Pratt & Whitney Canada PT6 C-67 E
GPTKB entity
Statements (97)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:turbofan_engine
|
| gptkbp:application |
gptkb:Eurocopter_EC175
gptkb:Bell_429 gptkb:Agusta_Westland_AW139 gptkb:Sikorsky_S-76_C+ helicopters |
| gptkbp:average_temperature |
high operating temperature
|
| gptkbp:certification |
FAA certified
EASA certified |
| gptkbp:combustor_type |
annular
reverse flow combustion |
| gptkbp:compression_ratio |
16:1
|
| gptkbp:compressor_type |
axial compressor
|
| gptkbp:configuration |
twin-shaft
|
| gptkbp:control_system |
gptkb:electronic
gptkb:full_authority_digital_engine_control_(FADEC) digital control system |
| gptkbp:cooling_system |
air-cooled
|
| gptkbp:design |
modular design
|
| gptkbp:diameter |
approximately 16 in
approximately 18 in |
| gptkbp:elevation |
up to 20,000 ft
|
| gptkbp:emissions_standard |
low emissions
compliant with ICAO standards |
| gptkbp:engine |
gptkb:PT6_family
gptkb:military_aircraft gptkb:Pratt_&_Whitney_Canada passenger transport cargo transport commercial aviation private aviation air start utility helicopters commercial and military applications starter-generator system 1,100 shaft horsepower PT6 C series |
| gptkbp:engine_configuration |
gptkb:turbofan_engine
1,800 shp twin-engine configuration dual-engine configuration advanced design features twin-shaft turboprop turboprop engine design |
| gptkbp:engine_family_name |
gptkb:PT6_family
|
| gptkbp:engine_maintenance_requirement |
low maintenance
|
| gptkbp:engine_power |
high performance
high reliability excellent performance up to 5,000 hours proven reliability |
| gptkbp:engine_thrust_output |
1,800 shp at sea level
|
| gptkbp:engine_type |
gptkb:turbofan_engine
turboprop high-performance engine PT6 C-67 E |
| gptkbp:first_flight |
gptkb:2005
gptkb:2007 |
| gptkbp:fuel_capacity |
46 cm
lightweight engine 181 kg 137 cm |
| gptkbp:fuel_economy |
high fuel efficiency
0.5 lb/hp/hr 1,800 shp at takeoff approximately 0.5 kg/k W/h |
| gptkbp:fuel_type |
gptkb:Jet_A-1
gptkb:Jet_A hydromechanical |
| gptkbp:gearbox |
reduction gearbox
|
| https://www.w3.org/2000/01/rdf-schema#label |
Pratt & Whitney Canada PT6 C-67 E
|
| gptkbp:legal_principle |
gas turbine cycle
|
| gptkbp:length |
approximately 54 in
|
| gptkbp:maintenance |
scheduled maintenance
3,600 hours |
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney_Canada
|
| gptkbp:market_segment |
commercial aviation
|
| gptkbp:notable_feature |
gptkb:dual-channel_FADEC
|
| gptkbp:notable_features |
high power-to-weight ratio
|
| gptkbp:operational_range |
up to 20,000 feet
|
| gptkbp:power_output |
1,800 shp
1,100 shp |
| gptkbp:propulsion |
4.5:1
1,800 shp 1,100 lbf |
| gptkbp:reliability |
high
high reliability |
| gptkbp:service_entry |
gptkb:2005
|
| gptkbp:turbine_type |
single-stage turbine
single-stage power turbine |
| gptkbp:type |
turbo-prop engine
|
| gptkbp:weight |
lightweight design
approximately 400 lb approximately 300 lb |
| gptkbp:bfsParent |
gptkb:Leonardo_AW169
gptkb:AW169_M |
| gptkbp:bfsLayer |
6
|