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The 400 saw extensive use in full-size Chevrolet and GMC trucks; K5 Blazer/Jimmy, 1/2-ton, 3/4-ton, 1-ton, and even larger 'medium duty' trucks had an option to be equipped with a 400. The engine was available in midsize A-Body and full-size B-Body passenger cars until the end of the 1976 model year. Early models produced 265 hp (198 kW) with a ...
On wing times can reach 14,000 hours, an overhaul costs over $1.5 million and a set of LLPs $2.1 million for a 25,000 cycle life. [4] In 1995, GE invested $200 million to develop the -8C derivative for the CRJ700 .
Windshields offered greater glass area. Front-door armrests were redesigned with integral pull bars. The base model carried the inline six-cylinder 250 cu in (4.1 L), 105 hp (78 kW), three V8 engines (262 cu in (4.29 L), a 1975-only option, a 305 cu in (5.00 L) and a 350 cu in (5.7 L)) for 1976 only, were offered.
One of the companies Durant bought in 1909 was the Northway Motor and Manufacturing Company founded by Ralph Northway who had previously supplied engines to Buick, Oakland, Cartercar and other 1900s manufacturers, including V8 engines to Oldsmobile, Oakland and Cadillac when they were independent companies. [1]
Developed by GE Aircraft Engines during the late 1960s, the original engine comprises a single stage fan, driven by a 4-stage low pressure (LP) turbine, supercharging a 14-stage high pressure (HP) compressor, driven by a 2-stage HP turbine. An annular combustor is featured. The TF34-GE-400A is rated at 9,275 lbf (41.26 kN) static thrust.
J35-GE-2 3,820 lbf (17.0 kN) thrust, prototypes built by General Electric. J35-GE-7 3,745 lbf (16.66 kN) thrust, built by General Electric, powered the 2 Republic XP-84 Thunderjet prototypes J35-GE-15 4,000 lbf (18 kN) thrust, built by General Electric, powered the sole Republic XP-84A Thunderjet J35-A-3 4,000 lbf (18 kN) thrust J35-C-3
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