40TH IIEE ANNUAL NATIONAL CONVENTION AND 3E XPO 2015 SMX Convention Center, Mall of Asia Complex, Pasay City
November 25 - 28, 2015
IIEE@40: A Journey of Service for Excellence
Gas Turbine Combined Cycle Power System Technical Presentation by
Engr. Enrique I. Flores, PEE IIEE State of Qatar Chapter
What is a Gas Turbine Combined Cycle? A combined-cycle power plant uses both gas turbines and a steam turbine together to produce up to 50 percent more electricity from the same fuel than a traditional simple-cycle plant. The waste heat from the gas turbine exhaust routed directly to the heat recovery steam generator to produce steam and routed to the nearby steam turbine which generates extra power.
Combined Cycle Power Plant
GTCC Power System 1.) Fuel Tanks or Natural Gas Facility 2.) Black Start System 3.) Gas Turbine Units 4.) Heat Recovery Steam Generators 5.) Steam Turbine Unit 6.) Main and Auxiliary Transformers 7.) Local and Central Control Room 8.) Feed Water System 9.) Main Condenser 10.) Main Cooling Water System 11.) High Voltage Switchyard 12.) Other Balance of Plant (BOP)
Gas Turbine Combined Cycle Efficiency GAS TURBINE = 30 – 33%
COMBINED CYCLE = 20 – 25% TOTAL NET EFFICIENCY = 50 – 60%
World Record Highest Efficiency
The 600 MW Combined Cycle Power Plant Irsching 4 by Siemens achieved a world record highest efficiency of 60.75 (net) in May 2011 in Erlargen Germany
Bataan Combined Cycle Power Plant Philippines
The 600 MW Combined Cycle Power Plant in Limay Bataan Philippines was the first of its kind in the Philippines commissioned in 1992 as a fast track project during the nation wide black-outs in our country due to lack of power plants to support the booming economy.
Efficiency of Power Plants
Gas Turbine = 26% - 33% Diesel Generator = 39% - 45% Combined Cycle (Dual Pressure) = 38% - 47%
E-Development
FUEL SUPPLY SYSTEM
Standard Fuel for GT 1.) Jet A/Kerosene 2.) Natural Gas 3.) Distillate (including No.2 Fuel oil and Diesel oil)
Natural Gas Supply
Standard Natural Gas Storage Tank
Natural Gas Supply
Gas Pressure Reducing Station: It reduces the natural gas pressure supplied by the Oil Refineries to the gas pressure required by the Gas Turbine Units . For example: From 70 Bars to 30 Bars.
Natural Gas Supply
Japan is the highest importer of LNG.
Natural Gas Supply
Global gas imports is increasing fast.
Diesel Fuel Tank Facility
Consist of the following components: 1.) Diesel Fuel Tank Farm 2.) Fuel Treatment Facility 3.) Fuel Forwarding Pumps 4.) Fuel Pipe Lines
Fuel Treatment Plant
Electrostatic Separator is a descriptive term of Baker, which means the treatment of crude oil through mixture of water and high voltage current. So far the measurement has been widely used and agreed in oil refining industry and turbine power stations worldwide. Because fractions of metallic contaminations, especially Na, K, V and Pb, exist in fuel oil, they frequently suffer to high temperature erosion and fouling. In the process of combustion, these impurities will form mixed dust subject in low melting point, which can cohere with the metallic parts in the hot gas path. With the accumulation of these melted dust subjects on thermalloy material, high temperature erosion will happen and as a result, will lead parts to failure.
Diesel Fuel Tank
Fuel Tank Protections 1.) Lightning arresters 2.) Flame Detectors 3.) Foam spray inside the tank 4.) Deluge Cooling water spray outside and around the tank 5.) Grounding System 6.) Tank overflow 7.) Containment Wall 8.) Fire Fighting Equipment
Deluge Fire Protection Skid
Deluge Fire Pumps
Tank Farm On Fire
Common cause of Fuel Tanks fire: 1.) Lightning strikes 2.) Human or operators error 3.) Fuel pipe line leaks
BLACK START SYSTEM
What is a Black Start System? It is the process of starting or restoring an electric power station to operation without relying on the external transmission network. This normally happens during total loss of power in the grid on a bad weather. In order to have a black start capability, most power plants have a dedicated diesel generator of 2MW to 5MW capacity called the Black Start Diesel Generator (BSDG), which can be used to restart back the first gas turbine generator and its auxiliaries back in service which will in turn provide enough supply of power to start the other remaining gas turbines to restore back the whole Power Plant during black out condition.
