Gas Turbine Power Plant

Similar documents
Basic Requirements. ICE Fuel Metering. Mixture Quality Requirements. Requirements for Metering & Mixing

1 In all circumstances, it can be easily ignited by the spark. 2 The maximum possible amount of chemical energy can be

Gas Power System. By Ertanto Vetra

(a) then mean effective pressure and the indicated power for each end ; (b) the total indicated power : [16]

Idealizations Help Manage Analysis of Complex Processes

CONCEPTUAL DESIGN OF A NEW TYPE OF ENGINE FOR VARIOUS APPLICATIONS WITH EXPECTED 10% HIGHER OVERALL EFFICIENCY

MEB THERMAL ENGINEERING - I QUESTION BANK UNIT-I PART-A

Power Cycles. Ideal Cycles, Internal Combustion

Content : 4.1 Brayton cycle-p.v. diagram and thermal efficiency. 4Marks Classification of gas turbines.

Mohammad Faisal Haider. Department of Mechanical Engineering Bangladesh University of Engineering and Technology

UNIT 1 GAS POWER CYCLES

Gas Power Cycles. Tarawneh

SIDDHARTH INSTITUTE OF ENGINEERING & TECHNOLOGY :: PUTTUR (AUTONOMOUS) QUESTION BANK UNIT I I.C ENGINES

VALVE TIMING DIAGRAM FOR SI ENGINE VALVE TIMING DIAGRAM FOR CI ENGINE

Process 1-2: Reversible adiabatic compression process. Process 2-3: Reversible isothermal heat addition

Performance Enhancement of Multi-Cylinder Common Rail Diesel Engine for Automotive Application

Chapter 9 GAS POWER CYCLES

Thermodynamic Cycles. Alicia Ma. Esponda Cascajares

CHAPTER I GAS POWER CYCLES

Chapter 9 GAS POWER CYCLES

Chapter 8 Production of Power from Heat

PROCESS ECONOMICS PROGRAM

AC Motors vs DC Motors. DC Motors. DC Motor Classification ... Prof. Dr. M. Zahurul Haq

ME3264: LAB 9 Gas Turbine Power System

Dipl.-Ing. Frank Pflüger. A new charging system for commercial diesel engines. Academy

1. (a) If a large power generating station is operating with steam at 16,000 kpa and 500 and exhausting to a condenser at, 37.6 mm mercury absolute;

Did you know? If you follow the maintenance guidelines for your vehicle, your turbo will last longer.

Scheme G Sample Question Paper Course Name : Diploma in Automobile Engineering Course Code : AE

Class Notes on Thermal Energy Conversion System

First Law Analysis of a DI Diesel Engine Running on Straight Vegetable oil

Scheme - G. Sample Test Paper-I. Course Name : Diploma in Mechanical Engineering Course Code : ME Semester : Fifth Subject Title : Power Engineering

Thermodynamics II MIDTERM MECH 351/2 Fall 06 CONCORDIA UNIVERSITY FACULTY OF ENGINEERING AND COMPUTER SCIENCE DEPARTMENT OF MECHANICAL ENGINEERING

Hours / 100 Marks Seat No.

The Internal combustion engine (Otto Cycle)

BASIC CIVIL & MECHANICAL ENGINEERING

Combustion engines. Combustion

Gas Turbine Power Plant Mr.B.Ramesh, M.E.,(Ph.D)

So how does a turbocharger get more air into the engine? Let us first look at the schematic below:

Attention is drawn to the following places, which may be of interest for search:

When should an Electric Adjustable Speed Drive be used instead of a Gas or Steam Turbine? Paul Blaiklock, Manish Verma, Stephan Bondy

(v) Cylinder volume It is the volume of a gas inside the cylinder when the piston is at Bottom Dead Centre (B.D.C) and is denoted by V.

Engine Cycles. T Alrayyes

Synergies and Differences between Fossil- and Solar-Powered Cycles

Internal Combustion Engines

4. With a neat sketch explain in detail about the different types of fuel injection system used in SI engines. (May 2016)

USO4CICV01/US04CICH02:

KISSsys Application 008: Gearbox Concept Analysis

Asian Marine Engineering Conference 2015 MAN Diesel & Turbo SE Turbocharger. Malte Oltmanns Promotion Manager October 2015

Powertrain Efficiency Technologies. Turbochargers

Week 10. Gas Power Cycles. ME 300 Thermodynamics II 1

Turbo Tech 101 ( Basic )

Sustainable Energy Mod.1: Fuel Cells & Distributed Generation Systems

L34: Internal Combustion Engine Cycles: Otto, Diesel, and Dual or Gas Power Cycles Introduction to Gas Cycles Definitions

Comparison of Air-Standard Atkinson, Diesel and Otto Cycles with Constant Specific Heats

Design and Fabrication of Simple Turbo Alternator

ME2301 THERMAL ENGINEERING L T P C OBJECTIVE:

SUGAR MILL DRIVES. The Variable Speed Drive with Limited Speed Range. Constant Speed Drives. A Cane Mill Drive. Variable Speed over a Wide Range

Smart Grid Technology Principle and Application Smart Grid Measurement and Control

Analysis of Sequential Turbocharger Systems for Diesel Engines Rob Stalman, Vanco Smiljanowski, Uwe Späder, Ford Research & Advanced Europe

Earlier Lecture. For an optimum design of a Stirling cryocooler, a compromise between the operating and the design parameters may be sought.

