W P C A. Worldwide Pollution Control Association. WPCA-Entergy Increasing Energy Efficiency of Existing Units Seminar January 22, 2014

Similar documents
Tradition & Technology

V. A. Sedunin 1, O. V. Komarov 1, V. L. Blinov 1, A. V. Skorokhodov 1 & A. O. Procopets 2. Abstract. 1 Introduction

Compressor Seal Replacement and Upgrades SERVICES

Numerical Fluid Analysis of a Variable Geometry Compressor for Use in a Turbocharger

Inlet Swirl on Turbocharger Compressor Performance

WESEP 594 Research Seminar

Application of Sweep to Low Pressure Turbine Cascade Blade for Tip Flow Containment

ASSIGNMENT-1 HYDROPOWER PLANT

THEORETICAL EVALUATION OF FLOW THROUGH CENTRIFUGAL COMPRESSOR STAGE

Flow Through Axial and Centrifugal Compressors by Kartik Sharma Mentors Prof. Gautam Biswas Prof. Subrata Sarkar

Job Sheet 1 Blade Aerodynamics

Citation Journal of Thermal Science, 18(4),

Design and Analysis of a High Pressure Ratio Mixed Flow Compressor Stage

Efficiency Improvement of a New Vertical Axis Wind Turbine by Individual Active Control of Blade Motion

ME1251 THERMAL ENGINEERING UNIT IV AIR COMPRESSORS

TOPICS TO BE COVERED

COMPUTATIONAL FLOW MODEL OF WESTFALL'S LEADING TAB FLOW CONDITIONER AGM-09-R-08 Rev. B. By Kimbal A. Hall, PE

Compressors. Basic Classification and design overview

TEPZZ 6Z4795A T EP A2 (19) (11) EP A2 (12) EUROPEAN PATENT APPLICATION. (43) Date of publication: Bulletin 2013/25

Tip Seal Behavior in Scroll Compressors

ASSIGNMENT-1 HYDROPOWER PLANT

Understanding Centrifugal Compressor Capacity Controls:

Axial and Centrifugal Compressor Mean Line Flow Analysis Method

MECHANICAL EQUIPMENTS: COMPRESSORS, PUMPS, SEALS, SPEED DRIVES, CONTROL VALVES & ACTUATORS & SAFETY RELIEF VALVES

Computational analysis of fish survival at the John Day Powerhouse

(Refer Slide Time: 2:16)

Study of Secondary Flow Modifications at Impeller Exit of a Centrifugal Compressor

XDF BURNERS DUAL FUEL EXCESS AIR BURNER FEATURES DESCRIPTION EXCESS AIR OPERATION

COMPUTER-AIDED DESIGN AND PERFORMANCE ANALYSIS OF HAWT BLADES

Successful Implementation of Dry Gas Seal in High Pressure Recycle gas Compressor at Hydrocracker & Effect of Gas composition on DGS Performance

PRESSURE DISTRIBUTION OF SMALL WIND TURBINE BLADE WITH WINGLETS ON ROTATING CONDITION USING WIND TUNNEL

J. Szantyr Lecture No. 21 Aerodynamics of the lifting foils Lifting foils are important parts of many products of contemporary technology.

System REITHER A Patented Venturi Scrubber

Aerodynamic Analyses of Horizontal Axis Wind Turbine By Different Blade Airfoil Using Computer Program

Návrh vratného kanálu u dvoustupňového kompresoru Return channel design of the two stage compressor

Numerical simulation of radial compressor stages with seals and technological holes

Basic Fluid Mechanics

Evaluation of aerodynamic criteria in the design of a small wind turbine with the lifting line model

Fundamentals of Turboexpanders Basic Theory and Design

AIAA Brush Seal Performance Evaluation. P. F. Crudgington Cross Manufacturing Co. Ltd. Devizes, ENGLAND

Spool Compressor Tip Seal Design Considerations and Testing

Applied Fluid Mechanics

Ameliorating the Negative Damping in the Dynamic Responses of a Tension Leg Spar-Type Support Structure with a Downwind Turbine

AIRFOIL PROFILE OPTIMIZATION OF AN AIR SUCTION EQUIPMENT WITH AN AIR DUCT

MULTISTAGE PUMP EFFICIENCY GAINS THROUGH THE ELIMINATION OF THE SEAL CHAMBER PRESSURE EQUALIZATION LINE

Diaphragm pop-pop engine

TEPZZ 7_687ZA_T EP A1 (19) (11) EP A1 (12) EUROPEAN PATENT APPLICATION. (43) Date of publication: Bulletin 2014/15

Computational studies on small wind turbine performance characteristics

Research on Small Wind Power System Based on H-type Vertical Wind Turbine Rong-Qiang GUAN a, Jing YU b

solids Rotary Valves Type ZRS

DOUBLE-DUCTED FAN CROSS-RELATED APPLICATIONS

CFD SIMULATION STUDY OF AIR FLOW AROUND THE AIRFOIL USING THE MAGNUS EFFECT

Берг АБ Тел. (495) , факс (495) Turning Ideas Into Engineered Solutions KAYDON RING & SEAL, INC.

