Statements (59)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:application |
helicopters
|
| gptkbp:average_temperature |
up to 1,500 ° F
|
| gptkbp:certification |
FAA certified
|
| gptkbp:controls |
digital control system
|
| gptkbp:cooling_system |
air-cooled
|
| gptkbp:developer |
developed for military use
|
| gptkbp:diameter |
approximately 2.5 ft
|
| gptkbp:emissions_standard |
meets current standards
|
| gptkbp:engine_type |
axial compressor
single-stage turbine |
| gptkbp:features |
modular design
|
| gptkbp:first_introduced |
1960s
|
| gptkbp:fuel_capacity |
high fuel efficiency
|
| gptkbp:fuel_type |
gptkb:Jet_A
annular combustor |
| gptkbp:game_components |
gptkb:Company
gptkb:earthquake gptkb:park temperature sensors pressure sensors engine control unit air intake heat exchanger high-pressure turbine oil cooler exhaust nozzle accessory gearbox thrust reverser low-pressure turbine fuel filter starter motor engine diagnostics system control valves engine monitoring system vibration monitoring system high-pressure compressor fuel nozzle fuel control system air separator engine mount engine performance software thrust measurement system |
| https://www.w3.org/2000/01/rdf-schema#label |
Honeywell T55
|
| gptkbp:length |
approximately 5.5 ft
|
| gptkbp:maintenance |
2,500 hours
|
| gptkbp:manufacturer |
gptkb:Honeywell
|
| gptkbp:market |
aerospace market
|
| gptkbp:noise_level |
low noise output
|
| gptkbp:propulsion |
up to 5,000 lbf
|
| gptkbp:reliability |
high reliability
|
| gptkbp:services |
over 10,000 hours
|
| gptkbp:successor |
gptkb:Honeywell_T53
|
| gptkbp:technology |
advanced materials
|
| gptkbp:type |
gptkb:engine
|
| gptkbp:used_in |
gptkb:aircraft
|
| gptkbp:weight |
approximately 1,200 lb
|
| gptkbp:bfsParent |
gptkb:CH-47_Chinook
|
| gptkbp:bfsLayer |
4
|