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<blockquote data-quote="Halcon_del_sur" data-source="post: 132427" data-attributes="member: 567">Este es el motor, aparentemente equipa al H-500 y al Bo-105:Rolls Royce Allison 250-C18 Gas Turbine Shaft EngineType: dual spool, free turbine turboshaft Inlet: Axial with fixed inlet guide vanes Compressor: Mixed flow; six stage axial, 1 stage centrifugal Burner: Single can reverse flow combustor Turbine: dual spool; two stage gas producer, two stage free power turbine Exhaust: upward facing, dual exhaust diffuser Power Rating: 317 shaft horsepower (SHP) at 6,016 rpm Peak Torque Output: 425 lb/ft at 1,500 rpm Weight: 143 lbs. Power/weight: 2.2:1 Air mass flow: 3.0 lbs/sec Compression Ratio: 6.2:1 at 51,000 rpm Maximum TIT: 1850 degrees F Specific Fuel Consumption: 0.70 lb/shp/hr <img src="http://img452.imageshack.us/img452/8183/250c20ki2.jpg" alt="" class="fr-fic fr-dii fr-draggable " style="" /><img src="http://img252.imageshack.us/img252/1936/250c18hn0.jpg" alt="" class="fr-fic fr-dii fr-draggable " style="" />Nótense los dos conductos laterales a la salida del cárter del compresor centrífugo, ambos se dirigen hacia la parte posterior del motor, que al tener flujo inverso presenta la tobera a la mitad de la máquina.<img src="http://img78.imageshack.us/img78/7942/800pxallison28mtu29250cll1.jpg" alt="" class="fr-fic fr-dii fr-draggable " style="" />Saludos.P.D: el motor de Labala no estaba lejos de estos 315 SHP que entrega el Allison, y es muchísimo más sencillo.</blockquote>

[QUOTE="Halcon_del_sur, post: 132427, member: 567"] Este es el motor, aparentemente equipa al H-500 y al Bo-105: [B]Rolls Royce Allison 250-C18 Gas Turbine Shaft Engine[/B] Type: dual spool, free turbine turboshaft Inlet: Axial with fixed inlet guide vanes Compressor: Mixed flow; six stage axial, 1 stage centrifugal Burner: Single can reverse flow combustor Turbine: dual spool; two stage gas producer, two stage free power turbine Exhaust: upward facing, dual exhaust diffuser Power Rating: [B]317 shaft horsepower (SHP)[/B] at 6,016 rpm Peak Torque Output: [B]425 lb/ft [/B]at 1,500 rpm Weight: [B]143 lbs.[/B] Power/weight: [B]2.2:1[/B] Air mass flow: 3.0 lbs/sec Compression Ratio: 6.2:1 at 51,000 rpm Maximum TIT: 1850 degrees F Specific Fuel Consumption: [B]0.70 lb/shp/hr [/B] [IMG]http://img452.imageshack.us/img452/8183/250c20ki2.jpg[/IMG] [IMG]http://img252.imageshack.us/img252/1936/250c18hn0.jpg[/IMG] Nótense los dos conductos laterales a la salida del cárter del compresor centrífugo, ambos se dirigen hacia la parte posterior del motor, que al tener flujo inverso presenta la tobera a la mitad de la máquina. [IMG]http://img78.imageshack.us/img78/7942/800pxallison28mtu29250cll1.jpg[/IMG] Saludos. P.D: el motor de Labala no estaba lejos de estos 315 SHP que entrega el Allison, y es muchísimo más sencillo. [/QUOTE]

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