Hitachi Hatsukaze

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Hatsukaze
Klemm 35 Hirth HM504.jpg
The Hitachi Hatsukaze was a license-built Hirth HM 504, shown here installed in a Klemm Kl 35
Type Four-cylinder liquid-cooled inverted Inline piston engine
National origin Japan
Manufacturer Hitachi
Major applications Kyushu K9W1
Kokusai Ki-86
Number built 1,376
Developed from license-built Hirth HM 504

The Hitachi Hatsukaze also known as the Hitachi model GK4, was Hitachi's fourth design in a series of aircraft engines built in Japan prior to and during World War II. The original Hatsukaze was a license-built Hirth HM 504. Hatsukazi 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-built Bücker Bü 131 Jungmann variants that were the standard primary trainers for the Imperial Japanese Navy and Imperial Japanese Army.

The naval version of the engine was designated GK4, the army version as Ha-47.

The Hatsukaze Model 12 was the power section linked to a compressor to create a primitive jet engine called a motorjet, the resulting Tsu-11 was intended to power Yokosuka MXY7 Ohka 22 flying bombs. The standard Hatsukaze 11 engine was modified at a Navy arsenal by replacing the propeller drive shaft and engine front crankcase cover with a step-up gearbox. After modification, the engine was designated as the . 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. The heated compressed air then exits through the tailpipe providing static thrust of 180 kg (396 lb). 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 the Yokosuka MXY-9 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
82 kW (110 hp) IJN version, 339 built [2]
GK4A Ha-47 11
82 kW (110 hp) IJA version, 1,037 built[2]
Hatsukaze Toku ("Toku" translates as "special") Model 13
power section for the Ishikawajima Tsu 11 Motorjet engine

Applications[edit]

Specifications (Hatsukaze GK4A)[edit]

General characteristics

  • Type: 4-cylinder air-cooled inline piston engine
  • Bore: 110 mm (4.13 in)
  • Stroke: 125 mm (4.53 in)
  • Displacement: 4,752 cm3 (290 in3)
  • Length: 1,070 mm
  • Width: 200 mm
  • Dry weight: 115 kg

Components

  • Cooling system: Air-cooled

Performance

See also[edit]

References[edit]

Notes
  1. ^ Francillon p. 505.
  2. ^ a b Bridgeman
Bibliography
  • Bridgeman, Leonard. "The Bücker Bü 131B 'Jungmann'." Jane's Fighting Aircraft of World War II. London: Studio, 1946. ISBN 1-85170-493-0.
  • Jackson, Paul. Jane's All The World's Aircraft 2003–2004. Coulsdon, UK: Jane's Information Group, 2003. ISBN 0-7106-2537-5
  • Francillon, R.J. Japanese Aircraft of the Pacific War. London, Putnam, 1970. ISBN 370 00033 1.