INVESTIGATION OF PRESSURE CONTOURS AND VELOCITY VECTORS OF NACA 0015IN COMPARISON WITH OPTIMIZED NACA 0015 USING GURNEY FLAP

EFFECT OF LEADING EDGE SWEEP ON THE PERFORMANCE OF A CENTRIFUGAL COMPRESSOR IMPELLER. Abstract 1. INTRODUCTION

Variable Volume-Ratio and Capacity Control in Twin-Screw Compressors

EFFECTIVE DESIGN OF CONVERTER HOODS. 111 Ferguson Ct. Suite 103 Irving, Texas U.S.A. 400 Carlingview Dr. Toronto, ON M9W 5X9 Canada.

AERODYNAMIC TIP DESENSITIZATION OF AN AXIAL TURBINE ROTOR USING TIP PLATFORM EXTENSIONS

INTRODUCTION 1.0 GENERAL

Influence of the Number of Blades on the Mechanical Power Curve of Wind Turbines

Chapter 2 Pump Types and Performance Data

Multistage pump efficiency gains through the elimination of the seal chamber pressure equalization line

Nuclear Engineering and Design

Axial and Radial Force Control for CO2 Scroll Expander

Pushing the Boundaries of UpFront CFD. Sean Horgan and Mike Clapp 80/20 Engineering Ltd

An Impeller Blade Analysis of Centrifugal Gas Compressor Using CFD

Pressure distribution of rotating small wind turbine blades with winglet using wind tunnel

Use of a Tracer Gas Technique to Study Mixing in a Low Speed Turbine

Numerical analysis of influence of streamline rudder on screw propeller efficiency

Development and evaluation of a pitch regulator for a variable speed wind turbine PINAR TOKAT

NEW POLYTECHNIC, KOLHAPUR

Case study. Rotating Equipment Engineer Qatargas Operating Company. Sr. Rotating Equipment Engineer

Influencing Factors Study of the Variable Speed Scroll Compressor with EVI Technology

Grid Generation for Screw Compressors with Variable Geometry Rotors

Structure of Mechanically Agitated Gas-Liquid Contactors

Effects of Air Injection on Aerodynamic Performance of a Single-Stage Transonic Axial Compressor

Assessing Fish Condition After Passage Through Conventional and Fish-Friendly Turbines Using a Release Recapture Technique

Self-Aligning Cylindrical Roller Bearings. Plummer Block Housing. Series ACB, sealed on both sides. Series SLG01

Design of a Partial Admission Impulse Turbine for an Automotive ORC-Application. Harald S. Kunte, Joerg R. Seume

Rotary vane steering gear for smaller vessels

Another convenient term is gauge pressure, which is a pressure measured above barometric pressure.

Casing wall static pressure distribution behavior in a centrifugal compressor with asymmetric inlet/outlet structures

Numerical Analysis of the Tip Leakage Flow Field in a Transonic Axial Compressor with Circumferential Casing Treatment

Rotary air valves used for material feed and explosion protection are required to meet the criteria of NFPA 69 (2014)

SHROUD CONTOUR OPTIMIZATION FOR A TURBOCHARGER CENTRIFUGAL COMPRESSOR TRIM FAMILY

Design of Naca63215 Airfoil for a Wind Turbine

Development of Technology to Estimate the Flow Field around Ship Hull Considering Wave Making and Propeller Rotating Effects

EXPERIMENTAL ANALYSIS OF FLOW OVER SYMMETRICAL AEROFOIL Mayank Pawar 1, Zankhan Sonara 2 1,2

A Research on the Airflow Efficiency Analysis according to the Variation of the Geometry Tolerance of the Sirocco Fan Cut-off for Air Purifier

Pump Selection and Sizing (ENGINEERING DESIGN GUIDELINE)

The Quarter Pounder A Vehicle to Launch Quarter Pound Payloads to Low Earth Orbit

Streakline Flow Visualization Study of a Horseshoe Vortex in a Large-Scale, Two-Dimensional Turbine Stator Cascade

Computational fluid dynamics analysis of a mixed flow pump impeller

Gas Measurement Fundamentals Certification. Curriculum

IAI WARNING! INSTRUCTION MANUAL TO REDUCE THE RISK OF INJURY, USER MUST READ AND UNDERSTAND THIS INSTRUCTION MANUAL. ORIGINAL INSTRUCTIONS

ASME International Mechanical Engineering Congress & Exhibition IMECE 2013 November 15-21, 2013, San Diego, California, USA

