|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:aircraft_operated
|
gptkb:Eurocopter_EC175
gptkb:Bell_429
gptkb:Agusta_Westland_AW139
gptkb:Sikorsky_S-76_C
gptkb:Sikorsky_S-76_C+
|
|
gptkbp:application
|
helicopters
|
|
gptkbp:average_temperature
|
up to 1,000 ° F
|
|
gptkbp:certification
|
FAA certified
|
|
gptkbp:combustor_type
|
annular combustor
|
|
gptkbp:compression_ratio
|
16:1
|
|
gptkbp:compressor_type
|
axial compressor
|
|
gptkbp:configuration
|
twin-shaft
|
|
gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
digital engine control
|
|
gptkbp:cooling_system
|
air-cooled
oil cooling
|
|
gptkbp:diameter
|
approximately 16 in
approximately 18 in
|
|
gptkbp:emissions_standard
|
ICAO Chapter 4
|
|
gptkbp:engine
|
gptkb:PT6_family
air start
|
|
gptkbp:engine_configuration
|
twin-spool
|
|
gptkbp:engine_power
|
up to 5,000 hours
|
|
gptkbp:engine_type
|
gptkb:turbofan_engine
turboprop
PT6 C-67 E
PT6 C-67 D
PT6 C-67 F
PT6 C-67 G
PT6 C-67 H
|
|
gptkbp:first_flight
|
gptkb:2007
|
|
gptkbp:fuel_economy
|
0.5 lb/hp/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
electronic fuel control
dual fuel system
|
|
gptkbp:gearbox
|
reduction gearbox
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Pratt & Whitney Canada PT6 C-67 C
|
|
gptkbp:ignition_system
|
dual ignition system
|
|
gptkbp:is_tested_for
|
engine health monitoring system
|
|
gptkbp:length
|
approximately 54 in
|
|
gptkbp:maintenance
|
3,600 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney_Canada
|
|
gptkbp:number_of_stages
|
6 stages
|
|
gptkbp:operational_use
|
gptkb:civil_aviation
gptkb:military_aircraft
|
|
gptkbp:power_output
|
1,800 shp
1,100 shp
|
|
gptkbp:propulsion
|
1,100 lbf
3.67 hp/lb
|
|
gptkbp:service_ceiling
|
20,000 ft
|
|
gptkbp:turbine_type
|
free turbine
|
|
gptkbp:weight
|
approximately 400 lb
approximately 300 lb
|
|
gptkbp:bfsParent
|
gptkb:Agusta_Westland_AW139
|
|
gptkbp:bfsLayer
|
5
|