Movatterモバイル変換


[0]ホーム

URL:


Jump to content
WikipediaThe Free Encyclopedia
Search

Hitachi Hatsukaze

From Wikipedia, the free encyclopedia
Hatsukaze
Hitachi Hatsukaze at theNational Air and Space Museum
TypeFour-cylinder air-cooled invertedInlinepiston engine
National originJapan
ManufacturerHitachi
Major applicationsKyushu K9W
Kokusai Ki-86
Number built1,376
Developed fromHirth HM 504
VariantsIshikawajima Tsu-11

TheHitachi Hatsukaze (初風, Hatsukaze - fresh wind), also known as theHitachi GK4 (short Navy),Hitachi Army Type 4 110hp Air Cooled Inline (Army long),Hitachi Ha47 (Army Hatzudoki) andHa-11 model 11 (unified), was Hitachi's fourth design in a series ofaircraft engines built in Japan prior to and duringWorld War II. The original Hatsukaze was a license-builtHirth HM 504. Hatsukaze engines were air-cooled, four-cylinder, inverted inline engines developing around 82 kW (110 hp).[1]

Design and development

[edit]

Hatsukaze engines were produced in very large numbers, as the powerplant for the license-builtBücker Bü 131Jungmann variants that were the standard primarytrainers for theImperial Japanese Navy andImperial Japanese Army.

The naval version of the engine was designated GK4, the army version as Ha47.

TheHatsukaze Model 12 was the power section linked to acompressor to create a primitivejet engine called amotorjet; the resultingIshikawajima Tsu-11 was intended to powerYokosuka MXY7 Ohka Model 22flying bombs. The standard Hatsukaze Model 11 engine was modified at a Navy arsenal by replacing the propeller drive shaft and engine front crankcase cover with a step-up gearbox. The gearbox increased engine output shaft RPM at a 1:3 ratio. At engine speed of 3,000 rpm, the compressor section was operating at 9,000 rpm. The compressed air was then ducted into a combustion chamber where a liquid fuel was sprayed and burnt. The heated compressed air then exits through the tailpipe providing static thrust of 180 kgf (397 lbf). It is likely that about 1/3 of the total thrust was contributed by adding the combustion chamber aft of the compressor.

The Tsu-11 was also selected to power theYokosuka MXY9 Shuka ("Autumn Fire"), a trainer intended to prepare pilots for the Mitsubishi J8M rocket-powered interceptor. Neither of these aircraft entered service, however, as their development took place too late in the war.

Variants

[edit]
GK4 Hatsukaze
license-built Hirth HM 504 inverted inline four-cylinder aviation engine.
GK4A Hatsukaze 11
IJNAS (Imperial Japanese Navy Air Service) version, 82 kW (110 hp) ; 339 built.[2]
Ha47 Model 11
(long designationArmy Type 4 110hp Air Cooled Inline) IJAAS (Imperial Japanese Army Air Service) version, 82 kW (110 hp) ; 1,037 built.[2]
Hatsukaze Toku Model 13
("Toku" translates as "special") power section for theIshikawajima Tsu 11 motorjet engine

Applications

[edit]
  • Kyushu K9W1 Type 2 Momiji ("Cypress") license built Bücker Bü 131s.
  • Kokusai Ki-86 Type 4 ("Cypress") license built Bücker Bü 131s.

Specifications (Hatsukaze GK4A)

[edit]

General characteristics

Components

  • Cooling system: Air-cooled

Performance

See also

[edit]

Related development

Related lists

References

[edit]

Notes

[edit]
  1. ^Francillon p. 505.
  2. ^abBridgeman

Bibliography

[edit]
  • Bridgeman, Leonard. "The Bücker Bü 131B 'Jungmann'."Jane's Fighting Aircraft of World War II. London: Studio, 1946.ISBN 1-85170-493-0.
  • Francillon, R.J.Japanese Aircraft of the Pacific War. London, Putnam, 1970.ISBN 0-370-00033-1.
  • Goodwin, Mike & Starkings, Peter (2017).Japanese Aero-Engines 1910-1945. Sandomierz, Poland: MMPBooks.ISBN 978-83-65281-32-6.
  • Jackson, Paul.Jane's All The World's Aircraft 2003–2004. Coulsdon, UK: Jane's Information Group, 2003.ISBN 0-7106-2537-5
Piston engines
Retrieved from "https://en.wikipedia.org/w/index.php?title=Hitachi_Hatsukaze&oldid=1321527167"
Categories:

[8]ページ先頭

©2009-2026 Movatter.jp