PW 100 series of engines are the forefront in modern day, condition of the artwork regional and commuter turboprop engines. With its 3 spool style and design, effortless to maintain modular design, and significant electric power ranking, the motor is a rational alternative for medium to massive turboprops which include the Bombardier Q400, DeHavilland Dash 8 and Embraer EMB 120. Some consider the PW 100 to be the alternative to the venerable PT6, but in fact the PW 100 picks up wherever the PT6 Substantial variation still left off in conditions of energy, gas economic system, and reliability. The PW 100 sequence consists of a amount of versions. There is no true PW 100 motor the engines start off with the PW118 engine and finish at the PW127J.

The engines are effectively the exact same, with, for the most element, a steady maximize in electrical power output, as nicely as slight variations in motor output pace and in the proportion of mechanical shaft horsepower vs. thrust made. In other phrases, every turboprop is rated in equivalent shaft horsepower, (eshp) which is a blend of the real mechanical horsepower offered at the output shaft combined with the sum of horsepower obtainable as a conversion of the thrust that is produced at the tailpipe. The proportion differs, but is ordinarily in the variety of 80% ability generated by the propeller, 20% produced by the tailpipe.

The Effective Product PW 100 Motor is wholly modular in its building that is, it is created up of a range of interchangeable modules that can quickly be taken off and changed in the occasion that there is a challenge with the motor. The modules consist of the turbo-device, the energy turbine assembly, the inlet housing, and the output reduction gearbox. The compact turbo-equipment is made up of the twin spool gasoline generator and the accessory gearbox. The electricity turbine connects to the rear of the turbo-equipment and characteristics a two phase electricity turbine which drives a shaft that runs forward up the heart of the turbo-equipment shafts. The inlet housing mounts to the entrance of the turbo-machine and supplies the space for air to be drawn into the compressor and the support for the output reduction gearbox. The output reduction gearbox mounts to the front of the inlet housing and can take the high velocity input from the electrical power turbine shaft and converts it to a large torque, minimal rpm output taken off the propeller flange at the entrance of the gearbox.

Atmospheric air is drawn in by means of the engine nacelle driving the propeller into a passive particle separator, which is component of the nacelle. Clear ingestion air is drawn upward into the downward dealing with scroll style motor inlet. Air is drawn into the turbo-equipment by the one phase, centrifugal compressor. The air is accelerated outward by the compressor and fed into various curved diffuser ducts which smoothly deposit the airflow to the experience of the solitary phase, centrigugal, large strain compressor. The substantial pressure compressor raises the strain to a structure pressure ratio of approximately 15:1 on some of the later models. The higher tension compressor feeds the airflow to a diffuser which converts the dynamic force into static tension, as it enters the annular, reverse movement combustor. The compressed air enters the interior combustion liner wherever it is mixed with jet gasoline and ignited. The resultant gas is expanded through the high force nozzle to impinge on the single stage axial large tension turbine, which drives the substantial stress compressor and the accent gearbox. The gas is then even more expanded through the reduced pressure nozzle to push the minimal force turbine, which drives the low pressure compressor. Last but not least, the fuel is expanded by the two stage energy turbine to drive a concentric shaft up to the front of the engine, which drives the output reduction gearbox. The exhaust is then directed out of the short, axial circulation, fixed place exhaust outlet to offer shut to 2,000 lbs. of thrust on some Popular Types of PW-100 Engine. The output reduction gearbox lowers electricity turbine speed down to a usable 1,200 or 1,300 rpm, to travel a four bladed, continuous velocity propeller. Accessories incorporate a generator, oil pumps, fuel pumps, hydraulic pumps, and a FADEC gas manage.

The twin spool compressor features many pros above a very similar one spool compressor. By enabling the two compressors to run at distinctive speeds, the compressors can be optimized a vast variety of airflows. This allows for a better design and style stress ratio, a lot much better portion energy effectiveness, and incredibly quick motor response. Superior stress ratios and substantial turbine inlet temperatures allow for incredibly low particular fuel consumption, and advanced cooling procedures and condition of the art components enable for long time involving overhaul periods.

There are a few of other variants of the PW 100 that are well worth mentioning. The PW150 engine is a high electricity growth of the PW 100 it is pretty similar in general structure and dimensions to the PW 100, besides that the very low strain compressor is a one phase axial adopted by a single phase centrifugal. Force ratio is a better 18:1, and the motor makes ability in the 5000 es-hp class, which can make it a acceptable alternative for the Allison T56 or an different to the Rolls Royce AE1107C. There are also turbo-shaft versions of the PW 100, wherever the output reduction gearbox and inlet are eradicated and replaced with a screened bell-mouth inlet and a provider bearing. The engine output is at electricity turbine pace. The engine could be an alternative to the CT7 (T700) turbo-shaft in medium helicopters, even though so significantly it has not been made use of in this application. There is a maritime variant of this turbo-shaft offered for contemporary military floor outcome ships, on the other hand. These models are referred to as the ST18M. Power output is around 3,200 shaft horsepower.