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The Chrysler 1.8, 2.0, and 2.4 are inline-4 engines designed originally for the Dodge and Plymouth Neon compact car. These engines were loosely based on their predecessors, the Chrysler 2.2 & 2.5 engine, sharing the same 87.5 mm (3.44 in) bore. The engine was developed by Chrysler with input from the Chrysler-Lamborghini team that developed the ...
The compression ratio of the engine is 10.5:1. [2] The 2.0 L engine was offered by Dodge in the Dodge Caliber. Outside North America, the 2.0 was the base engine for the 2007 Chrysler Sebring and 2008 Dodge Avenger. Applications: 2007–2012 Dodge Caliber SE and SXT, 158 hp (118 kW) and 141 lb⋅ft (191 N⋅m) torque; 2007–2017 Jeep Patriot ...
An illustration of several key components in a typical four-stroke engine. For a four-stroke engine, key parts of the engine include the crankshaft (purple), connecting rod (orange), one or more camshafts (red and blue), and valves. For a two-stroke engine, there may simply be an exhaust outlet and fuel inlet instead of a valve system.
The 2.4L version is an inline 4-cylinder engine that carries a bore of 88.0 mm, stroke of 97.0 mm and a 10.5:1 compression ratio; the engine dry weight is 146 kg (322 lb) and it makes 165 PS (121 kW; 163 hp) at 5,800 rpm and 22.3–23 kg⋅m (161–166 lb⋅ft; 219–226 N⋅m) of torque at 4,250 rpm.
MultiAir technology can increase power (up to 10%) and torque (up to 15%), as well as reduce consumption levels (up to 10%) and emissions of CO 2 (up to 10%), particulates (up to 40%) and NOx (up to 60%) [3] [7] when compared to a traditional petrol engine. The system also provides smoother cold weather operation, greater torque delivery, and ...
The American-Statesman's midweek high school soccer report for the Austin area: Boys. Georgetown 3, Hendrickson 1: Martin Valdes continued a season-long scoring binge with two goals and an assist ...
[2]: 172 The first engine fired successfully in September, and on August 16, 1942, a trial rocket stopped in mid-air and crashed due to a failure in the turbopump. [2] [4] The first successful V-2 launch was on October 3, 1942. [5] Starting from the 1938-1940, Robert H. Goddard's team also independently developed small turbopumps.
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