Statements (50)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
aircraft engine
|
| gptkbp:aircraft |
biplanes
|
| gptkbp:application |
military aircraft
|
| gptkbp:bore |
4.0 in
|
| gptkbp:compressionRatio |
5.0:1
|
| gptkbp:coolingSystem |
liquid cooling
water-cooled |
| gptkbp:cylinderCount |
8
|
| gptkbp:displacement |
5.0 L
|
| gptkbp:drivetrain |
overhead valve
|
| gptkbp:engine |
distinctive sound
civilian aircraft V engine layout influenced future aircraft engines contributed to aviation history. inline V engine design technological advancements in aviation engines |
| gptkbp:engineConfiguration |
over 10,000 units produced
V8_configuration |
| gptkbp:engineType |
lightweight construction
simple design reciprocating engine various variants developed |
| gptkbp:firstFlight |
1916
|
| gptkbp:fuelType |
aviation gasoline
carbureted magneto ignition |
| https://www.w3.org/2000/01/rdf-schema#label |
Curtiss OX-5 V-8
|
| gptkbp:is_used_in |
gptkb:Curtiss_JN-4_Jenny
|
| gptkbp:manufacturer |
gptkb:Curtiss_Aeroplane_and_Motor_Company
|
| gptkbp:maximum_speed |
maximum RPM of 2,000
|
| gptkbp:notableUsers |
gptkb:U.S._Army_Air_Service
|
| gptkbp:operationalHistory |
historically significant engine
|
| gptkbp:performances |
smooth operation
high reliability reliable performance easy maintenance good fuel efficiency specific performance specifications |
| gptkbp:powerOutput |
100 hp
|
| gptkbp:productionYears |
1916-1925
|
| gptkbp:propulsion |
fixed-pitch propeller
|
| gptkbp:purpose |
aviation
|
| gptkbp:related_engine |
Curtiss_OX_series
|
| gptkbp:setting |
V engine
|
| gptkbp:stroke |
5.0 in
|
| gptkbp:successor |
Curtiss_OX-6
|
| gptkbp:torque |
high torque output
|
| gptkbp:type |
gptkb:V8_engine
|
| gptkbp:weight |
200 lb
|