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AERONAUTICAL ENGINE M09

AERONAUTICAL ENGINE M09. By I.C.P. Srl. I.C.P. Srl. PROJECT PHILOSOPHY. Side view. I.C.P. Srl. PROJECT PHILOSOPHY. Objectives: Realization of an aeronautical piston engine With high performances Low fuel consumption Low environmental impact Aerobatic. I.C.P. Srl.

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AERONAUTICAL ENGINE M09

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  1. AERONAUTICAL ENGINE M09 By I.C.P. Srl

  2. I.C.P. Srl PROJECT PHILOSOPHY Side view

  3. I.C.P. Srl PROJECT PHILOSOPHY Objectives: • Realization of an aeronautical piston engine • With high performances • Low fuel consumption • Low environmental impact • Aerobatic

  4. I.C.P. Srl PROJECT PHILOSOPHY Top view

  5. I.C.P. Srl PROJECT PHILOSOPHY Characteristics: • Innovative conceptsapplication • Study of new patented system • Strictly aeronautical mentality • Combinig engineering theory and pratical aeronautical experience

  6. I.C.P. Srl PROJECT PHILOSOPHY Side view

  7. I.C.P. Srl THE PROJECT: • Component FEM verification • One piece crankcase • Design that simplifies assembly and installation • Easy bolt on installation • Light weight (160 Lbs Ready To Fly) • 115 Hp

  8. I.C.P. Srl FEM ANALYSISMAIN CRANKCASE

  9. I.C.P. Srl FEM ANALYSIS ENGINE ATTACHEMENT

  10. I.C.P. Srl FEM ANALYSIS CRANKCASE ATTACHEMENT DETAILS

  11. I.C.P. Srl CRANKCASEmaximum strenght at a minimum weight MAIN CRANKCASE

  12. I.C.P. Srl CRANKCASE GEAR BOX CRANKCASE

  13. I.C.P. Srl ARCHITECTURE • V 90° cylinder • Displacement 75 cu inch • 4-stroke • Integrated oil tank • Small front section to allow a more aerodynamic cowling

  14. I.C.P. Srl ARCHITECTURE

  15. I.C.P. Srl ARCHITECTURE • Narrow angle combustion chamber, angled chamber roof • Twin spark plug • Best surface/volume ratio of the combustion chamber to improve combustion and fuel consumption

  16. I.C.P. Srl

  17. I.C.P. Srl

  18. I.C.P. Srl TIMING SYSTEM • Double overhead camshaft (4 valves per cylinder) with Morse-tec chain • Differential rate gear reduction system • Automatical mechanical tensioner • Chain wear indicator (I.C.P. patent pending) • Automatic decompressor (for easy start) of the exhaust valve

  19. I.C.P. Srl TIMING SYSTEM 4 VALVES FOR CYLINDER

  20. I.C.P. Srl TIMING SYSTEM

  21. I.C.P. Srl TIMING SYSTEM

  22. I.C.P. Srl COOLING SYSTEM • Liquid cooled • Centrifugal pump • Regulating thermostat • Water/oil heat exchanger incorporated in the oil tank

  23. I.C.P. Srl COOLING SYSTEM

  24. I.C.P. Srl COOLING SYSTEM

  25. I.C.P. Srl INVERTED FLIGHT

  26. I.C.P. Srl LUBRICATION • Dry sump • Inertial oil suction (I.C.P. patent pending), to Guarantee oil flow in all flight attitude • Integrated oil tank and lubrication circuit • 3 coaxial pumps ( 2 scavenger and 1 delivery) • 2 oil filters: replaceable cartridge and a fixed plastic mesh at inertial oil suction

  27. I.C.P. Srl LUBRICATION LUBRICATION GULLIES

  28. I.C.P. Srl LUBRICATION ALL TANK WITH INERTIAL OIL SUCTION

  29. I.C.P. Srl LUBRICATION CARTRIDGE FILTER PLASTIC MESH OIL FILTERS

  30. I.C.P. Srl LUBRICATION OIL PUMPS

  31. I.C.P. Srl LUBRICATION SYSTEM

  32. I.C.P. Srl INVERTED FLIGHT

  33. I.C.P. Srl FUEL SYSTEM • Administrated directly by CAN line also connected to the cockpit engine monitor • 2 redundant system with continous self - diagnosis • Primary system: Magneti Marelli electronic injection with two Lamba probe • Secondary system: mechanical injection carburator installed into the throttle body (I.C.P. patent pending)

  34. I.C.P. Srl FUEL SYSTEM THROTTLE BODY AND INJECTORS

  35. I.C.P. Srl GEAR REDUCTION SYSTEM • Gears with “long addendum” profile • Dampener • Overload clutch • Gear reduction ratio 1:2.95

  36. I.C.P. Srl GEAR REDUCTION SYSTEM

  37. I.C.P. Srl IGNITION SYSTEM • Starter with rare earth magnetos • Free wheel clutch • Automatic exhaust valve compressor at start

  38. I.C.P. Srl STARTER SYSTEM

  39. I.C.P. Srl GENERATOR 32 Amp three-phase generator

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