LMA 1500
Product Overview
GAS
TURBINE
Model: LMA
1500.
Cycle: Simple.
Fuel: Natural
Gas (distillate or #2 diesel options).
Starting System: Hydraulic
start system.
Shaft power: 15,400
hp.
Rotating Parts: Dry
flexible load coupling.
GENERATOR
Type: Ideal
Electric "SAB" horizontal, brushless, and air cooled.
Cooling System: Air cooled, open ventilated. Fin
fan, air-to-air cooling.
Rate: 12,500
KVA, 60 hz, 1800 rpm, 13800 volts.
Excitation: Field
suitable, brushless exciter-regulator.
Lubrication: Lube
oil system is integrated with the package.
PERFORMANCE (ISO Conditions)
Power Turbine Speed: 5500 rpm
Exhaust flow: 162
lbs/s
Power turbine temp: 800°
Fahrenheit (101 MMBTU/HR. Exhaust @ 600° Fahrenheit drop)
Generator output: 10,000
KW - (11,500 PEAK)
Generator Efficiency: 0.973
GAS TURBINE SPECS
Table Of Contents
1.00 Equipment List
1.01 Standard Equipment
1.02 Optional Equipment
1.10 Installation Requirements
1.20 Purchaser's Responsibilities
1.30 Acceptance Test
1.40 Performance Rating
Specifications
~~~~~~~~~~~~~~~~~~~~
1.00 EQUIPMENT
LIST
1.01 Standard
Equipment
- •Bell mouth.
- •Bullet nose.
- •Gas generator
with fuel nozzles and manifold(s) for natural gas, liquid fuel, or dual fuel
(as stipulated for each engine model).
- •Gas detection
System.
- •Power turbine.
- •Lubrication
system components.
- •Engine driven
lube and scavenge pump.
- •Lube supply
manifold.
- •Instrumentation:
- (2) gas generator
speed sensors; magnetic pickup type.
- (2) power
turbine speed sensors; magnetic pickup type.
- (11) power
turbine inlet temperature probes; chromel/alumel type.
- (1) gas generator
vibration sensor; accelerometer type.
- (1) power
turbine vibration sensor; accelerometer type.
- (1) oil supply
temperature sensor; RTD single element type.
- (5) oil scavenger
temperature sensors; RTD single element type.
- (1) lube oil
supply pressure tap.
- (1) scavenger
oil pressure tap.
- (2) pressure
tap for compressor discharge pressure.
- (1) pressure
tap for fuel manifold pressure.
- (1) power
turbine inlet pressure tap.
- •Single ignition
system: igniter, high tension cable and exciter.
1.0.2 Optional
Equipment
- •Fuel pump
with filter (engine mounted) for liquid fueled gas turbine only.
- •Fuel pump
with filter (off engine mounted) for dual fuel application.
- •Air or natural
gas start system.
- •Inlet seal
kit.
- •Compressor
inlet pressure (Pt2) probe.
- •Dual redundant
lube temperature sensor kit.
- •Additional
accelerometers kit.
- •Electronic
chip detector kit.
- •Inlet cooling
system.
- •SCR system.
- •Fuel/gas
compressor.
- •Oil debris
monitoring system.
- •Individual
EGT thermocouple readout system.
- •Remote control
and monitoring system.
- •Ultraviolet
flame detector kit.
- •Dual ignition
System Kit.
- •Spare parts
package.
- •Compressor
water wash system.
- •Air filtration
system.
- •Intake Extinguishing
System
- •Skid and
control enclosures
- •Shipping
Container.
1.10 INSTALLATION
REQUIREMENTS
Reliable operation
and low maintenance costs for the gas turbine require that the purchaser installation
designs and operating/maintenance practices be in accordance with the instructions
defined in the then-current Installation Design Manual and the Operation
and Maintenance Manual.
1.20 PURCHASER'S
RESPONSIBILITIES
It is to be recognized
that the purchaser has system responsibility for technical integration of the
LMA 1500 gas turbine into a complete gas turbine system, satisfying the installation/interface
requirements and recommended operation/maintenance practices defined in the
then-current Installation Design Manual and Operation and Maintenance
Manual. The purchaser's attention is specifically referred to, but not
limited to, such system interfacing consideration s as vibration, controls,
fuel quality, inlet air quality, inlet system design and construction, and gas
turbine cooling.
1.30 ACCEPTANCE
TEST
Each gas turbine
is tested at LM Alternatives test facility to verify proper mechanical operation
and compliance with guarantee performance levels. Testing is in accordance with
LM Alternatives established practice for industrial gas turbines. Measurements
at five test data points, spanning the entire power range, are taken to establish
shaft horsepower and heat rate. Test data is corrected to the guarantee conditions.
Upon completion of the test, a formal Test Acceptance Report, including copies
of all original test log and data sheets, is issued by Engineering.
1.40 PERFORMANCE
RATING
Industrial
Gas Generator Performance Characteristics
(59 ° Fahrenheit,
sea level, no losses, fuel LHV 18,400 btu/lb)
Power turbine
rate: 5,500
rpm.
Fuel: Natural
Gas (#2 Diesel Option)
Insentropic gas horsepower: 17,300 hp.
Exhaust gas temperature: 975°
Fahrenheit (800° Fahrenheit @ power turbine)
Exhaust gas pressure: 36
psi
Heat rate: 7800
btu/ghp-hr
Airflow: 158
lb/sec.
SFC (nominal): 0.51
lb/hp-hr
Nitrous Oxide emission: 75
ppm
Carbon Monoxide emission: 75 ppm
Emission levels for
power levels between 75% and 100% of base load.
Sample Diagram
Updated January 2000.
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