54
Gas Turbine Gas Turbine Technologies Technologies for Electric for Electric Generation Generation by Rob Shepard, P.E. www.Neel-Schaffer.com rob.shepard@neel- schaffer.com

MS3-ASME Gas Turbine Technologies Presentation

Embed Size (px)

DESCRIPTION

related to gas turbines

Citation preview

Gas Turbine TechnologiesGas Turbine Technologiesfor Electric Generationfor Electric Generation

by

Rob Shepard, P.E.

www.Neel-Schaffer.com

[email protected]

2

Gas Turbine Basics

Gas Turbines Types How They Work Applications Components of Plant Flow Paths Operation

3

Gas Turbine Applications

Simple Cycle Combined Cycle Cogeneration

4

Types of Gas Turbine Plants

Simple Cycle Operate When Demand is High – Peak Demand Operate for Short / Variable Times Designed for Quick Start-Up Not designed to be Efficient but Reliable

Not Cost Effective to Build for Efficiency

Combined Cycle Operate for Peak and Economic Dispatch Designed for Quick Start-Up Designed to Efficient, Cost-Effective Operation Typically Has Ability to Operate in SC Mode

5

The energy contained in a flowing ideal gas is the sum of enthalpy and kinetic energy.

Pressurized gas can store or release energy. As it expands the pressure is converted to kinetic energy.

Principles ofOperation

Open CycleAlso referred to as simple cycle)

Link to picture

6

Brayton Cycle – Gas Turbine Cycle

7

Thermodynamic Fundamentals Pressure Ratio &

CT Components

8

Combustion or Gas Turbine

9

Principles of Operation

Compressor As air flows into the compressor, energy is transferred from its

rotating blades to the air. Pressure and temperature of the air increase.

Most compressors operate in the range of 75% to 85% efficiency.

Combustor The purpose of the combustor is to increase the energy stored in

the compressor exhaust by raising its temperature.

Turbine The turbine acts like the compressor in reverse with respect to

energy transformation.

Most turbines operate in the range of 80% to 90% efficiency.

10

Principles of Operation Overall Energy Transformations (Thermal Efficiency)

Useful Work = Energy released in turbine minus energy absorbed by compressor.

The compressor requires typically approximately 50% of the energy released by the turbine.

Overall Thermal Efficiency = Useful Work/Fuel Chemical Energy *100

Typical overall thermal efficiencies of a combustion turbine are 20% - 40%.

11

Gas Turbine Applications

Simple Cycle

Link to picture

12

Simple Cycle Power PlantWestinghouse 501D5 – 340 MW

13

Combined Cycle Power Plant

14

Combined Cycle Plant DesignGT PRO 13.0 Drew Wozniak

1512 10-13-2004 23:27:31 file=C:\Tflow13\MYFILES\3P 0 70.gtp

Net Power 95959 kWLHV Heat Rate 7705 BTU/kWh

p[psia], T[F], M[kpph], Steam Properties: Thermoflow - STQUIK

4.717 m Fogger

1X GE 6581B 2 X GT

33781 kW

12.54 p 90 T 30 %RH 944 m 4327 ft elev.

12.39 p 68 T 948.7 m

Natural gas 18.58 m

96 T 77 TLHV 369671 kBTU/h

149.2 p 684 T

143.2 p 2072 T

967.3 m

12.93 p 1034 T 1934.6 M

73.85 %N2 13.53 %O2 3.233 %CO2+SO2 8.497 %H2O 0.8894 %Ar

1031 T 1934.6 M

1031 897 569 568 538 534 481 419 326 268

268 T 1934.6 M

30813 kW

0.1296 M

FW

1.694 p 120 T 222.1 M

120 T

Natural gas 0 M

122 T 292.6 M

122 T 17.19 p 220 T

29.58 M

17.19 p 220 T 29.65 M

LPB

29.65 M 292.6 M

203.6 p 373 T 292.6 M

IPE2

203.6 p 383 T 36.75 M

IPB

199.7 p 460 T 36.75 M

IPS1

195.8 p 500 T 36.75 M

IPS2

924.2 p 472 T 251.1 M

HPE2

910.5 p 523 T 251.1 M

HPE3

910.5 p 533 T 248.6 M

HPB1

879.8 p 954 T 248.6 M

HPS3

850 p 950 T 248.6 M

879.8 p 954 T

6.89 M

183 p 375 T 70 M V4

26.36 M 195.8 p 597 T

V8

6.89 M

15

Gas Turbine ComponentsCompressor – Combustor - Turbine

16

Gas Turbine Components & Systems (cont’d)

Combustion System Silo, Cannular, Annular Water, Steam, DLN

Turbine Multiple Shaft, Single

Shaft Number of Stages Material and

Manufacturing Processes

Exhaust System Simple Cycle Stack Transition to HRSG

Generator Open-Air cooled TEWAC Hydrogen Cooled

Starting Systems Diesel Motor Static

Paper Towel thru compressor

17

Combustion Turbine Fuels

Conventional Fuels Natural Gas Liquid Fuel Oil

Nonconventional Fuels Crude Oil Refinery Gas Propane

Synthetic Fuels Chemical Process Physical Process

18

GE Combustion Turbine Comparisons

19

Parameter Heavy Duty Aero-Derivative

Capital Cost, $/kW Lower Higher

Capacity, MW 10 - 330 5 – 100

Efficiency Lower Higher

Plan Area Size Larger Smaller

Maintenance Requirements Lower Higher

Technological Development Lower Higher

Advanced Heavy-Duty Units Advanced Aeroderivative Units

Gas Turbine Types

20

Gas Turbine Major Sections

Air Inlet Compressor Combustion System Turbine Exhaust Support Systems

21

Gas Turbine Barrier Inlet Filter Systems

22

Gas Turbine Pulse Inlet Filter System

23

Inlet Guide Vanes

24

Inlet Guide Vanes

25

Gas Turbine Compressor Rotor Assembly

26

6B Gas Turbine

27

Gas Turbine Cut Away Side View

28

Gas Turbine Combustor Arrangement

29

Frame 5 GT

30

GE LM2500 Aeroderivative Gas Turbine

Compressor

Compressor Turbine Section

Power Turbine Section

31

FT4 Gas Turbine

32

FT4 Gas Turbine – Gas Generator (Compressor)

