Hitachi Ha-51
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The Hitachi Ha-51 (unified designation), was a Japanese air-cooled twenty-two-cylinder twin-row radial aircraft engine designed by
Hitachi () is a Japanese Multinational corporation, multinational Conglomerate (company), conglomerate founded in 1910 and headquartered in Chiyoda, Tokyo. The company is active in various industries, including digital systems, power and renewable ener ...
during the final years of
World War II World War II or the Second World War (1 September 1939 – 2 September 1945) was a World war, global conflict between two coalitions: the Allies of World War II, Allies and the Axis powers. World War II by country, Nearly all of the wo ...
. The first prototype ran in 1944 at a rating of , 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.


Design

In 1942, the most powerful Japanese aircraft engine in service produced less than and the
Imperial Japanese Army The Imperial Japanese Army (IJA; , ''Dai-Nippon Teikoku Rikugun'', "Army of the Greater Japanese Empire") was the principal ground force of the Empire of Japan from 1871 to 1945. It played a central role in Japan’s rapid modernization during th ...
understood that this constrained the development of higher performance aircraft. In response, in December 1942, the Army issued a request for a new radial aircraft engine capable of more than which was to be designated Ha.51. Two companies responded, Nakajima and
Hitachi () is a Japanese Multinational corporation, multinational Conglomerate (company), conglomerate founded in 1910 and headquartered in Chiyoda, Tokyo. The company is active in various industries, including digital systems, power and renewable ener ...
. The Hitachi engine was designed at the company’s engine plant in Tachikawa as a 22-cylinder engine, with cylinders arranged as a two-row radial engine with 11 cylinders per row instead of 9. The resulting Hitachi design was one of the first radial aircraft engines with more than twenty cylinders developed anywhere in the world. The engine had a steel crankcase, with an aluminium head mounted on steel cylinders each of bore and stroke , similar to the eighteen-cylinder Nakajima Homare, but angled at 60° rather than 78° to accommodate the additional four cylinders. Five engines were ordered and three built. The first ran in 1944. One prototype engine was built and ran for 100 hours on test. The engine reported very high oil consumption, up to 20g/kW⋅h, which was attributed to the rigidity of the crankcase. The factory was bombed on 24 April 1945 and the programme was halted. The Japanese Army did not have an aircraft available that needed the engine and development had taken substantial resources and these were to redirected to producing engines that had a more immediate need.


Surviving engines

A single example found at Haneda is on display at the museum next to
Narita airport , also known as Tokyo-Narita International Airport or simply Narita Airport, formerly and originally known as , is the secondary international airport serving the Greater Tokyo Area, the only other one being Haneda Airport (HND). It is about e ...
.


Specification


See also


References


Citations


Bibliography

* * * {{Hitachi aeroengines 1940s aircraft piston engines Aircraft air-cooled radial piston engines Hitachi aircraft engines