Statements (80)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:jet_engine
|
| gptkbp:application |
gptkb:military_aircraft
civil aircraft |
| gptkbp:compression_ratio |
6:1
|
| gptkbp:configuration |
9-cylinder
|
| gptkbp:cooling_system |
air-cooled
air-cooled engine |
| gptkbp:design |
aircraft engine design
|
| gptkbp:displacement |
1340 cubic inches
|
| gptkbp:engine |
gptkb:series
over 10,000 units R-1340 family |
| gptkbp:engine_configuration |
horizontally opposed
radial layout |
| gptkbp:engine_type |
piston engine
R-1340-4 R-1340-AN R-1340-100 R-1340-18 R-1340-23 R-1340-25 R-1340-28 R-1340-30 R-1340-32 R-1340-34 R-1340-36 R-1340-38 R-1340-40 R-1340-42 R-1340-44 R-1340-46 R-1340-48 R-1340-50 R-1340-52 R-1340-54 R-1340-56 R-1340-58 R-1340-60 R-1340-62 R-1340-64 R-1340-66 R-1340-68 R-1340-7 R-1340-70 R-1340-72 R-1340-74 R-1340-76 R-1340-78 R-1340-80 R-1340-82 R-1340-84 R-1340-86 R-1340-88 R-1340-90 R-1340-92 R-1340-94 R-1340-96 R-1340-98 R-1340-99 R-1340-AX |
| gptkbp:first_flight |
gptkb:1932
|
| gptkbp:fuel_type |
aviation gasoline
carbureted |
| https://www.w3.org/2000/01/rdf-schema#label |
Pratt & Whitney R-1340
|
| gptkbp:ignition_system |
magneto ignition
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney
|
| gptkbp:notable_users |
gptkb:Royal_Canadian_Air_Force
gptkb:United_States_Air_Force gptkb:United_States_Navy |
| gptkbp:power_output |
600 horsepower
|
| gptkbp:production_years |
1932-1945
|
| gptkbp:successor |
gptkb:Pratt_&_Whitney_R-985
|
| gptkbp:type |
gptkb:radial_engine
|
| gptkbp:used_in |
gptkb:Douglas_DC-3
gptkb:Boeing_Stearman_PT-17 |
| gptkbp:valve_configuration |
overhead valves
|
| gptkbp:weight |
about 600 pounds
|
| gptkbp:bfsParent |
gptkb:Boeing_247_D
gptkb:Model_14_A_Super_Electra |
| gptkbp:bfsLayer |
6
|