aeronautical engine m09

AERONAUTICAL ENGINE M09By I.C.P. Srl

PROJECT PHILOSOPHY

I.C.P. SrlSide view

PROJECT PHILOSOPHYObjectives: Realization of an aeronautical piston engineWith high performancesLow fuel consumptionLow environmental impactAerobaticI.C.P. Srl

PROJECT PHILOSOPHYTop viewI.C.P. Srl

PROJECT PHILOSOPHYCharacteristics:Innovative concepts applicationStudy of new patented systemStrictly aeronautical mentalityCombinig engineering theory and pratical aeronautical experience

I.C.P. Srl

PROJECT PHILOSOPHYSide viewI.C.P. Srl

THE PROJECT:Component FEM verification One piece crankcaseDesign that simplifies assembly and installationEasy bolt on installationLight weight (160 Lbs Ready To Fly)115 Hp I.C.P. Srl

FEM ANALYSIS MAIN CRANKCASEI.C.P. Srl

FEM ANALYSISI.C.P. SrlENGINE ATTACHEMENT

FEM ANALYSISI.C.P. SrlATTACHEMENT DETAILSCRANKCASE

CRANKCASE maximum strenght at a minimum weight I.C.P. SrlMAIN CRANKCASE

CRANKCASE I.C.P. SrlGEAR BOX CRANKCASE

ARCHITECTUREV 90 cylinderDisplacement 75 cu inch4-strokeIntegrated oil tankSmall front section to allow a more aerodynamic cowlingI.C.P. Srl

ARCHITECTUREI.C.P. Srl

Narrow angle combustion chamber, angled chamber roofTwin spark plugBest surface/volume ratio of the combustion chamber to improve combustion and fuel consumptionI.C.P. SrlARCHITECTURE

I.C.P. Srl

I.C.P. Srl

TIMING SYSTEMDouble overhead camshaft (4 valves per cylinder) with Morse-tec chainDifferential rate gear reduction systemAutomatical mechanical tensionerChain wear indicator (I.C.P. patent pending)Automatic decompressor (for easy start) of the exhaust valveI.C.P. Srl

I.C.P. Srl4 VALVES FOR CYLINDERTIMING SYSTEM

I.C.P. SrlTIMING SYSTEM

I.C.P. SrlTIMING SYSTEM

COOLING SYSTEMLiquid cooledCentrifugal pumpRegulating thermostatWater/oil heat exchanger incorporated in the oil tank

I.C.P. Srl

I.C.P. SrlCOOLING SYSTEM

I.C.P. SrlCOOLING SYSTEM

I.C.P. SrlINVERTED FLIGHT

LUBRICATIONDry sumpInertial oil suction (I.C.P. patent pending), to Guarantee oil flow in all flight attitudeIntegrated oil tank and lubrication circuit3 coaxial pumps ( 2 scavenger and 1 delivery) 2 oil filters: replaceable cartridge and a fixed plastic mesh at inertial oil suctionI.C.P. Srl

LUBRICATIONI.C.P. SrlLUBRICATION GULLIES

LUBRICATIONI.C.P. SrlALL TANK WITH INERTIAL OIL SUCTION

LUBRICATIONI.C.P. SrlOIL FILTERSPLASTIC MESHCARTRIDGE FILTER

LUBRICATIONI.C.P. SrlOIL PUMPS

I.C.P. SrlLUBRICATION SYSTEM

I.C.P. SrlINVERTED FLIGHT

FUEL SYSTEMAdministrated directly by CAN line also connected to the cockpit engine monitor 2 redundant system with continous self - diagnosisPrimary system: Magneti Marelli electronic injection with two Lamba probeSecondary system: mechanical injection carburator installed into the throttle body (I.C.P. patent pending) I.C.P. Srl

I.C.P. SrlTHROTTLE BODY AND INJECTORSFUEL SYSTEM

GEAR REDUCTION SYSTEMGears with long addendum profileDampenerOverload clutchGear reduction ratio 1:2.95

I.C.P. Srl

I.C.P. SrlGEAR REDUCTION SYSTEM

Starter with rare earth magnetos Free wheel clutchAutomatic exhaust valve compressor at start

I.C.P. SrlIGNITION SYSTEM

I.C.P. SrlSTARTER SYSTEM

GENERATORI.C.P. Srl32 Amp three-phase generator