EP918Ti - 185HP (Turbo/EFI/FADEC)

Artikkelnr.: EP918Ti

€50.759 ex. VAT The markets best power to weight ratio engine ! Based on Rotax 916iS

NOK1,00 inkl. mva.

Produktinfo

As our engines are built to order, and comes with several options and in multiple configurations, orders must be places directly with us or via our global dealers via email or phone.

- Technical Engine Data

  •  Engine Displacement: 1352ccm3
  •  Bore x Stroke: 84.00x61.00mm
  •  Gearbox reduction ratio: 2.54:1
  •  Engine weight w/gearbox w/overload clutch, turbocharger, intercooler, exhaust system: 81.5Kg / 179.6lb
  •  Engine suspension frame: 2Kg / 4.4lb
  •  External Alternator: 3Kg / 6.6lb
  •  Air Guide Baffle: 0.4Kg / 0.8lb
  •  Fuel Pump Assy: 1.6Kg / 3.5lb
  •  Power output: 185HP (133Kw) 
  •  Torque: 266Nm (113ft/lb) @ 5300rpm
  •  PTO Torque: 592Nm (436ft/lb)@ 5800rpm
  •  Fluids: 50/50 Glycol/Water mix (silicate free), XPS 5W-50

- Operating Limitations

  •  Idle speed: 1800rpm
  •  Max rpm: 5800rpm (max 5 minutes)
  •  Max cont. rpm: 5500rpm
  •  Cruise rpm: 4000-5400rpm
  •  Critical Altitude: MAT max 50°C – 15.000’ Note – The max.cont. power is available up to critical altitude
  •  Operating Altitude: 23.000’
  •  Acceleration: -0.5G (max 5 seconds)
  •  Static roll angle: 40°
  •  Intake air temp: 50°C (120°F)
  •  Manifold pressure: Max 54In/Hg (Max.cont. 42In/Hg)
  •  Fuel: AKI 93 / 98 RON / E10 (Alternatively AVGAS UL91/100LL)
  •  Oil pressure below 3500rpm: 0.8-5Bar (11.6-72.5psi)
  •  Oil pressure above 3500rpm: 2.0-5Bar (29-72.5psi)
  •  Oil temp ground ops: 100°C (-4 – 212°F)
  •  Oil temp: min 50°C before max power, limit 130°C (120 – 266°F)
  •  Coolant temp ground ops: -20 – 90°C (-4 – 194°F)
  •  Coolant temp normal operations: 40 – 120°C (104 - 248°F)
  •  Fuel pressure: 2.5-4.0Bar (36-58psi)
  •  EGT limits: 950°C (1742F°)
  •  EGT-split: 200°C below 3ltr/hr, 500°C above 3ltr/hr
  •  Ambient temperature: Ground -20 – 50°C (-4 – 120°F)
  •  Ambient temperature: Flight -40 – 50°C (-40 – 120°F)
  •  Oil consumption: Max. 0.06 l/h (0.13 liq pt/h)


- Description & Key Features

  •  Fully sequential ignition and fuel control
  •  Closed loop EGT
  •  Adaptive knock control
  •  High Boost / Low Boost function
  •  CAN data stream
  •  EFIS compatible
  •  4-Cylinder
  •  4-stroke liquid-/air-cooled engine with opposed cylinders
  •  Dry sump forced lubrication with separate oil tank, automatic adjustment by hydraulic valve tappets
  •  Redundant electronic fuel injection and ignition
  •  Fully programable dual Engine Management System
  •  Dual alternators (15/35Amp)
  •  Electric starter (12 or 24 volt)
  •  Propeller speed reduction gearbox (2.54:1)
  •  Flow optimized equal lenght air intake system / intercooler
  •  Turbocharger / stainless steel exhaust
  •  TBO 1,200 hrs
  •  Maximum operating altitude 23.000 feet
  •  Maintenance in accordance with the Rotax® 915iS LMM/HMM. (Supplementary EP917Ti MM

• Tested To 202HP

• Dual ECU, Fully Redundant, Full FADEC

• CAN Aerospace - Communicates with Garmin, Dynon...

• Same Mounting Points And Dimensions As 915/916iS

• Sea Level Power Up To 15.000’

• Service Ceiling 23.000’

• Fully Sequential Fuel & Ignition Control

• Closed Loop EGT & Injector Control

• Adaptive Knock Control For Max Efficiency

• Fully User Tunable And Programmable ECU (2D/3D/4D)

• In-Flight High / Low Boost Setting

• Based On The Already Prooven 916iS

• Gyrocopter, Fixed wing, Helicopter, UAV, Airboat

• TBO 2000

• Available With Hyd.Governor Intake & Stubby Intake