About: Piaggio P.XII

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The Piaggio P.XII is an Italian 18-cylinder radial aircraft engine developed in the 1930s by Rinaldo Piaggio S.p.A. The P.XII was two Piaggio P.X engines in tandem, which were versions of the French Gnome-Rhône 9K Mistral made under license, themselves being much modified Gnome-Rhône 9A - a license-built Bristol Jupiter. The engine was used in some Italian aircraft from 1940 until the end of World War II, especially the Piaggio P.108. An up-rated version was tested as the Piaggio P.XXII.

Attributes	Values
rdf:type	software yago:AircraftEngine102687423 yago:Artifact100021939 yago:Device103183080 yago:Engine103287733 yago:HeatEngine103507963 yago:Instrumentality103575240 yago:Internal-combustionEngine103579982 yago:Machine103699975 yago:Motor103789946 yago:Object100002684 yago:PhysicalEntity100001930 yago:RadialEngine104040373 yago:Whole100003553 yago:WikicatAircraftAir-cooledRadialPistonEngines yago:WikicatPiaggioAircraftEngines yago:WikicatRadialEngines
rdfs:label	Piaggio P.XII (it) Piaggio P.XII (en)
rdfs:comment	The Piaggio P.XII is an Italian 18-cylinder radial aircraft engine developed in the 1930s by Rinaldo Piaggio S.p.A. The P.XII was two Piaggio P.X engines in tandem, which were versions of the French Gnome-Rhône 9K Mistral made under license, themselves being much modified Gnome-Rhône 9A - a license-built Bristol Jupiter. The engine was used in some Italian aircraft from 1940 until the end of World War II, especially the Piaggio P.108. An up-rated version was tested as the Piaggio P.XXII. (en) Il Piaggio P.XII RC.35 "Tornado" era un motore aeronautico radiale 18 cilindri a doppia stella raffreddato ad aria sviluppato dall'azienda italiana Rinaldo Piaggio S.p.A. negli anni trenta ed utilizzato in numerosi velivoli a cominciare dal 1940 fino alla fine della seconda guerra mondiale. (it)
foaf:depiction
dcterms:subject	Piaggio aircraft engines Aircraft air-cooled radial piston engines 1930s aircraft piston engines
Wikipage page ID	37724389 (xsd:integer)
Wikipage revision ID	1111476298 (xsd:integer)
Link from a Wikipage to another Wikipage	Province of Padua Savoia-Marchetti SM.84 Savoia-Marchetti SM.89 List of aircraft engines CANT Z.1015 Radial engine Gnome-Rhône 18L Gnome-Rhône 9K Piaggio aircraft engines CANT Z.1018 CANT Z.511 Tumansky M-90 Due Carrare Bristol Jupiter Centrifugal compressor Aircraft air-cooled radial piston engines 1930s aircraft piston engines Piaggio P.108 World War II Overhead valve Piaggio Aero 87 octane Rinaldo Piaggio S.p.A. dbr:Caproni_Ca.169 dbr:Museo_dell'Aria_e_dello_Spazio
sameAs	Piaggio P.XII Piaggio P.XII Piaggio P.XII Piaggio P.XII Piaggio P.XII Piaggio P.XII
specfuelcon	0.279500 (xsd:double)
specpower	22.290000 (xsd:double)
supercharger	Centrifugal compressor, geared to 7.81:1 (en)
valvetrain	2 (xsd:integer)
dbp:wikiPageUsesTemplate	dbt:Piaggio_aeroengines dbt:Commons_category dbt:Convert dbt:ISBN dbt:Reflist dbt:Aircontent dbt:Infobox_aircraft_engine dbt:Pistonspecs
thumbnail	wiki-commons:Special:FilePath/Piaggio_P.XII,_Museo_dell'aria_e_dello_spazio_(San_Pelagio,_Due_Carrare).jpg?width=300
national origin	Italy (en)
manufacturer	Piaggio Aero
power	Take-off: at 2,100rpm Military: at 2,100rpm at Cruising: at 1,700rpm at (en)
ref	Aircraft Engines of the World 1945. (en)
type	18 (xsd:integer) Radial engine
has abstract	The Piaggio P.XII is an Italian 18-cylinder radial aircraft engine developed in the 1930s by Rinaldo Piaggio S.p.A. The P.XII was two Piaggio P.X engines in tandem, which were versions of the French Gnome-Rhône 9K Mistral made under license, themselves being much modified Gnome-Rhône 9A - a license-built Bristol Jupiter. The engine was used in some Italian aircraft from 1940 until the end of World War II, especially the Piaggio P.108. An up-rated version was tested as the Piaggio P.XXII. (en) Il Piaggio P.XII RC.35 "Tornado" era un motore aeronautico radiale 18 cilindri a doppia stella raffreddato ad aria sviluppato dall'azienda italiana Rinaldo Piaggio S.p.A. negli anni trenta ed utilizzato in numerosi velivoli a cominciare dal 1940 fino alla fine della seconda guerra mondiale. (it)
components other	Starter: Garelli compressed air starter *Ignition: 2x Marelli AQ18 magnetos, 2 x spark plugs per cylinder fed by a shielded ignition harness. (en)
compression	6.500000 (xsd:double)
coolingsystem	Air (en)
fuelsystem	Single Piaggio downdraught carburettor with automatic boost and mixture control (en)
fueltype	87 (xsd:integer)
general other	Frontal Area: (en)
lists	*List of aircraft engines (en)
major applications	Piaggio P.108 CANT Z.1018 (en)
oilcon	0.013400 (xsd:double)
oilsystem	Pressure fed at , dry sump (en)
power/weight	1.324000 (xsd:double)
reduction gear	Epicyclic reduction gear, gear ratio: 0.62:1 (en)
see also	Gnome-Rhône 18L Tumansky M-90 (en)
gold:hypernym	Engine
prov:wasDerivedFrom	wikipedia-en:Piaggio_P.XII?oldid=1111476298&ns=0
page length (characters) of wiki page	5352 (xsd:nonNegativeInteger)
foaf:isPrimaryTopicOf	wikipedia-en:Piaggio_P.XII
is Link from a Wikipage to another Wikipage of	Savoia-Marchetti SM.84 Savoia-Marchetti SM.89 List of aircraft engines

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