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  2. Toyota T engine - Wikipedia

    en.wikipedia.org/wiki/Toyota_T_engine

    The EFI system saw the introduction of knock control. It is turbocharged by a Toyota CT20 Turbo (the same unit as used in the 2L-T diesel) to generate 160 PS (118 kW; 158 hp) at 6,000 rpm and 206 N⋅m (152 lb⋅ft) at 4,800 rpm. This was the first turbocharged twin-cam engine built in Japan.

  3. Toyota R engine - Wikipedia

    en.wikipedia.org/wiki/Toyota_R_engine

    The first fuel injected 22R-E engines appeared in August 1982. Output of these engines is commonly rated at 78 kW (105 hp; 106 PS) at 4,800 rpm and 185 N⋅m (136 lb⋅ft) at 2,800 rpm. In 1985, the engine was significantly reworked, output was up to 84 kW (113 hp; 114 PS) at 4,800 rpm and 190 N⋅m (140 lb⋅ft) at 3,600 rpm.

  4. Hitachi - Wikipedia

    en.wikipedia.org/wiki/Hitachi

    Hitachi, Ltd. [nb 1] (Japanese pronunciation: [çi̥taꜜtɕi]) is a Japanese multinational conglomerate founded in 1910 and headquartered in Chiyoda, Tokyo.The company is active in a range of industries, including digital systems, power and renewable energy, railway systems, healthcare products, and financial systems. [4]

  5. GM Medium Gasoline Engine - Wikipedia

    en.wikipedia.org/wiki/GM_Medium_Gasoline_Engine

    The high-performance turbocharged 1,995 cc (2.0 L) 20A4E engine with central direct injection has 79 mm × 81.5 mm (3.11 in × 3.21 in) bore and stroke, with cylinder pressure of 130 bar (1,900 psi) and compression ratio of 9.5:1 for Performance version and 10.5:1 for Eco version is developed and manufactured by Chinese Saic Motor company.

  6. Showa Corporation - Wikipedia

    en.wikipedia.org/wiki/Showa_Corporation

    Showa is a brand of high-performance automotive, motorcycle and outboard suspension systems of Hitachi Astemo, based in Gyoda, Saitama in Japan. [2] SHOWA Corporation headquarters in Gyoda, Japan. The company was founded in 1938 as Showa Aircraft Precision Works. [3]

  7. Nord Aviation CT20 - Wikipedia

    en.wikipedia.org/wiki/Nord_Aviation_CT20

    The Nord Aviation CT20 was a French turbojet-powered radio-controlled target drone introduced in 1957. Developed from the Arsenal / S.F.E.C.M.A.S. T.5.510, the CT.20 was built by Nord Aviation and powered by a Turbomeca Marboré II engine, providing a top speed of 900 km/h (560 mph; 490 kn) and a flying time of 55 to 60 minutes.

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