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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.
The use of "G" to denote twin cam engines was decided on in 1971, with the renaming of the 10R into 8R-G. Before that, twin cams had received separate numerical codes. [1] In 1987, Toyota began assigning dual letter engine codes to some of the "engine family" categories in some engine lines, particularly six-cylinder models.
The initial design of the engine was a civil version of the Olympus 22R, redesignated as the 591. [1] The 22R had been designed for sustained (45 minutes) flight at Mach 2.2 [3] as the engine for the BAC TSR-2. The 591 was redesigned, being known as the 593, with specification finalised on 1 January 1964. [1]
TSR-2 with Olympus Mk.320 engines on display at the Royal Air Force Museum Cosford. The performance specification for the BAC TSR-2 was issued in 1962. It was to be powered by two BSEL Olympus Mk 320 (BOl.22R) engines each rated at 19,610 lbf (87.2 kN) dry and 30,610 lbf (136.2 kN) with reheat at take-off.
The 1985 model year (which began production in August 1984) saw the arrival of the electronically fuel-injected 2.4 L 22R-E (and 22R-EC with California emissions controls). This increased the power output from 96 hp (72 kW) for the 22R [18]: 204 to 116 hp (87 kW) for the 22R-E, [19] though the carbureted engine remained available until 1988 ...
Two of New York City’s firefighter unions are slamming the newly implemented $9 congestion toll plan, saying Sunday that it will likely hurt response times — which “could mean a difference ...