Honeywell AGT1500 turbine engine
GPTKB entity
Properties (63)
Predicate | Object |
---|---|
gptkbp:instanceOf |
turbine engine
|
gptkbp:application |
military vehicles
|
gptkbp:certifications |
FAA_certified
|
gptkbp:climate |
up to 1,600°F
|
gptkbp:component |
combustor
control unit temperature sensor speed sensor ignition system fuel pump gearbox air intake system pressure sensor oil cooler thrust reverser fuel filter oil filter starter motor vibration damper compressor rotor exhaust_nozzle turbine_rotor |
gptkbp:compressionRatio |
15:1
|
gptkbp:controls |
digital display
digital electronic control starter-generator |
gptkbp:coolingSystem |
air-cooled
synthetic oil |
gptkbp:design_feature |
modular design
|
gptkbp:diameter |
approximately 20 inches
|
gptkbp:drivetrain |
reduction gearbox
|
gptkbp:emissionsStandard |
gptkb:EPA_Tier_4
|
gptkbp:engine |
low vibration
|
gptkbp:engineType |
two stages
five stages |
gptkbp:exhaustSystem |
axial exhaust
|
gptkbp:facilities |
gptkb:Honeywell_Aerospace
|
gptkbp:fanEvents |
nickel-based superalloy
|
gptkbp:fuel_capacity |
0.5 miles per gallon
0.4 lb/hp/hr |
gptkbp:fuelType |
JP-8
annular combustor hydromechanical fuel control |
https://www.w3.org/2000/01/rdf-schema#label |
Honeywell AGT1500 turbine engine
|
gptkbp:installation |
vertical installation
|
gptkbp:introduced |
1980
|
gptkbp:is_used_in |
gptkb:M1_Abrams_tank
|
gptkbp:legal_principle |
Brayton_cycle
|
gptkbp:length |
approximately 60 inches
|
gptkbp:maintenance |
500 hours
|
gptkbp:manufacturer |
gptkb:Honeywell_International_Inc.
|
gptkbp:market_segment |
military aviation
|
gptkbp:noise_level |
85 dB
|
gptkbp:operationalRange |
up to 10,000 feet
|
gptkbp:powerOutput |
1500 horsepower
|
gptkbp:propulsion |
3,000 pounds
0.8 lb/hp |
gptkbp:safety_features |
redundant systems
|
gptkbp:services |
over 5,000 hours
|
gptkbp:setting |
turbo-shaft
|
gptkbp:training |
gptkb:Advanced_Gas_Turbine_Program
|
gptkbp:type |
gas turbine engine
|
gptkbp:weight |
approximately 1,200 pounds
|