Turbines

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Name Family Aircraft Engine Manufacturer Aircraft Engine Type Comment Dry Weight Diameter Full Weight Length Height Width Control System List Price Program launch FETT First Flight Certification Production Start Production End Service End Number Built LPCompressorStages LPCompressorTechnology IPCompressorStages IPCompressorTechnology HPCompressorStages HPCompressorTechnology CombustionChamber HPTurbineStages HPTurbineTechnology IPTurbineStages IPTurbineTechnology LPTurbineStages LPTurbineTechnology MaximumTakeoffPower MaximumContinuousPower OEI30sec OEI2min OEI2min5 OEIContinuous OverallPressureRatio T3 T4 T9 BPMaxRotationSpeed IPMaxRotationSpeed HPMaxRotationSpeed MaxRotatingDiameter OutputSpeed ThrustToWeight SpecificFuelConsumption Fuel TimeBetweenOverhaul Modules HydrocarbonTakeOff HydrocarbonClimbOut HydrocarbotApproach HydrocarbonIdle HydrocarbonUnitaryAverage HydrocarbonUnitarySigma HydrocarbonUnitaryRange HydrocarbonUnitaryCharacteristic HydrocarbonUnitaryCharacteristictoRegulatory HydrocarbonLTO CarbonMonoxideTakeOff CarbonMonoxideClimbOut CarbonMonoxideApproach CarbonMonoxideIdle CarbonMonoxideUnitaryAverage CarbonMonoxideUnitarySD CarbonMonoxideUnitaryRange CarbonMonoxideUnitaryCharacteristic CarbonMonoxideUnitaryCharacteristictoRegulatory NOxTakeOff NOxClimbOut NOxApproach NOxIdle NOxUnitaryAverage NOxUnitarySD NOxUnitaryRange NOxUnitaryCharacteristic NOxUnitarytoStandard NOxUnitarytoCAEP2 NOxUnitarytoCAEP4 NOxUnitarytoCAEP6 NOxUnitarytoCAEP8 NOxLTO SmokeTakeOff SmokeClimbOut SmokeApproach SmokeIdle SmokeMax SmokeSigma SmokeRange SmokeCharacteristic SmokeCharacteristictoRegulatory FuelFlowTakeOff FuelFlowClimbout FuelFlowApproach FuelFlowIdle FuelLTO FuelVentingCompliant
Arrius 2G1 Arrius Safran Helicopter Engines Turboshaft Ka226 116.00 968.00 670.00 470.00 FADEC Single Channel 0 0 1 centrifugal Annular reverse flow 1 axial 0 1 axial 537.00 457.00 591.00 537.00 6000.00 Jet-A1 3000.00 2 NA
WZ-8D Arriel South Aero-engine Industry Corporation Turboshaft Z-11, AC311 Branding of the Arriel 1D1 produced under license by SAIC 122.00 1200.00 610.00 470.00 Hydromecanical 0 0 2 1 axial, 1 centrifugal Annular 1 axial 0 1 axial 531.00 466.00 6000.00 Jet-A1 5 NA