last Stage of LP Turbine

Page 3: Irreversible Flow from Turbine Exit to Condenser P M V Subbarao Professor Mechanical Engineering Department I I T Delhi Irreversibilities due to Closed

First Stage of A Turbine : Governing Stage

• A governing stage is the first stage in a turbine with nozzle steam distribution.

• The principal design feature of a governing stage is that its degree of partiality changes with variations of flow rate through the turbine.

• The nozzles of a governing stages are combined into groups, each of them being supplied with steam from a separate governing valve.

• A governing stage is separated by a spacious chamber from the subsequent non-controlled stages.

• Governing stages may be of a single-row or two-row type.• Single row impulse governing stage is employed for an enthalpy

drop of 80-120 kJ/kg.• Two row governing stages are used when enthalpy drop is high,

100 – 250 kJ/kg.

Page 4: Irreversible Flow from Turbine Exit to Condenser P M V Subbarao Professor Mechanical Engineering Department I I T Delhi Irreversibilities due to Closed

Governing Stage

Page 5: Irreversible Flow from Turbine Exit to Condenser P M V Subbarao Professor Mechanical Engineering Department I I T Delhi Irreversibilities due to Closed

Selection of Enthalpy Drop & Type of Governing stage

• The enthalpy drop & type of governing stages are selected by considering the probable effect of the governing stage on the design and efficiency of the turbine.

• Higher the number of governing stages, lower will be the number of other stages.

• A high enthalpy drop in governing stage ensures a lower temperature of steam in its chamber and permits application of less expensive materials.

• In high capacity steam turbines, a single-row governing stages are preferred, since the advantages of elevated enthalpy drop are justified economically.

• The efficiency of governing stages,

in

inVustageg T

p

mk

0002.083.0/,

in

inVustagesg T

p

mk

0002.08.0/2,

Page 6: Irreversible Flow from Turbine Exit to Condenser P M V Subbarao Professor Mechanical Engineering Department I I T Delhi Irreversibilities due to Closed

Steam Path in Non-Controlled Stages

• Estimate approximate mass flow rate of steam by assuming an overall turbine internal efficiency of 0.85.

• Calculate flow through the condenser, using optimum of number of FWHs. (Using Cycle Calculations).

• Calculate Modified Efficiency of Low volume and intermediate volume stages.

• For a group of stages between two successive FWHs.

Z

h

m

lgroupiso

steam

avgrouplistages

,12sin

12000

6001

5.0925.0

groupegroupiav ..

•Average density is calculated as

Page 7: Irreversible Flow from Turbine Exit to Condenser P M V Subbarao Professor Mechanical Engineering Department I I T Delhi Irreversibilities due to Closed

• The efficiency of groups of very high volume stages:

• While designing the steam path, it is essential to consider the pressure losses in the following:

• Pressure loss in reheater: 0.1 prh.

• Pressure loss in connecting pipes between turbine cylinders:0.2ppipe.

groupiso

evgroupisogegigroup

hv h

hhxx

10000

4001

28.01870.0 ,,

Page 8: Irreversible Flow from Turbine Exit to Condenser P M V Subbarao Professor Mechanical Engineering Department I I T Delhi Irreversibilities due to Closed

Internal Reheating due to Irreversibilities

3

4s

4IIs

4IIIs

4Is

4Vs

4IVs

4Ia

4IIa

4IIIa

4IVa

4Va

4VIs

4VIa

T

s

Governing group

Group 1

Group 2

Group 3

Group 4

Group 5

Macro available enthalpy:

Micro available enthalpy:

shh 43

...444443

sasas IIIIIIIII hhhhhh

Page 9: Irreversible Flow from Turbine Exit to Condenser P M V Subbarao Professor Mechanical Engineering Department I I T Delhi Irreversibilities due to Closed

Macro available enthalpy:

Micro available enthalpy:

shh 43

N

Ijsas jjI hhhh 14443

Reheat Factor:

N

Ijsas

sh

jjI hhhh

hhR

14443

43

Page 10: Irreversible Flow from Turbine Exit to Condenser P M V Subbarao Professor Mechanical Engineering Department I I T Delhi Irreversibilities due to Closed

