Irreversible Flow from Turbine Exit to Condenser

Slides:



Advertisements
Similar presentations
An Introduction To Marine Steam Propulsion Plant [Source: US Navy]
Advertisements

OFF DESIGN PERFORMANCE PREDICTION OF STEAM TURBINES
Lecture# 9 MASS AND ENERGY ANALYSIS OF CONTROL VOLUMES
CHAPTER 5: Mass and Energy Analysis of Control Volumes
Performance Analysis of Power Plant Condensers P M V Subbarao Professor Mechanical Engineering Department I I T Delhi A Device Which makes Power Plant.
Irreversibilities : Turbine to Condenser-II
Vapor and Combined Power Cycles
9 CHAPTER Vapor and Combined Power Cycles.
Department of Mechanical Engineering ME 322 – Mechanical Engineering Thermodynamics Lecture 25 Comparison to Carnot’s Heat Engine Effects of Boiling and.
Chapter 1 VAPOR AND COMBINED POWER CYCLES
Yet Another Four Losses in Turbines - 1 P M V Subbarao Professor Mechanical Engineering Department A Set of Losses not Strictly due to Geometry of Blading….
Yet Another Four Losses in Turbines - 2 P M V Subbarao Professor Mechanical Engineering Department A Set of Losses not Strictly due to Geometry of Blading….
The Centrifugal Pump.
A Vapor Power Cycle Boiler T Turbine Compressor (pump) Heat exchanger
Instructional Design Document Steam Turbine. Applied Thermodynamics To study and understand the process of steam flow in impulse and reaction turbine.
Study of Multi Stage Steam Turbines
Power Generation Using Multi Component Working Fluids P M V Subbarao Professor Mechanical Engineering Department Indian Institute of Technology Delhi Synthesis.
Large Steam& Gas Turbines P M V Subbarao Professor Mechanical Engineering Department Backbones of Modern Nations ……
Thermodynamics II Chapter 1 VAPOR POWER CYCLES
Exergy Analysis of STHE P M V Subbarao Professor Mechanical Engineering Department I I T Delhi Formalization of Thermo-economics…..
Vapor and Combined Power Cycles (2)
The First Law of Thermodynamics
Lesson 8 SECOND LAW OF THERMODYNAMICS
Vapour Compression Refrigeration Systems
A Vapor Power Cycle Boiler T Turbine Compressor (pump) Heat exchanger
STEAM TURBINE POWER CYCLES. The vast majority of electrical generating plants are variations of vapour power plants in which water is the working fluid.
Chapter 10 VAPOR AND COMBINED POWER CYCLES
CHAPTER 5: Mass and Energy Analysis of Control Volumes
1 ChemE 260 Improvements and Non-Ideal Behavior in the Rankine Cycle May 20, 2005 Dr. William Baratuci Senior Lecturer Chemical Engineering Department.
Chapter 4 Control Volume Analysis Using Energy. Learning Outcomes ►Distinguish between steady-state and transient analysis, ►Distinguishing between mass.
Chapter 10 Vapor and Combined Power Cycles Study Guide in PowerPoint to accompany Thermodynamics: An Engineering Approach, 7th edition by Yunus.
Chapter 5 MASS AND ENERGY ANALYSIS OF CONTROL VOLUMES
The Rankine Cycle: An Alternate Ideal Thermodynamic Model P M V Subbarao Professor Mechanical Engineering Department IIT Delhi A Feasible Mathematical.
Presentation on Steam Power Plants R.C.Chaturvedi
Meghe Group of Institutions Department for Technology Enhanced Learning 1UNIT IV.
Parametric Study of Turbine Cascades P M V Subbarao Professor Mechanical Engineering Department Identification of New design Variables.……
Heat Transfer by Convection
More Discussions on Irreversible Flow Thorough Multi- stage Turbines P M V Subbarao Professor Mechanical Engineering Department Continuous Opportunities.
Chapter 5 Part 2 Mass and Energy Analysis of Control Volumes Study Guide in PowerPoint to accompany Thermodynamics: An Engineering Approach, 8th edition.
1 Chapter 5 Mass and Energy Analysis of Control Volumes.
First Law of Thermodynamics applied to Flow processes
Review Questions Chapter 5
Chapter 10 VAPOR AND COMBINED POWER CYCLES
Chapter: 06 MASS AND ENERGY ANALYSIS OF CONTROL VOLUMES.
BASICS OF MECHANICAL ENGINEERING
Objectives Evaluate the performance of gas power cycles for which the working fluid remains a gas throughout the entire cycle. Analyze vapor power.
7–12 ISENTROPIC EFFICIENCIES OF STEADY-FLOW DEVICES
Thermodynamics Cycles.
STEAM TURBINES Steam turbine is a device which is used to convert kinetic energy of steam into mechanical energy. In this, enthalpy of steam is first converted.
SNS COLLEGE OF ENGINEERING Coimbatore-107 Subject: Thermal Engineering
prepared by Laxmi institute tech. Mechanical eng. Department.
Simple Thermal Power Plant
TOPIC:- VAPOUR CYCLES CREATED BY:
VAPOR & COMBINED POWER CYCLES
The Multistage Impulse Turbines
Chapter 5 The First Law of Thermodynamics for Opened Systems
Blade Power at Maximum Efficiency COnditions
Chapter 7 Entropy: A Measure of Disorder
9 CHAPTER Vapor and Combined Power Cycles.
Analysis of Multi Stage Steam Turbines
Mass and Energy Analysis of Control Volumes (Open Systems)
SSSF Analysis of Devices Used in Power Generation - II
Design of Steam & Gas Turbines
What is a Turbine ? A Turbine is a device which converts the heat energy of steam into the kinetic energy & then to rotational energy. The Motive Power.
Turbines for Steam Power Plants
Heat Recovery Steam Generators
Condenser in Power Plants
Combined Cycle Power Plants
First Law Analysis of Steam Power Plants
Analysis of Reheat Rankine Cycle
Presentation transcript:

