Chrysler IV-2220 (original) (raw)
The Chrysler XIV-2220 (XI-2220 from 1944) was an experimental 2,500 hp, 2,220 cubic inch (36.4 liter) liquid-cooled inverted-V-16 aircraft engine designed by Chrysler starting in 1940. Although several aircraft designs had considered using it, by the time it was ready for use in 1945 the war was already over. Only a few engines were built during the program, and it retained its 'X' designation the entire time as the XIV-2220, later XI-2220. The IV-2220 is historically important as it was Chrysler's first hemi, a design that would re-appear for many years later and is now a Chrysler trademark.
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| Property | Value |
|---|---|
| dbo:abstract | The Chrysler XIV-2220 (XI-2220 from 1944) was an experimental 2,500 hp, 2,220 cubic inch (36.4 liter) liquid-cooled inverted-V-16 aircraft engine designed by Chrysler starting in 1940. Although several aircraft designs had considered using it, by the time it was ready for use in 1945 the war was already over. Only a few engines were built during the program, and it retained its 'X' designation the entire time as the XIV-2220, later XI-2220. The IV-2220 is historically important as it was Chrysler's first hemi, a design that would re-appear for many years later and is now a Chrysler trademark. (en) クライスラー・IV-2220はアメリカ合衆国の自動車メーカーであるクライスラーが1940年に試作した水冷倒立V型16気筒の航空機用エンジンである。同社にとって最初のヘミエンジンであり、以後ヘミエンジンはクライスラーのトレードマークとなった。 (ja) |
| dbo:thumbnail | wiki-commons:Special:FilePath/Chrysler_IV-2220_(1).png?width=300 |
| dbo:wikiPageExternalLink | http://www.enginehistory.org/ http://1000aircraftphotos.com/Contributions/PippinBill/5109.htm |
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| dbp:compression | 6.300000 (xsd:double) |
| dbp:coolingsystem | Liquid-cooled (en) |
| dbp:firstRun | 1945 (xsd:integer) |
| dbp:fuelcon | 0.420000 (xsd:double) |
| dbp:fuelsystem | 1 (xsd:integer) |
| dbp:fueltype | 100 (xsd:integer) |
| dbp:majorApplications | dbr:Curtiss_P-60 |
| dbp:manufacturer | dbr:Chrysler |
| dbp:oilcon | 0.005000 (xsd:double) |
| dbp:oilsystem | Pressure fed at , dry sump, 120 S.U. grade oil. (en) |
| dbp:power | * at 3,400 rpm for takeoff * at METO * at 3,200 rpm normal rating * at 2,800 rpm cruise (en) |
| dbp:power/weight | 1.020000 (xsd:double) |
| dbp:ref | Aircraft Engines of the World 1946 (en) |
| dbp:specfuelcon | *0.54 lb/ ) METO *0.43 lb/ ) normal rating (en) |
| dbp:specpower | 1.130000 (xsd:double) |
| dbp:supercharger | With aftercooler (en) |
| dbp:turbocharger | With water-to-air intercooler (en) |
| dbp:type | 16 (xsd:integer) dbr:Aircraft_engine |
| dbp:valvetrain | Single overhead camshaft actuating two valves per cylinder (en) |
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| rdfs:comment | The Chrysler XIV-2220 (XI-2220 from 1944) was an experimental 2,500 hp, 2,220 cubic inch (36.4 liter) liquid-cooled inverted-V-16 aircraft engine designed by Chrysler starting in 1940. Although several aircraft designs had considered using it, by the time it was ready for use in 1945 the war was already over. Only a few engines were built during the program, and it retained its 'X' designation the entire time as the XIV-2220, later XI-2220. The IV-2220 is historically important as it was Chrysler's first hemi, a design that would re-appear for many years later and is now a Chrysler trademark. (en) クライスラー・IV-2220はアメリカ合衆国の自動車メーカーであるクライスラーが1940年に試作した水冷倒立V型16気筒の航空機用エンジンである。同社にとって最初のヘミエンジンであり、以後ヘミエンジンはクライスラーのトレードマークとなった。 (ja) |
| rdfs:label | Chrysler IV-2220 (en) クライスラー・IV-2220 (ja) |
| owl:sameAs | freebase:Chrysler IV-2220 yago-res:Chrysler IV-2220 wikidata:Chrysler IV-2220 dbpedia-ja:Chrysler IV-2220 https://global.dbpedia.org/id/4hhRW |
| prov:wasDerivedFrom | wikipedia-en:Chrysler_IV-2220?oldid=1098537674&ns=0 |
| foaf:depiction | wiki-commons:Special:FilePath/Chrysler_IV-2220_(1).png |
| foaf:isPrimaryTopicOf | wikipedia-en:Chrysler_IV-2220 |
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| is foaf:primaryTopic of | wikipedia-en:Chrysler_IV-2220 |
