Gnome Monosoupape 9-cylinder rotary engine
GPTKB entity
Statements (28)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:bore |
110 mm
|
| gptkbp:category |
gptkb:piston_engine
gptkb:aircraft_piston_engine |
| gptkbp:configuration |
rotary
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:countryOfOrigin |
gptkb:France
|
| gptkbp:displacement |
16.3 L
|
| gptkbp:firstFlight |
1913
|
| gptkbp:fuelType |
gptkb:gasoline
|
| gptkbp:manufacturer |
gptkb:Gnome_et_Rhône
|
| gptkbp:notableFeature |
no conventional intake valves
rotating crankcase single valve per cylinder |
| gptkbp:numberOfEngines |
9
|
| gptkbp:powerOutput |
100 hp
|
| gptkbp:stroke |
150 mm
|
| gptkbp:successor |
gptkb:Gnome_Monosoupape_11-cylinder_rotary_engine
|
| gptkbp:usedDuring |
gptkb:World_War_I
|
| gptkbp:usedIn |
gptkb:Nieuport_11
gptkb:Avro_504 gptkb:Sopwith_Camel gptkb:Morane-Saulnier_Type_N |
| gptkbp:valveConfiguration |
monosoupape (single valve)
|
| gptkbp:weight |
150 lb
|
| gptkbp:bfsParent |
gptkb:Airco_DH.2
|
| gptkbp:bfsLayer |
6
|
| https://www.w3.org/2000/01/rdf-schema#label |
Gnome Monosoupape 9-cylinder rotary engine
|