The Hitachi Ha-51 (unified designation), was a Japanese air-cooled twenty-two-cylinder twin-row radial aircraft engine designed by Hitachi during the final years of World War II. The first prototype ran in 1944 at a rating of 1,772 kW (2,000 hp), but only four examples were built. In August 1945, development was halted. The engine had yet to find an application and bombing had destroyed the factory where production was to take place.
Attributes | Values |
---|
rdfs:label
| - Hitachi Ha-51 (en)
- ハ51 (エンジン) (ja)
|
rdfs:comment
| - The Hitachi Ha-51 (unified designation), was a Japanese air-cooled twenty-two-cylinder twin-row radial aircraft engine designed by Hitachi during the final years of World War II. The first prototype ran in 1944 at a rating of 1,772 kW (2,000 hp), but only four examples were built. In August 1945, development was halted. The engine had yet to find an application and bombing had destroyed the factory where production was to take place. (en)
- ハ51は、第二次世界大戦後期に日立航空機が開発試作した航空機用空冷星型エンジンである。 大馬力を達成するために空冷星型複列22気筒という珍しい形式を採用しており、計画出力は2,500~3,000馬力であった。試作機による試運転が行われたが問題が多発し、1945年(昭和20年)4月の空襲により開発が中止された。 製作数は4基。 (ja)
|
dcterms:subject
| |
Wikipage page ID
| |
Wikipage revision ID
| |
Link from a Wikipage to another Wikipage
| |
Link from a Wikipage to an external page
| |
sameAs
| |
similar engines
| - * Wright R-4090 Cyclone 22
* BMW 802 (en)
|
supercharger
| |
dbp:wikiPageUsesTemplate
| |
national origin
| |
manufacturer
| |
power
| - ** Max power: at 3000 rpm at sea level
** Rated:
**: at 3000 rpm at
**: at 3000 rpm at (en)
|
ref
| |
type
| |
has abstract
| - The Hitachi Ha-51 (unified designation), was a Japanese air-cooled twenty-two-cylinder twin-row radial aircraft engine designed by Hitachi during the final years of World War II. The first prototype ran in 1944 at a rating of 1,772 kW (2,000 hp), but only four examples were built. In August 1945, development was halted. The engine had yet to find an application and bombing had destroyed the factory where production was to take place. (en)
- ハ51は、第二次世界大戦後期に日立航空機が開発試作した航空機用空冷星型エンジンである。 大馬力を達成するために空冷星型複列22気筒という珍しい形式を採用しており、計画出力は2,500~3,000馬力であった。試作機による試運転が行われたが問題が多発し、1945年(昭和20年)4月の空襲により開発が中止された。 製作数は4基。 (ja)
|
first run
| |
lists
| - * List of aircraft engines (en)
|
number built
| |
reduction gear
| |
prov:wasDerivedFrom
| |
page length (characters) of wiki page
| |
foaf:isPrimaryTopicOf
| |
is Link from a Wikipage to another Wikipage
of | |
is Wikipage redirect
of | |
is foaf:primaryTopic
of | |