33

FT4 Gas Turbine – Gas Generator (Compressor)

34

FT4 Gas Turbine – Free Turbine

35

FT4 Gas Turbine – Free Turbine Gas Path

36

FT4 Gas Generator Performance

37

FT4 Free Turbine Performance

38

Aeroderivative Versus Heavy Duty Combustion Turbines

Aeroderivatives Higher Pressure Ratios and Firing Temperatures Result

in Higher Power Output per Pound of Air Flow Smaller Chilling/Cooling Systems Required Compressor Inlet Temperature Has a Greater Impact on

Output and Heat Rate Benefits of Chilling/Cooling Systems are More

Pronounced

39

Typical Simple Cycle CT Plant Components

Prime Mover (Combustion Turbine) Fuel Supply & Preparation Emissions Control Equipment Generator Electrical Switchgear Generator Step Up Transformer Starting System (Combustion Turbines) Auxiliary Cooling Fire Protection Lubrication System

40

Typical Peaking Plant Components

Lube Oil System GSU Generator

Fire ProtectionStarting EngineSwitchgear / MCC

41

Combining the Brayton and Rankine Cycles

Gas Turbine Exhaust used as the heat source for the Steam Turbine cycle

Utilizes the major efficiency loss from the Brayton cycle Advantages:

Relatively short cycle to design, construct & commission Higher overall efficiency Good cycling capabilities Fast starting and loading Lower installed costs No issues with ash disposal or coal storage

Disadvantages High fuel costs Uncertain long term fuel source Output dependent on ambient temperature

42

Picture courtesy of Nooter/EriksenPicture courtesy of Nooter/Eriksen

How does a Combined Cycle Plant Work?

43

Combined Cycle Heat Balance

44

Combined Cycles Today Plant Efficiency ~ 58-60 percent

Biggest losses are mechanical input to the compressor and heat in the exhaust

Steam Turbine output Typically 50% of the gas turbine output More with duct-firing

Net Plant Output (Using Frame size gas turbines) up to 750 MW for 3 on 1 configuration Up to 520 MW for 2 on 1 configuration

Construction time about 24 months Engineering time 80k to 130k labor hours Engineering duration about 12 months Capital Cost ($900-$1100/kW) Two (2) versus Three (3) Pressure Designs

Larger capacity units utilize the additional drums to gain efficiency at the expense of higher capital costs

45

Combined Cycle Efficiency

Simple cycle efficiency (max ~ 44%*) Combined cycle efficiency (max ~58-60%*) Correlating Efficiency to Heat Rate (British Units)

= 3412/(Heat Rate) --> 3412/ = Heat Rate* Simple cycle – 3412/.44 = 7,757 Btu/Kwh* Combined cycle – 3412/.58 = 5,884 Btu/Kwh*

Correlating Efficiency to Heat Rate (SI Units) = 3600/(Heat Rate) --> 3600/ = Heat Rate* Simple cycle – 3600/.44 = 8,182 KJ/Kwh* Combined cycle – 3600/.58 = 6,207 KJ/Kwh*

Practical Values HHV basis, net output basis Simple cycle 7FA (new and clean) 10,860 Btu/Kwh (11,457 KJ/Kwh) Combined cycle 2x1 7FA (new and clean) 6,218 Btu/Kwh (6,560 KJ/Kwh)

*Gross LHV basis

46

Gas Turbine Generator Performance

Factors that Influence Performance Fuel Type, Composition, and Heating Value Load (Base, Peak, or Part) Compressor Inlet Temperature Atmospheric Pressure Inlet Pressure Drop

Varies significantly with types of air cleaning/cooling

Exhaust Pressure Drop Affected by addition of HRSG, SCR, CO catalysts

Steam or Water Injection Rate Used for either power augmentation or NOx control

Relative Humidity

47

Altitude Correction

48

Humidity Correction

49

Cogeneration Plant

A Cogeneration Plant Power generation facility that also provides

thermal energy (steam) to a thermal host. Typical thermal hosts

paper mills, chemical plants, refineries, etc… potentially any user that uses large quantities of

steam on a continuous basis. Good applications for combined cycle plants

Require both steam and electrical power

50

Major Combined Cycle Plant Equipment

Combustion Turbine (CT/CTG) Steam Generator (Boiler/HRSG) Steam Turbine (ST/STG) Heat Rejection Equipment Air Quality Control System (AQCS) Equipment Electrical Equipment

51

Heat Recovery Steam Generator (HRSG)

52

Steam Turbine

GE D11

53

Same Function as discussed earlier in Session 9 Usually utilizes a

cooling tower to reject heat to the atmosphere

Rarely uses once through cooling (retrofit applications or ocean)

Heat Rejection Equipment - Condenser

54

Questions?

Rob Shepard

Neel-Schaffer, Inc.

www.Neel-Schaffer.com

[email protected]