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A T56 on a mobile test unit at MCAS Futenma, 1982 T56-A-1 (Series I) A 1,600 lb weight (730 kg) engine delivering 3,460 shp (2,580 kW) and 725 lbf (329 kgf; 3.22 kN) residual jet thrust, which is equal to 3,750 equivalent shp (2,800 kW); single-shaft 14-stage axial flow compressor, cannular combustion chamber with 6-cylindrical through-flow combustion liners, 4-stage axial flow turbine; 13,800 ...
Turbo-Hydramatic 425 (TH425 or THM 425, [1] later 325) was an automatic transmission developed and produced by General Motors. The THM425 was a derivative of the THM400; most parts directly interchange and some others will interchange with minor modifications. The internal parts spin the opposite direction in the THM425; the helical angle of ...
1995 V.M.C 2500 Turbotronic, 117 PS (86 kW) at 4,200 rpm and 235 N⋅m (173 lb⋅ft) at 2,200 rpm; This engine was also used in some early Toyota Land Cruisers & Hilux, and Opel Fronteras. The 425 OHV used in Chrysler Voyager 1991–2000 only 1996 and 1997 was with chain.
Engine fan with viscous drive. A fan clutch is a thermostatic engine cooling fan that can freewheel at low temperatures when cooling is not needed, allowing the engine to warm up faster, relieving unnecessary load on the engine. As temperatures increase, the clutch engages so that the fan is driven by engine power and moves air to cool the engine.
These motors are sometimes called DC motors, sometimes EC motors and occasionally DC/EC motors. DC stands for direct current and EC stands for electronically commutated.. DC motors allow the speed of the fans within a fan coil unit to be controlled by means of a 0-10 Volt input control signal to the motor/s, the transformers and speed switches associated with AC fan coils are not required.
In 1965, the USAF selected the A-7D as a replacement for its fast-jet F-100 and F-105 supersonic fighter-bombers in the close air support role. Though the USAF had wanted the TF30, Pratt & Whitney was unable to meet the production timetable, because its facilities were already committed to producing other engines.
The "T1-134" variant was proposed as a replacement for the engines on the Tu-134. D-436T2 The "T2" variant is uprated to 80 kN (18,000 lb f) of thrust and is used on the Tu-334-100D and the Tu-334-200D. [8] D-436TP The "TP" variant is a specific "maritime" corrosion-resistant version developed for use in the Be-200 amphibious aircraft. This ...
TF39s on a C-5 Galaxy, from the rear TF-39 on display at the Museum of Aviation View looking into the fan showing snubbered blades on the inner half-stage and inlet guide vanes in the outer duct in front of the full stage. The TF39 was a revolutionary 1960s engine rated from 41,000 to 43,000 lb f (191 to 205 kN) of thrust. It introduced use of ...
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