Statements (50)
Predicate | Object |
---|---|
gptkbp:instanceOf |
engine
|
gptkbp:bore |
5.5 inches
|
gptkbp:compressionRatio |
7.0:1
|
gptkbp:controls |
Throttle_control
|
gptkbp:coolingSystem |
Air-cooled
|
gptkbp:cylinderCount |
18
Double Wasp |
gptkbp:displacement |
3,350 cubic inches
|
gptkbp:engine |
Passenger transport
Cargo transport Commercial aviation Military aviation Transport aircraft Heavy bombers Electric starter Long-range missions Single-speed supercharger Cooled by air Nose-mounted |
gptkbp:engineConfiguration |
Wet sump
Horizontally_opposed |
gptkbp:engineType |
Regular maintenance required
High performance at altitude |
gptkbp:firstFlight |
1941
|
gptkbp:fuelType |
Avgas
Dual ignition |
https://www.w3.org/2000/01/rdf-schema#label |
R-3350-63
|
gptkbp:manufacturer |
gptkb:Wright_Aeronautical_Corporation
|
gptkbp:notableFeature |
gptkb:R-3350-26
R-3350-32 R-3350-54 R-3350-23 R-3350-97 |
gptkbp:operationalHistory |
Used in military and civilian aircraft
|
gptkbp:powerOutput |
2,200 to 3,000 horsepower
|
gptkbp:propulsion |
Variable-pitch propeller
|
gptkbp:relatedPatent |
R-3350-54
R-2800 R-1830 R-4360-17 R-4360-23 |
gptkbp:retirementYear |
1960s
|
gptkbp:setting |
Air-cooled
|
gptkbp:stroke |
6.5 inches
|
gptkbp:successor |
R-4360
|
gptkbp:type |
gptkb:Radial_Engine
|
gptkbp:usedIn |
gptkb:Boeing_B-17_Flying_Fortress
gptkb:Lockheed_Constellation gptkb:Douglas_DC-7 |
gptkbp:weight |
1,800 pounds
|