Английская Википедия:Ishikawajima-Harima J3

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Шаблон:Short description

The Ishikawajima-Harima J3 was a Japanese turbojet aircraft engine. It was the first jet engine designed and built in Japan after the Second World War and was used to power the Fuji T-1 trainer and as a booster engine in the Kawasaki P-2J patrol aircraft.

Design and development

Development of the J3, the first Japanese post-war jet engine,[1] intended to power the Fuji T-1 jet trainer, was begun in 1955 by the Nippon Jet-Engine Company, with Ishikawajima-Harima Heavy Industries (IHI) being designated prime contractor in 1959.[2][3] The resulting engine was a small, simple axial-flow turbojet.

The first pre-production engine began flight testing in a Curtiss C-46 testbed in February 1960, with production deliveries beginning in April 1962.[4]

Operational history

While the J3 was designed to power the Fuji T-1, it was not ready in time and the first version of the T-1 was powered by imported British Bristol Orpheus engine. The J3-IHI-3 version of the engine equipped the later T-1B version.[4] A more powerful version of the J3, the J3-IHI-7 was used to re-engine the T-1Bs and as booster engines for the Kawasaki P-2J maritime patrol aircraft.[5]

Variants

Файл:J3-IHI-3 01.jpg
J3-1
Nippon Jet-Engine Company prototype.[3][6]
J3-IHI-3
Initial production version for Fuji T-1B trainer. 11.8 kN (2,645 lbf) thrust.[4]
J3-IHI-7
More powerful version used as auxiliary engine in the P-2J and to re-engine T-1B trainers. 13.7 kN (3,080 lbf) thrust.[5]
J3-IHI-7C
Шаблон:Cvt for take-off.
J3-IHI-8
Шаблон:Cvt for take-off.
J3-IHI-F
Aft-fan variant, Шаблон:Cvt.[4] — the later Ishikawajima-Harima F3 turbofan engine began flights in 1985.[7][8]

Applications

Specifications (J3-IHI-7C)

Шаблон:Jetspecs

See also

Шаблон:Aircontent

References

Шаблон:Reflist

Further reading

Шаблон:Commons category

Шаблон:IHI aeroengines Шаблон:Japan military gas turbine aeroengines

  1. Flight International 9 October 1976, p. 1150.
  2. Flight International 28 June 1962, p. 1012.
  3. 3,0 3,1 Taylor 1966, p. 492.
  4. 4,0 4,1 4,2 4,3 Taylor 1966, pp. 492–493.
  5. 5,0 5,1 Ошибка цитирования Неверный тег <ref>; для сносок Janes 76 не указан текст
  6. Шаблон:Cite book
  7. Hamada, T., Akagi, M., Toda, D., Shimazaki, H., & Ohmomo, M. (1989). T-4 Inlet/Engine Compatibility Flight Test Results. Presented at the AIAA/ASME/SAE/ASEE 25th Joint Propulsion Conference, Monterey, CA: American Institute of Aeronautics and Astronautics.
  8. Шаблон:Cite book