Internal Reheating due to Irreversibilities : HP

3

4s

4IIs

4IIIs

4Is

4Vs

4IVs

4Ia

4IIa

4IIIa

4IVa

4Va

4VIs

4VIa

T

s

Governing stage

Stage 1

Stage 2

Stage 3

Stage 4

Stage 5

22.33 MPa,3379.0

15.74 MPa,3303.0 k J/kg

13.77 MPa, 3269.0 k J/kg

12.12 MPa, 3236.5.0 k J/kg

10.56 MPa, 3203.8 k J/kg

9.2 MPa, 3171.0 k J/kg

7.94 MPa, 3140.4 k J/kg

4VIIa

6.9 MPa, 3104.9 k J/kg

4VIIIa

5.17 MPa, 3036.7 k J/kg

4IXa

5.95 MPa, 3070.9 k J/kg

Pho=5 %

Pho=19.5%

Pho=21%

Pho=22%

Pho=23.5%

Pho=25%

Pho=30%

Pho=32%

Stage 6

Stage 7

Stage 8

Pho=35%

Page 11: Irreversible Flow from Turbine Exit to Condenser P M V Subbarao Professor Mechanical Engineering Department I I T Delhi Irreversibilities due to Closed

0

2

4

6

8

10

12

14

Stages

Loss

(kJ/

kg)

Cumulative loss

Cumulative Losses for All Stages : 500 MW

Page 12: Irreversible Flow from Turbine Exit to Condenser P M V Subbarao Professor Mechanical Engineering Department I I T Delhi Irreversibilities due to Closed

Definition of Efficiency

• Relative blade efficiency is calculated as:

• Internal Relative Efficiency is calculated as:

dropEnthalpy Effective

loss Blade Moving & Nozzle-dropEntalpy Effectiverel

dropEnthalpy Effective

loss profile - loss leakage-losses Blade Moving & Nozzle-dropEntalpy Effectiveint, rel

Page 13: Irreversible Flow from Turbine Exit to Condenser P M V Subbarao Professor Mechanical Engineering Department I I T Delhi Irreversibilities due to Closed

Blade Efficiency & Internal Relative Efficiency: 800 MW

Page 14: Irreversible Flow from Turbine Exit to Condenser P M V Subbarao Professor Mechanical Engineering Department I I T Delhi Irreversibilities due to Closed

LP Turbine Exhaust System • In a condensing steam turbine, the low-pressure exhaust hood,

consisting of a diffuser and a collector or volute!, connects the last stage turbine and the condenser.

• The function of the hood is to transfer the turbine leaving kinetic energy to potential energy while guiding the flow from the turbine exit plane to the condenser.

• Most of exhaust hoods discharge towards the downward condenser. • Flow inside the hood therefore must turn about 90 deg from the

axial direction to the radial direction before exhausting into the condenser.

• The 90-deg turning results in vortical flow in the upper half part of the collector and also high losses.

• The exhaust hood is one of the few steam turbine components that has the considerable aerodynamic losses.

• It is a challenge for engineers to operate a hood with high pressure recovery and low total pressure loss in a compact axial length.

Page 15: Irreversible Flow from Turbine Exit to Condenser P M V Subbarao Professor Mechanical Engineering Department I I T Delhi Irreversibilities due to Closed

Exhaust Hood

Page 16: Irreversible Flow from Turbine Exit to Condenser P M V Subbarao Professor Mechanical Engineering Department I I T Delhi Irreversibilities due to Closed

Exhaust Diffuser For L P Turbine

Page 17: Irreversible Flow from Turbine Exit to Condenser P M V Subbarao Professor Mechanical Engineering Department I I T Delhi Irreversibilities due to Closed

Steam Turbine Exhaust Size Selection

• The steam leaving the last stage of a condensing steam turbine can carry considerably useful power to the condenser as kinetic energy.

• The turbine performance analysis needs to identify an exhaust area for a particular load that provides a balance between exhaust loss and capital investment in turbine equipment.

Page 18: Irreversible Flow from Turbine Exit to Condenser P M V Subbarao Professor Mechanical Engineering Department I I T Delhi Irreversibilities due to Closed

Path Lines in Exhaust Hood

Page 19: Irreversible Flow from Turbine Exit to Condenser P M V Subbarao Professor Mechanical Engineering Department I I T Delhi Irreversibilities due to Closed

Exhaust Losses

• Exhaust losses are losses which occur between last stage of turbine and condenser.

• Exhaust losses made up of four components:• Actual leaving losses• Gross hood loss• Annulus restriction loss• Turn up loss

Page 20: Irreversible Flow from Turbine Exit to Condenser P M V Subbarao Professor Mechanical Engineering Department I I T Delhi Irreversibilities due to Closed

Residual velocity loss

• Steam leaving the last stage of the turbine has certain velocity, which represent the amount of kinetic energy that cannot be imparted to the turbine shaft and thus it is wasted

Exhaust end loss

1. Exhaust end loss occur between the last stage of low pressure turbine and condenser inlet.

2. Exhaust loss depends on the absolute steam velocity.

Turbine Exhaust end loss = Expansion-line -end point - Used energy at end point.

