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gptkbp:instance_of
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gptkb:turbofan_engine
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gptkbp:application
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gptkb:military_aircraft
|
|
gptkbp:average_temperature
|
1,500 ° F
|
|
gptkbp:certification
|
FAA certified
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|
gptkbp:combustor_type
|
annular
|
|
gptkbp:compressor_type
|
gptkb:14
|
|
gptkbp:control_system
|
hydromechanical
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|
gptkbp:cooling_system
|
air-cooled
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|
gptkbp:design
|
axial-flow
|
|
gptkbp:development
|
1950s to 1960s
|
|
gptkbp:emissions_standard
|
Stage 3
|
|
gptkbp:engine
|
helicopters
modular
Brayton cycle
over 10,000 units
T64-GE-416
developed for military use.
dual-spool design
major overhaul every 5,000 hours
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|
gptkbp:engine_configuration
|
twin-spool
military specifications
detailed in military documents
|
|
gptkbp:engine_power
|
high efficiency
proven track record
|
|
gptkbp:engine_type
|
T64-GE-412
|
|
gptkbp:first_flight
|
gptkb:1955
|
|
gptkbp:fuel_capacity
|
4.5 ft
2.5 ft
|
|
gptkbp:fuel_economy
|
0.5 lb/hp/hr
|
|
gptkbp:fuel_type
|
kerosene
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
General Electric T64
|
|
gptkbp:is_tested_for
|
static test stand
General Electric test facility
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:noise_level
|
85 d B
|
|
gptkbp:notable_users
|
gptkb:Sikorsky_CH-53_Sea_Stallion
|
|
gptkbp:operational_use
|
1960s
|
|
gptkbp:power_output
|
1,500 shp
|
|
gptkbp:propulsion
|
2.5
3,000 lbf
|
|
gptkbp:reliability
|
high
|
|
gptkbp:service_ceiling
|
20,000 ft
|
|
gptkbp:successor
|
gptkb:General_Electric_T700
|
|
gptkbp:turbine_type
|
2
|
|
gptkbp:type
|
gptkb:turbofan_engine
|
|
gptkbp:used_in
|
gptkb:Lockheed_C-130_Hercules
|
|
gptkbp:variant
|
T64-GE-413
|
|
gptkbp:weight
|
1,200 lb
|
|
gptkbp:bfsParent
|
gptkb:CH-53_E_Super_Stallion
gptkb:MH-53_E_Sea_Dragon
|
|
gptkbp:bfsLayer
|
5
|