Ishikawajima-Harima J3

Last updated
J3
Ishikawajima-Harima XJ3 turbojet engine left front view in Yamato Museum May 6, 2019 02.jpg
Type Turbojet
National origin Japan
Manufacturer Ishikawajima-Harima
Major applications Fuji T-1
Kawasaki P-2J

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.

Contents

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

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
13.7 kN (3,080 lbf) for take-off.
J3-IHI-8
15.19 kN (3,415 lbf) for take-off.
J3-IHI-F
Aft-fan variant, 16.7 kN (3,750 lbf). [4] — the later Ishikawajima-Harima F3 turbofan engine began flights in 1985. [7] [8]

Applications

Specifications (J3-IHI-7C)

Data from Jane's All The World's Aircraft 1976–77 [5]

General characteristics

Components

Performance

See also

Comparable engines

Related lists

Related Research Articles

<span class="mw-page-title-main">BMW 003</span> Early German axial turbojet engine

The BMW 003 is an early axial turbojet engine produced by BMW AG in Germany during World War II. The 003 and the Junkers Jumo 004 were the only German turbojet engines to reach production during World War II.

<span class="mw-page-title-main">Ishikawajima Ne-20</span>

The Ishikawajima Ne-20 was Japan's first turbojet engine. It was developed during World War II in parallel with the nation's first military jet, the Nakajima Kikka.

<span class="mw-page-title-main">Mitsubishi T-2</span> Japanese supersonic jet trainer aircraft

The Mitsubishi T-2 was a supersonic jet trainer aircraft used by the Japan Air Self-Defense Force. Introduced in 1975, it was the first Japanese-designed aircraft to break the sound barrier. It was the basis of the Mitsubishi F-1 strike fighter. All T-2s were retired by 2006.

<span class="mw-page-title-main">Pratt & Whitney J57</span> Turbojet engine

The Pratt & Whitney J57 is an axial-flow turbojet engine developed by Pratt & Whitney in the early 1950s. The J57 was the first 10,000 lbf (45 kN) thrust class engine in the United States. It is a two spool engine.

<span class="mw-page-title-main">General Electric J79</span> Axial flow turbojet engine

The General Electric J79 is an axial-flow turbojet engine built for use in a variety of fighter and bomber aircraft and a supersonic cruise missile. The J79 was produced by General Electric Aircraft Engines in the United States, and under license by several other companies worldwide. Among its major uses was the Lockheed F-104 Starfighter, Convair B-58 Hustler, McDonnell Douglas F-4 Phantom II, North American A-5 Vigilante and IAI Kfir.

<span class="mw-page-title-main">Pratt & Whitney J75</span> Turbojet engine

The Pratt & Whitney J75 is an axial-flow turbojet engine first flown in 1955. A two-spool design in the 17,000 lbf (76 kN) thrust class, the J75 was essentially the bigger brother of the Pratt & Whitney J57 (JT3C). It was known in civilian service as the JT4A, and in a variety of stationary roles as the GG4 and FT4.

<span class="mw-page-title-main">Allison J35</span>

The General Electric/Allison J35 was the United States Air Force's first axial-flow compressor jet engine. Originally developed by General Electric in parallel with the Whittle-based centrifugal-flow J33, the J35 was a fairly simple turbojet, consisting of an eleven-stage axial-flow compressor and a single-stage turbine. With the afterburner, which most models carried, it produced a thrust of 7,400 lbf (33 kN).

<span class="mw-page-title-main">Fuji T-1</span> Japanese jet trainer aircraft

The Fuji T-1 Hatsutaka was Japan's first jet-powered trainer aircraft. Its first flight was in January 1958. A total of 66 T-1 planes were built. It was retired in March 2006.

<span class="mw-page-title-main">Kawasaki T-4</span> Japanese jet trainer aircraft

The Kawasaki T-4 is a Japanese subsonic intermediate jet trainer aircraft developed and manufactured by the commercial conglomerate Kawasaki Heavy Industries. Its sole operator is the Japan Air Self-Defense Force (JASDF), in part due to historic restrictions on the exporting of military hardware. In addition to its primary training mission, the T-4 has been used by the JASDF's Blue Impulse aerobatic team as well as liaison duties with most fighter units. The first XT-4 prototype flew on 29 July 1985, while the first production aircraft was delivered during September 1988.

<span class="mw-page-title-main">Rolls-Royce Trent 900</span> 2000s British turbofan aircraft engine

The Rolls-Royce Trent 900 is a high-bypass turbofan produced by Rolls-Royce plc to power the Airbus A380, competing with the Engine Alliance GP7000. Initially proposed for the Boeing 747-500/600X in July 1996, this first application was later abandoned but it was offered for the A3XX, launched as the A380 in December 2000. It first ran on 18 March 2003, made its maiden flight on 17 May 2004 on an A340 testbed, and was certified by the EASA on 29 October 2004. Producing up to 374 kN (84,000 lbf), the Trent 900 has the three shaft architecture of the Rolls-Royce Trent family with a 2.95 m (116 in) fan. It has a 8.5–8.7:1 bypass ratio and a 37–39:1 overall pressure ratio.