ISO 1217 INTERNATIONAL STANDARD. Displacement compressors Acceptance tests. Compresseurs volumétriques Essais de réception. Fourth edition

Attention is drawn to the following places, which may be of interest for search:

η th W = Q Gas Power Cycles: Working fluid remains in the gaseous state through the cycle.

FLUID DYNAMICS TRANSIENT RESPONSE SIMULATION OF A VEHICLE EQUIPPED WITH A TURBOCHARGED DIESEL ENGINE USING GT-POWER

GCE AS and A Level. Physics A. AS exams 2009 onwards A2 exams 2010 onwards. Unit 5C: Approved specimen question paper. Version 1.1

Noble Group of Institutions, Junagadh. Faculty of Engineering Department of Mechanical Engineering

Thermodynamics cycles can be classified into different categories depending on fluid used or the different processes:

If you like us, please share us on social media. The latest UCD Hyperlibrary newsletter is now complete, check it out.

Mechanism Feasibility Design Task

Basic Steam Locomotive Action

Unit 32 Three-Phase Alternators

S C&e. United States Patent (19) Hall. 11) 4,051, Oct. 4, 1977 (54) MODIFIED RANKINE CYCLE ENGINE

Product Manual (Revision A) Original Instructions. Manifold Gauge Pressure Fuel Limiter for PG Governors. Operation Manual

Consultant Jim Berry, USA, discusses the ways in which dual driven pipeline compressors can offer flexible and cost-saving operational modes.

ACTUAL CYCLE. Actual engine cycle

(Refer Slide Time: 1:13)

2. Turbocharger System

By Shridevi Bhat 13/02/2016

ME Thermal Engineering Question Bank

KINGS COLLEGE OF ENGINEERING DEPARTMENT OF MECHANICAL ENGINEERING. Question Bank. UNIT-I THERMODYNAMIC CYCLES Part-A (2 Marks)

INTERNAL COMBUSTION ENGINE (SKMM 4413)

7,15 436, Bore , ,12 Compression ratio. 17 Wet weight

GYANMANJARI INSTITUTE OF TECHNOLOGY (GMIT) SUBJECT: ELEMENTS OF MECHANICAL ENGINEERING Assignment Ch 1

7,15 436, Bore , ,12 Compression ratio. 18 Wet weight

Increasing Low Speed Engine Response of a Downsized CI Engine Equipped with a Twin-Entry Turbocharger

WINTER 14 EXAMINATION

Mathcad Assignment System Calculation. Dr Malcolm W. Renton

1.1 Block Diagram of Drive Components of Electric Drive & their functions. Power Processor / Modulator. Control. Unit

Sustainable Energy Mod.1: Fuel Cells & Distributed Generation Systems

UNIVERSITY POLYTECHNIC B.I.T., MESRA, RANCHI

Development of Low-Exergy-Loss, High-Efficiency Chemical Engines

2.61 Internal Combustion Engines

USE OF A THERMODYNAMIC ENGINE CYCLE SIMULATION TO STUDY A TURBOCHARGED SPARK-IGNITION ENGINE

Abstract IJERTV2IS International Journal of Engineering Research & Technology (IJERT) ISSN: Vol. 2 Issue 9, September

A REVIEW ON STIRLING ENGINES

BASIC CONSIDERATIONS IN POWER CYCLE ANALYSIS THERMODYNAMICS CHAPTER 9

Turbocharger Compressor Calculations


REPORT DOCUMENTATION PAGE

Aerospace Propulsion Systems

Transcription:

Gas Turbine Power Plant Dr. M. Zahurul Haq Professor Department of Mechanical Engineering Bangladesh University of Engineering & Technology (BUET) Dhaka-1000, Bangladesh zahurul@me.buet.ac.bd http://teacher.buet.ac.bd/zahurul/ ME 403: Power Plant Engineering Gas turbines have these advantages over steam plants: They are small in size, mass, and initial cost per unit output. Their delivery time is relatively short and they can be installed quickly. They are quick starting (as low as 10 s), often by remote control. They are smooth running and have a capacity factor (percent of time the unit is operating at full power) of 96 to 98 percent. They can use a wide variety of liquid and gaseous fuels including gasified coal and synthetic fuels. They are subject to fewer environmental restrictions than other prime movers. c Dr. M. Zahurul Haq (BUET) Gas Turbine ME 403 (2015) 1 / 25 c Dr. M. Zahurul Haq (BUET) Gas Turbine ME 403 (2015) 2 / 25 T401 Schematic layout of a single-shaft gas turbine. T371 A comparison between the working cycle of a turbo-jet engine and a piston engine. T402 Schematic layout of a two-shaft gas turbine. c Dr. M. Zahurul Haq (BUET) Gas Turbine ME 403 (2015) 3 / 25 c Dr. M. Zahurul Haq (BUET) Gas Turbine ME 403 (2015) 4 / 25