CHAPTER-2 IMPACT OF JET

OPTIMIZATION OF SINGLE STAGE AXIAL FLOW COMPRESSOR FOR DIFFERENT ROTATIONAL SPEED USING CFD

Wind Energy Technology. What works & what doesn t

TUTORIAL: SURGE CONTROL AND DYNAMIC BEHAVIOR FOR CENTRIFUGAL GAS COMPRESSORS

Transcription:

Worldwide Pollution Control Association WPCA-Entergy Increasing Energy Efficiency of Existing Units Seminar January 22, 2014 All presentations posted on this website are copyrighted by the Worldwide Pollution Control Association (WPCA). Any unauthorized downloading, attempts to modify or to incorporate into other presentations, link to other websites, or to obtain copies for any other purposes than the training of attendees to WPCA Conferences is expressly prohibited, unless approved in writing by the WPCA or the original presenter. The WPCA does not assume any liability for the accuracy or contents of any materials contained in this library which were presented and/or created by persons who were not employees of the WPCA. Visit our website at www.wpca.info W P C A

Ways to Increase Turbine Efficiency and Improve Heat Rate Jim Auman Steam Turbine Engineering 2004. All Rights Reserved

Improving Efficiency and Heat Rate 3D Reaction Airfoils (Bowed) - Increased Stage Count - Reaction versus Impulse Designs - Proven Efficiency Improvement Advanced Control Stage Design Optimized Sealing Technology - Labyrinth Blade Path Seals - Spring-back and Retractable Seals - Sustainable Clearances Reduce Potential Leakage Paths Select LP Annulus Area for Best Efficiency 2

Industry Development of Airfoils Cylindrical Airfoil (since early 1900 s) constant profile section Twisted Airfoil (since late 70 s) variable profile sections adjustment to variable flow angles reduction of incidence loss 3D (since late 90 s) variable profile sections application of tangential lean or bow influence on radial pressure gradient reduction of secondary losses 3

3DV TM Current Generation Bowed Blading 3DS TM 3D with reduced Secondary losses 2 nd generation of advanced 3D blading based on twisted blades superimposed compound lean (bow) 3DV TM 3D blading with Variable stage reaction 3rd generation of advanced 3D blading based on 3DS blades optimized load distribution within the blade path achieve maximum overall blade path efficiency 4

3DS TM Blading Reduced Secondary Losses Modern 3DS TM blade η % > 2 % Cylindrical blading 3DS TM Blading Late 1990 s 3DS TM blading 2% efficiency improvement ψ 5

3DS TM Blading Pictorial 6

Advanced Control Stage Technology Past Features Turn around control stage Bolted on nozzle block Current - World Class Features Straight thru control stage Increased Impulse Chamber P & T Riveted, side entry rotating blade New, increased pitch airfoil section prevents HCF induced vane chipping Vane chipping calculation Improved airfoil profile design Contoured endwall nozzle Slide in nozzle block Triple pin rotating blade Improved materials Est. up to +3-5% CS η over Past Designs Modernized triple pin blade Contoured endwall Close pitch nozzles Increased pitch 7

Comparison of Blade Design Principles Impulse Stage 50% Reaction Stage V 1R V 1 U V 1R V 1 U V 2R V 2 U Fixed blade row accelerates the steam Moving blade row changes only the direction of the steam - High Work per Stage V 2R U V 2 Fixed blade row accelerates the steam Moving blade row changes both the speed and direction of the steam - Lower Peak Steam Velocity V1 - High Stage Count for Efficiency 8

Blade Path Sealing Technology HP Small Axial Expansion LP Large Axial Expansion Casing Casing Rotating Blade Rotating Blade Seal Optimization with Modern CFD-Tools Stationary Blade Stationary Blade Rotor Rotor 9

Sealing Technology Retractable Dummy Seal Rings TurboCare Retrofit: Brush Seals in Impulse Blade Path Benefits Reduction in leakage flow Improved efficiency Favorable wear behavior characteristics 10

Turbine Technology LP Last Stage Design Features L-0R Design Features Freestanding L-0 Full 3D Design Thin Trailing Edge Fir Tree Root Design Supersonic Airfoil Flame Hardened Leading Edges L-0C Design Features Thin Trailing Edge Welded Diaphragms Full 3D Design for optimum radial flow distribution and low exhaust loss Hollow Vanes Moisture Suction 11

Efficiency Improvement Summary 3D Reaction Airfoils (Bowed) - Increased Stage Count - Reaction versus Impulse Designs - Proven Efficiency Improvement Advanced Control Stage Design Optimized Sealing Technology - Labyrinth Blade Path Seals - Spring-back and Retractable Seals - Sustainable Clearances Reduce Potential Leakage Paths Select LP Annulus Area for Best Efficiency 12

Implementing New Technology for Improved Efficiency and Heat Rate Retrofit Turbine Modules 13

Improving Efficiency and Heat Rate Questions? 14