<span class="mw-page-title-main">Armstrong Siddeley Viper</span> 1950s British turbojet aircraft engine

The Armstrong Siddeley Viper is a British turbojet engine developed and produced by Armstrong Siddeley and then by its successor companies Bristol Siddeley and Rolls-Royce Limited. It entered service in 1953 and remained in use with the Royal Air Force, powering its Dominie T1 navigation training aircraft until January 2011.

<span class="mw-page-title-main">General Electric CJ610</span> Turbojet engine

The General Electric CJ610 is a non-afterburning turbojet engine derived from the military J85, and is used on a number of civilian business jets. The model has logged over 16.5 million hours of operation. Civilian versions have powered business jets such as the Learjet 23 and the Hamburger Flugzeugbau HFB 320 Hansa Jet. The engines are also used in the flyable Messerschmitt Me 262 reproductions built by the Me 262 Project in the United States.

<span class="mw-page-title-main">Bristol Siddeley Orpheus</span> 1957 turbojet aircraft engine family by Bristol Siddeley

The Bristol Siddeley Orpheus is a single-spool turbojet developed by Bristol Siddeley for various light fighter/trainer applications such as the Folland Gnat and the Fiat G.91. Later, the Orpheus formed the core of the first Bristol Pegasus vectored thrust turbofan used in the Harrier family.

<span class="mw-page-title-main">General Electric T58</span> American turboshaft engine for helicopters

The General Electric T58 is an American turboshaft engine developed for helicopter use. First run in 1955, it remained in production until 1984, by which time some 6,300 units had been built. On July 1, 1959, it became the first turbine engine to gain FAA certification for civil helicopter use. The engine was license-built and further developed by de Havilland in the UK as the Gnome, in the West Germany by Klöckner-Humboldt-Deutz, and also manufactured by Alfa Romeo and the IHI Corporation.

The Pratt & Whitney JT12, is a small turbojet engine. The Pratt & Whitney T73 is a related turboshaft engine.

<span class="mw-page-title-main">General Electric T64</span> Turboshaft engine

The General Electric T64 is a free-turbine turboshaft engine that was originally developed for use on helicopters, but which was later used on fixed-wing aircraft as well. General Electric introduced the engine in 1964. The original engine design included technical innovations such as corrosion resistant and high-temperature coatings. The engine features a high overall pressure ratio, yielding a low specific fuel consumption for its time. Although the compressor is all-axial, like the earlier General Electric T58, the power turbine shaft is coaxial with the HP shaft and delivers power to the front of the engine, not rearwards. Fourteen compressor stages are required to deliver the required overall pressure ratio. Compressor handling is facilitated by 4 rows of variable stators. Unlike the T58, the power turbine has 2 stages.

<span class="mw-page-title-main">Kawasaki P-2J</span> Japanese maritime patrol aircraft

The Kawasaki P-2J is a maritime patrol and ASW aircraft developed for the Japan Maritime Self-Defense Force. A turboprop-powered version of the radial-engined P-2 Neptune, the P-2J was developed as an alternative to buying the larger and more expensive P-3 Orion, which would eventually replace the P-2J in the 1980s.

<span class="mw-page-title-main">Fairchild J44</span>

The Fairchild J44 was a small turbojet developed in the 1940s by the Fairchild Engine Division.

<span class="mw-page-title-main">PZL Rzeszów SO-3</span>

The PZL Rzeszów SO-1 and PZL Rzeszów SO-3 are Polish turbojet engines designed by the Instytut Lotnictwa and manufactured by WSK PZL Rzeszów, to power the PZL TS-11 Iskra jet trainer. Thirty SO-1s were built, this being superseded by the improved SO-3, of which a further 580 were built. The engine has a seven-stage compressor, annular combustion chambers, and a single-stage turbine.

<span class="mw-page-title-main">Ishikawajima-Harima F3</span>

The Ishikawajima-Harima Heavy Industries (IHI) F3 is a low bypass turbofan engine developed in Japan by Ishikawajima-Harima Heavy Industries for the Kawasaki T-4 jet trainer aircraft. The first prototype engine, the XF3, was manufactured in 1981 and first flew in the XT-4 in July 1985. About 550 have been built.

References

  1. Flight International 9 October 1976, p. 1150.
  2. Flight International 28 June 1962, p. 1012.
  3. 1 2 Taylor 1966, p. 492.
  4. 1 2 3 4 Taylor 1966, pp. 492–493.
  5. 1 2 3 Taylor 1976, pp.735–736.
  6. Bridgman, Leonard, ed. (1959). Jane's all the World's Aircraft 1959–60. London: Sampson Low, Marston & Co. Ltd. p. 512.
  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. Wilkinson, Paul H. (1964). Aircraft engines of the World 1964/65 (20th ed.). London: Sir Isaac Pitman & Sons Ltd. p. 192.

Further reading