aeronautical engine m09
DESCRIPTION
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. - PowerPoint PPT PresentationTRANSCRIPT
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AERONAUTICAL ENGINE AERONAUTICAL ENGINE M09M09
By I.C.P. Srl
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PROJECT PHILOSOPHY
I.C.P. Srl
Side view
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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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PROJECT PHILOSOPHY
Top view
I.C.P. Srl
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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
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PROJECT PHILOSOPHY
Side view
I.C.P. Srl
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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
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FEM ANALYSISMAIN CRANKCASE
I.C.P. Srl
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FEM ANALYSIS
I.C.P. Srl
ENGINE ATTACHEMENT
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FEM ANALYSIS
I.C.P. Srl
ATTACHEMENT DETAILS CRANKCASE
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CRANKCASEmaximum strenght at a minimum weight
I.C.P. Srl
MAIN CRANKCASE
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CRANKCASE
I.C.P. Srl
GEAR BOX CRANKCASE
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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
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ARCHITECTURE
I.C.P. Srl
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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
ARCHITECTURE
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I.C.P. Srl
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I.C.P. Srl
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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
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I.C.P. Srl
4 VALVES FOR CYLINDER
TIMING SYSTEM
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I.C.P. Srl
TIMING SYSTEM
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I.C.P. Srl
TIMING SYSTEM
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COOLING SYSTEM
Liquid cooled Centrifugal pump Regulating thermostat Water/oil heat exchanger incorporated in
the oil tank
I.C.P. Srl
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I.C.P. Srl
COOLING SYSTEM
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I.C.P. Srl
COOLING SYSTEM
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I.C.P. Srl
INVERTED FLIGHT
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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
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LUBRICATION
I.C.P. Srl
LUBRICATION GULLIES
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LUBRICATION
I.C.P. Srl
ALL TANK WITH INERTIAL OIL SUCTION
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LUBRICATION
I.C.P. Srl
OIL FILTERS
PLASTIC MESH
CARTRIDGE FILTER
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LUBRICATION
I.C.P. Srl
OIL PUMPS
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I.C.P. Srl
LUBRICATION SYSTEM
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I.C.P. Srl
INVERTED FLIGHT
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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)
I.C.P. Srl
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I.C.P. Srl
THROTTLE BODY AND INJECTORS
FUEL SYSTEM
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GEAR REDUCTION SYSTEM
Gears with “long addendum” profile Dampener Overload clutch Gear reduction ratio 1:2.95
I.C.P. Srl
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I.C.P. Srl
GEAR REDUCTION SYSTEM
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Starter with rare earth magnetos Free wheel clutch Automatic exhaust valve compressor at
start
I.C.P. Srl
IGNITION SYSTEM
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I.C.P. Srl
STARTER SYSTEM
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GENERATOR
I.C.P. Srl
32 Amp three-phase generator
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