Black Start Diesel Generator
Consist of the following components: 1.) Diesel Engine 2.) Generator (2MW – 5 MW) 3.) Air Starting System (Small Diesel Engine Driven) 4.) Synchronizing and Monitoring Equipment
GAS TURBINE
What is a Gas Turbine? A gas turbine, also called a combustion turbine, is a type of internal combustion engine. It has an upstream rotating compressor coupled to a downstream turbine, and a combustion chamber in between. The gas turbine is the heart of the power plant. A gas turbine is a combustion engine that can convert natural gas or other liquid fuels to mechanical energy which then drives a generator that produces electrical energy or power output.
Gas Turbine Unit
Consist of the following components: 1.) Air Intake System 5.) Starting Unit 2.) Compressor and Blow-off 6.) Shaft and Bearings 3.) Turbine 8.) Exhaust Stack 4.) Generator 9.) Local Control Room
Gas Turbine Main Parts
Gas Turbine Unit
Combustion Chamber and Turbine
Gas Turbine Range
ABB Gas Turbine MW Range
Gas turbine technology Gas turbine power flow Exhaust gas
Power turbine Pt
Combustion chamber Pth
Compressor air
Pk
gearbox
generator
Pm
Liquid fuel
Pel
Pch Pt = Pk + Pm
Chemical power
Thermal power
Mechanical power
Electrical power
Global efficiency = Pel/Pch 33
Industrial Gas Turbine
Consist of the following main components: 1.) Inlet Air 2.) Compressor 3.) Combustion Chamber 4.) Turbine 5.) Exhaust
Gas Turbine compared to 4-stroke Engine
Admission
Compression
Combustion
Exhaust
Consist of the following steps: 1.) Admission – Admits mixture of air and fuel in to the cylinder. 2.) Compression – Compressed air using stages of blades. 3.) Combustion – Mixed compressed air and fuel then ignited to produce mechanical work. 4.) Exhaust – Hot gas is being released to the exhaust stack or to the steam boiler.
Gas Turbine
Gas Turbine Powered Car
Progress in blade metals
Gas Turbine Blade Damaged
Gas turbine rotor blades damaged by blade rubbing due to high vibrations. High vibrations can cause the rotor blades to rub against the turbine casing.
Gas Turbine Blade Metal Nickel base super alloys are used in the most demanding portions of the turbine engine, where a wide balance of high strength, high toughness, oxidation and corrosion resistance, temperature capability, and process ability are all needed. The blades used in the high pressure turbine rotor are subjected to a stringent set of requirements including a balance of creep resistance, temperature capability, environmental resistance, and damage tolerance. In today's engines, blade performance and durability is achieved through advanced super alloy single crystals combined with sophisticated internal cooling schemes and thermal barrier coatings.
Research is directed towards further advances in new alloys, where low density alloys with improved strength at temperatures exceeding 1100°C have been discovered.
Turbine Bearings
Axial Thrust Bearing Bearing No.1 Air Inlet Assembly
Radial Journal Bearing Bearing No.2 and 3 Combustor Assembly
Gas Turbine Starting Unit
Gas Turbine Starter is equipped with two starter motors used for turbine start-up and is used to drive the mechanical main oil pump. It has a gear box to reduce the drive speed of 14,950 rpm from the turbine to generator speed of 1500 rpm.
Gas Turbine Starting Unit The Gas Turbine Unit has the main function the following: 1.) To put the turbine in rotation to reach ignition speed (25 % of nominal speed). 2.) When combustion occurs, it supports the acceleration of the turbine.
3.) When turbine reached 66 % of nominal speed the starter motor is de-energised. The turbine will be at self sustaining speed to reach 100% or full speed.
Gas Turbine Starting Unit
Gas Turbine Static Frequency Converter (SFC) uses the synchronous generator of the gas turbine to operate it as a motor to run up to ignition speed and self sustaining speed.
Gas Turbine Generator
Consist of the following components: 1.) Rotor Winding 5.) Output Terminals 2.) Stationary Winding 6.) Bearings 3.) Exciter 7.) Shaft 4.) Diodes
GT Local Control Room
Control, Monitoring and Protections
Central Control Room
Control, Monitoring and Protections
Central Control Room
Typical Central Control Room Operator
Gas Turbine Protections 1.) Pedestal bearing vibrations >Max. 2.) Thrust bearing vibrations >Max. 3.) Turbine casing vibration >Max. 4.) Electronic over speed >110% 5.) Mechanical over speed >112% 6.) Turbine Inlet Temperature (TIT) 7.) Temperature After Turbine (TAT) 8.) Lube pressure and level Max. 3.) HP/LP Drum Level >Max. 4.) HP/LP Drum Level