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 …..

The Last Stage of LP Turbine

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.

Governing Stage

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,

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. Average density is calculated as

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.

Internal Reheating due to Irreversibilities 3 Governing group 4Is 4Ia Group 1 Macro available enthalpy: 4IIs 4IIa Group 2 4IIIs 4IIIa Group 3 4IVs T 4IVa Group 4 4Vs 4Va Group 5 4VIs 4VIa Micro available enthalpy: 4s s

Macro available enthalpy: Micro available enthalpy: Reheat Factor:

Internal Reheating due to Irreversibilities : HP 22.33 MPa,3379.0 3 Governing stage 4Is 4Ia 15.74 MPa,3303.0 k J/kg Pho=5 % Stage 1 4IIs 4IIa 13.77 MPa, 3269.0 k J/kg Pho=19.5% Stage 2 4IIIs 4IIIa 12.12 MPa, 3236.5.0 k J/kg Stage 3 Pho=21% 4IVs 4IVa 10.56 MPa, 3203.8 k J/kg T Stage 4 Pho=22% 4Vs 4Va 9.2 MPa, 3171.0 k J/kg Stage 5 Pho=23.5% 4VIs 4VIa 7.94 MPa, 3140.4 k J/kg Stage 6 Pho=25% 4VIIa 6.9 MPa, 3104.9 k J/kg Stage 7 4VIIIa 5.95 MPa, 3070.9 k J/kg Pho=30% Stage 8 4IXa 4s Pho=32% s Pho=35% 5.17 MPa, 3036.7 k J/kg

Cumulative Losses for All Stages : 500 MW

Definition of Efficiency Relative blade efficiency is calculated as: Internal Relative Efficiency is calculated as:

Blade Efficiency & Internal Relative Efficiency: 800 MW

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.

Exhaust Hood

Exhaust Diffuser For L P Turbine

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.

Path Lines in Exhaust Hood

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

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 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.

Typical exhaust loss curve showing distribution of component loss Condenser flow rate Percentage of Moisture at the Expansion line end point SP.Volume Annulus restriction loss Annulus velocity (m/s) Annulus area Total Exhaust Loss 50 Turn-up loss 40 Gross hood loss Exhaust Loss, kJ/kg of dry flow 30 20 Actual leaving loss 10 120 150 180 240 300 360 Annulus Velocity (m/s)

Optimal Design of Exhaust Hood

Performance Analysis of Power Plant Condensers P M V Subbarao Professor Mechanical Engineering Department I I T Delhi A Device Which makes Power Plant A True Cycle.. A Device Which set the limit on minimum cycle pressure…..

T-S Diagram : Rankine Cycle with FWHs.

A Device to Convert Dead Steam into Live Water Water ready to take Rebirth

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.

Two-Pass Surface Condenser

Layouts of A Condenser

Layouts of A Condenser

An Integral Steam Turbine and Condenser System