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The Rover K-series engine is a series of internal combustion engines built by Powertrain Ltd, a sister company of MG Rover. The engine was a straight-four cylinder built in two forms, SOHC and DOHC, ranging from 1.1 to 1.8 L; 67.9 to 109.6 cu in (1,113 to 1,796 cc).
From the X-100 Curtiss-Wright developed the larger X-200, of which the United States Air Force ordered two prototypes designated the X-19A. The X-19 had fore and aft high-mounted tandem wings . Each wing mounted two 13 ft (4.0 m) propellers that could be rotated through 90 degrees, allowing the aircraft to take off and land like a helicopter .
The engine is available in Australia, New Zealand, Pakistan, [1] India, Southern Africa, Central and South America. The twin-turbo variant saw its first use in September 2007 fitted to the 200-series Land Cruiser wagon, which is available in various worldwide markets. Yanmar also marinized the twin-turbo variant of this engine as 8LV. [2]
The flagship of the range, the 220 Coupé Turbo's performance came from the T-Series 2.0 litre 16 valve engine with turbocharging producing 200 PS (147 kW; 197 bhp) at 6000 rpm and 174 lb⋅ft (236 N⋅m) The fastest ever production Rover [4] achieved 150 mph (241 km/h) and a 0 to 60 mph time of 6.2 seconds and 30 to 70 mph in 5.7 seconds in a ...
The JT8D is an axial-flow front turbofan engine incorporating a two-spool design. There are two coaxially-mounted independent rotating assemblies: one rotating assembly for the low pressure compressor (LPC) which consists of the first six stages (i.e. six pairs of rotating and stator blades, including the first two stages which are for the bypass turbofan), driven by the second (downstream ...
The engine is a twin-rotor, 2X3X654 cc (39.9 cu in) displacement, liquid-cooled, gasoline Wankel engine design, with an integral mechanical gearbox reduction drive with a reduction ratio of 2.82:1. It employs dual electronic ignition systems and produces 150 hp (112 kW).
The C220, C221, C223 is a 2.2L engine with 58 hp and 93 ft·lb of torque used in the 1981–1982 Chevrolet LUV and the 1981 through 1987 Isuzu P'up; GM also used the C220 series as an option (RPO LQ7) with the Chevrolet S10/GMC S15; low demand led to its discontinuation after the 1985 model year where subsequent S-series were gasoline powered.
After proving [citation needed] the engine reliability on the ground and in the air, the project was merged into an official company structure. ULPower Aero Engines was officially formed in March 2006 to concentrate on the further design and manufacture of engines where light weight, power and reliability are important to the client.