Page 21: Irreversible Flow from Turbine Exit to Condenser P M V Subbarao Professor Mechanical Engineering Department I I T Delhi Irreversibilities due to Closed

Turn-up loss

Total Exhaust Loss

Gross hood loss

Actual leaving loss

Annulus restriction loss

Annulus Velocity (m/s)

Exh

aust

Los

s, k

J/kg

of

dry

flow

0 120 150 180 240 300 360

10

20

30

40

50Annulus velocity (m/s)

Condenser flow rate

Annulus area

Percentage of Moisture at the Expansion line end point

Typical exhaust loss curve showing distribution of component loss

SP.Volume

an

steamexan A

xvmV

3600

01.01.

Page 22: Irreversible Flow from Turbine Exit to Condenser P M V Subbarao Professor Mechanical Engineering Department I I T Delhi Irreversibilities due to Closed

Optimal Design of Exhaust Hood

Page 23: Irreversible Flow from Turbine Exit to Condenser P M V Subbarao Professor Mechanical Engineering Department I I T Delhi Irreversibilities due to Closed
Page 24: Irreversible Flow from Turbine Exit to Condenser P M V Subbarao Professor Mechanical Engineering Department I I T Delhi Irreversibilities due to Closed

Performance Analysis of Power Plant Condensers

P M V SubbaraoProfessor

Mechanical Engineering DepartmentI I T Delhi

A Device Which makes Power Plant A True Cycle..A Device Which set the limit on minimum cycle

pressure…..

Page 25: Irreversible Flow from Turbine Exit to Condenser P M V Subbarao Professor Mechanical Engineering Department I I T Delhi Irreversibilities due to Closed

T-S Diagram : Rankine Cycle with FWHs.

?,, exitcondincond pp

inCWT ,outCWT ,

?TTD

exhaustturbinep ,

hoodp

Page 26: Irreversible Flow from Turbine Exit to Condenser P M V Subbarao Professor Mechanical Engineering Department I I T Delhi Irreversibilities due to Closed

A Device to Convert Dead Steam into Live Water

Water ready to take Rebirth

Dead Steam

Page 27: Irreversible Flow from Turbine Exit to Condenser P M V Subbarao Professor Mechanical Engineering Department I I T Delhi Irreversibilities due to Closed

Steam Condenser

• Steam condenser is a closed space into which steam exits the turbine and is forced to give up its latent heat of vaporization.

• It is a necessary component of a steam power plant because of two reasons.• It converts dead steam into live feed water.• It lowers the cost of supply of cleaning and treating of working fluid.• It is far easier to pump a liquid than a steam.• It increases the efficiency of the cycle by allowing the plant to operate on largest

possible temperature difference between source and sink.• The steam’s latent heat of condensation is passed to the water flowing through the

tubes of condenser.• After steam condenses, the saturated water continues to transfer heat to cooling

water as it falls to the bottom of the condenser called, hotwell.• The difference between saturation temperature corresponding to condenser

vaccum and temperature of condensate in hotwell is called condensate depression.

Page 28: Irreversible Flow from Turbine Exit to Condenser P M V Subbarao Professor Mechanical Engineering Department I I T Delhi Irreversibilities due to Closed
Page 29: Irreversible Flow from Turbine Exit to Condenser P M V Subbarao Professor Mechanical Engineering Department I I T Delhi Irreversibilities due to Closed
Page 30: Irreversible Flow from Turbine Exit to Condenser P M V Subbarao Professor Mechanical Engineering Department I I T Delhi Irreversibilities due to Closed

Two-Pass Surface Condenser

Page 31: Irreversible Flow from Turbine Exit to Condenser P M V Subbarao Professor Mechanical Engineering Department I I T Delhi Irreversibilities due to Closed

Layouts of A Condenser

Page 32: Irreversible Flow from Turbine Exit to Condenser P M V Subbarao Professor Mechanical Engineering Department I I T Delhi Irreversibilities due to Closed

Layouts of A Condenser

Page 33: Irreversible Flow from Turbine Exit to Condenser P M V Subbarao Professor Mechanical Engineering Department I I T Delhi Irreversibilities due to Closed

An Integral Steam Turbine and Condenser System