AERONAUTICAL ENGINE M 09 By I C P

Зарегистрируйтесь, чтобы просмотреть полный документ!

РЕГИСТРАЦИЯ

AERONAUTICAL ENGINE M 09 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 PROJECT PHILOSOPHY Top view

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

I. C. P. Srl PROJECT PHILOSOPHY Side view

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

I. C. P. Srl FEM ANALYSIS MAIN CRANKCASE

I. C. P. Srl FEM ANALYSIS ENGINE ATTACHEMENT

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

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

I. C. P. Srl CRANKCASE GEAR BOX CRANKCASE

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

I. C. P. Srl ARCHITECTURE

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

I. C. P. Srl

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

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

I. C. P. Srl TIMING SYSTEM

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

I. C. P. Srl COOLING SYSTEM

I. C. P. Srl INVERTED FLIGHT

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

I. C. P. Srl LUBRICATION GULLIES

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

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

I. C. P. Srl LUBRICATION OIL PUMPS

I. C. P. Srl LUBRICATION SYSTEM

I. C. P. Srl INVERTED FLIGHT

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)