Statements (52)
Predicate | Object |
---|---|
gptkbp:instanceOf |
aircraft engine
|
gptkbp:application |
military aircraft
passenger aircraft cargo_aircraft |
gptkbp:bore |
5.5 in
|
gptkbp:compressionRatio |
7.0:1
|
gptkbp:controls |
mechanical control
|
gptkbp:coolingSystem |
air-cooled
direct air cooling |
gptkbp:cylinderCount |
18
|
gptkbp:displacement |
43.6 L
|
gptkbp:drivetrain |
2 per cylinder
|
gptkbp:engine |
horizontally opposed
cradle_mount |
gptkbp:engineConfiguration |
multi-row
|
gptkbp:engineType |
four-stroke engine
R-4360-1 R-4360-10 R-4360-2 R-4360-3 R-4360-4 R-4360-5 R-4360-6 R-4360-7 R-4360-8 R-4360-9 |
gptkbp:firstRace |
1944
|
gptkbp:fuelType |
aviation gasoline
carbureted dual ignition |
gptkbp:hasArea |
extensive testing required
FAA_certified |
https://www.w3.org/2000/01/rdf-schema#label |
Wright R-4360 Wasp Major
|
gptkbp:is_used_in |
gptkb:Boeing_B-17_Flying_Fortress
gptkb:Douglas_C-124_Globemaster_II Convair B-36 Peacemaker |
gptkbp:manufacturer |
gptkb:Wright_Aeronautical_Corporation
|
gptkbp:notable_feature |
durability
reliability smooth operation high power-to-weight ratio |
gptkbp:performances |
periodic maintenance required
major overhaul every 1,500 hours |
gptkbp:powerOutput |
3,000 hp
|
gptkbp:productionYears |
1944-1955
|
gptkbp:propulsion |
variable-pitch propeller
|
gptkbp:related_engine |
gptkb:Otto_cycle
|
gptkbp:setting |
supercharged
|
gptkbp:stroke |
6.0 in
|
gptkbp:successor |
gptkb:Wright_R-3350
|
gptkbp:type |
radial engine
|
gptkbp:weight |
1,800 lb
|