T403 T404 Representation of a simple cycle gas turbine. Representation of gas turbine cycle on temperature-entropy diagram. T405 Effect of pressure ratio on the temperature-entropy diagram for an ideal gas turbine cycle when T 3 is constant. c Dr. M. Zahurul Haq (BUET) Gas Turbine ME 403 (2015) 5 / 25 c Dr. M. Zahurul Haq (BUET) Gas Turbine ME 403 (2015) 6 / 25 T406 T407 T408 Variation of thermal efficiency and specific work with compressor pressure ratio. Schematic representation of a regenerative cycle. Heat transfer for a regenerative gas turbine cycle. c Dr. M. Zahurul Haq (BUET) Gas Turbine ME 403 (2015) 7 / 25 c Dr. M. Zahurul Haq (BUET) Gas Turbine ME 403 (2015) 8 / 25

T409 Effect of T 4 and pressure ratio on the thermal efficiency of a regenerative cycle. The limiting pressure ratios when T 5 = T 2 are shown. T410 Ideal and actual compression and expansion processes on the temperature-entropy diagram. c Dr. M. Zahurul Haq (BUET) Gas Turbine ME 403 (2015) 9 / 25 c Dr. M. Zahurul Haq (BUET) Gas Turbine ME 403 (2015) 10 / 25 T411 Variation of the isentropic efficiency with pressure ratio for a polytropic efficiency of 0.87. T412 Combustion temperature rise versus fuel-air ratio. c Dr. M. Zahurul Haq (BUET) Gas Turbine ME 403 (2015) 11 / 25 c Dr. M. Zahurul Haq (BUET) Gas Turbine ME 403 (2015) 12 / 25

T413 T414 Simple gas turbine thermal efficiency varying with pressure ratio. Performance of a practical simple gas turbine cycle as a carpet plot for a series of maximum cycle temperatures and pressure ratios. c Dr. M. Zahurul Haq (BUET) Gas Turbine ME 403 (2015) 13 / 25 c Dr. M. Zahurul Haq (BUET) Gas Turbine ME 403 (2015) 14 / 25 T418 Schematic representation of an intercooled gas turbine. T417 Carpet plot for a regenerative gas turbine cycle. T419 Two-stage intercooled compression process on the temperature-entropy diagram. c Dr. M. Zahurul Haq (BUET) Gas Turbine ME 403 (2015) 15 / 25 c Dr. M. Zahurul Haq (BUET) Gas Turbine ME 403 (2015) 16 / 25

T420 Variation of thermal efficiency with specific work for a practical intercooled gas turbine when optimised for maximum thermal efficiency. c Dr. M. Zahurul Haq (BUET) Gas Turbine ME 403 (2015) 17 / 25 T421 Schematic representation of an intercooled, regenerative gas turbine cycle. c Dr. M. Zahurul Haq (BUET) Gas Turbine ME 403 (2015) 18 / 25 T423 T422 Temperature-entropy diagram for the intercooled and nonintercooled, regenerative gas turbine cycles. c Dr. M. Zahurul Haq (BUET) Gas Turbine ME 403 (2015) 19 / 25 Variation of thermal efficiency with specific work for a practical intercooled, regenerative gas turbine cycle c Dr. M. Zahurul Haq (BUET) Gas Turbine ME 403 (2015) 20 / 25

T424 T427 Schematic representation of a reheat gas turbine. Variation of thermal efficiency with specific work when optimised for maximum thermal efficiency. c Dr. M. Zahurul Haq (BUET) Gas Turbine ME 403 (2015) 21 / 25 c Dr. M. Zahurul Haq (BUET) Gas Turbine ME 403 (2015) 22 / 25 T429 Schematic representation of a reheat-regenerative gas turbine. T430 Schematic representation of an intercooled, reheat and regenerative cycle. c Dr. M. Zahurul Haq (BUET) Gas Turbine ME 403 (2015) 23 / 25 c Dr. M. Zahurul Haq (BUET) Gas Turbine ME 403 (2015) 24 / 25

T433 Variation of thermal efficiency with specific work for practical intercooled, reheat and regenerative (ICRHR) cycle. c Dr. M. Zahurul Haq (BUET) Gas Turbine ME 403 (2015) 25 / 25

2024 © autodocbox.com Privacy Policy | Terms of Service | Feedback