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98-90i PROJECT ENGINE AVIO RAP 98-90i

ENGINE AVIO RAP 98-90i - Robby Moto Engineering RAP 2015.pdf · 98-90i project headquarters in casalmaggiore - cremona - italy production and commercialization of aeronautical components

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Page 1: ENGINE AVIO RAP 98-90i - Robby Moto Engineering RAP 2015.pdf · 98-90i project headquarters in casalmaggiore - cremona - italy production and commercialization of aeronautical components

98-90i PROJECT

ENGINE AVIO

RAP 98-90i

Page 2: ENGINE AVIO RAP 98-90i - Robby Moto Engineering RAP 2015.pdf · 98-90i project headquarters in casalmaggiore - cremona - italy production and commercialization of aeronautical components

98-90i PROJECT

HEADQUARTERS IN CASALMAGGIORE - CREMONA - ITALY

PRODUCTION AND COMMERCIALIZATION OF AERONAUTICAL COMPONENTS AND

RACING MOTORBIKE PARTS

Page 3: ENGINE AVIO RAP 98-90i - Robby Moto Engineering RAP 2015.pdf · 98-90i project headquarters in casalmaggiore - cremona - italy production and commercialization of aeronautical components

98-90i PROJECT

CHARACTERISTICS

ENGINE AVIO

RAP 98-90i

Page 4: ENGINE AVIO RAP 98-90i - Robby Moto Engineering RAP 2015.pdf · 98-90i project headquarters in casalmaggiore - cremona - italy production and commercialization of aeronautical components

98-90i PROJECT

� Dedicated unit ULM – LSA

� Cooling system oil-air thermoregulated (Patented)

� Axis-Propeller

� Right-hand rotation

� Injection and ignition electrical redundancy with variable anticipation

AIRCRAFT

� Product engineering and industrialization to reduce the number of components

Page 5: ENGINE AVIO RAP 98-90i - Robby Moto Engineering RAP 2015.pdf · 98-90i project headquarters in casalmaggiore - cremona - italy production and commercialization of aeronautical components

98-90i PROJECT

� AIRCRAFT

Max power 105 cv a 2750 rpm

Max torque 275 Nm a 2420 rpm Max RPM 3000 giri/min

� ELICOPTER

Max power 120 cv a 3400 rpm Max torque 270 Nm a 2300 rpm

Max RPM 3350 giri/min

Page 6: ENGINE AVIO RAP 98-90i - Robby Moto Engineering RAP 2015.pdf · 98-90i project headquarters in casalmaggiore - cremona - italy production and commercialization of aeronautical components

98-90i PROJECT

Cylinders In Aluminium alloy with NIKASIL coating , oil cooled

Pistons Forged in aluminium alloy with double rings system

Head Oil cooling system , 2 parallel valves , Heron camera

Adjusting Valves Automatic , with hydraulic recover free play game

Camshafts 8 cams system , with different intake profile and exaust profile

Page 7: ENGINE AVIO RAP 98-90i - Robby Moto Engineering RAP 2015.pdf · 98-90i project headquarters in casalmaggiore - cremona - italy production and commercialization of aeronautical components

98-90i PROJECT

Page 8: ENGINE AVIO RAP 98-90i - Robby Moto Engineering RAP 2015.pdf · 98-90i project headquarters in casalmaggiore - cremona - italy production and commercialization of aeronautical components

98-90i PROJECT

� DYNAMOMETRIC BENCH TES

� MAPPING INJECTION SYSTEM

Page 9: ENGINE AVIO RAP 98-90i - Robby Moto Engineering RAP 2015.pdf · 98-90i project headquarters in casalmaggiore - cremona - italy production and commercialization of aeronautical components

98-90i PROJECT

� Cooling system : oil-air thermoregulated (Patented)

� Lubrification: Lobes pump managed from camshaft. SAE 15W50 API SL JASO MA

� Carter : Dry sump possibility

� Fuel : Leadless commercial fuel ,91 octane

� Alternator : 12V- 400W

� 1000 rpm- 18 A

� 2000 rpm- 28 A

� 3000 rpm- 32 A

Page 10: ENGINE AVIO RAP 98-90i - Robby Moto Engineering RAP 2015.pdf · 98-90i project headquarters in casalmaggiore - cremona - italy production and commercialization of aeronautical components

98-90i PROJECT

� Possibility to Interchange the flange The

silent block support flange can be adapted to each setup cases

� Alternator with redundancy possibility

� Predisposition for GOVERNOR setup

ENDURANCE TEST WITH PROPELLER

Page 11: ENGINE AVIO RAP 98-90i - Robby Moto Engineering RAP 2015.pdf · 98-90i project headquarters in casalmaggiore - cremona - italy production and commercialization of aeronautical components

98-90i PROJECT

� Weight 72.5 kg ca

(included : alternator , starter engine , intake system , lubricant , radiator.

excluded:exhaust system)

� Ratio Weight/Power 0,56 kg/hp

� Consume 280 gr/kWh(*)

� Ratio compression 11:1

� Bore/Excursion 98 mm x 90 mm

� Cylindrate 2715cc

� Dimensions 660mm X 653mm X 453mm

Page 12: ENGINE AVIO RAP 98-90i - Robby Moto Engineering RAP 2015.pdf · 98-90i project headquarters in casalmaggiore - cremona - italy production and commercialization of aeronautical components

98-90i PROJECT

Robby Moto Engineering s.r.l. Via Giulio Galluzzi 14

26041 Casalmaggiore (CR) Tel 0375-41728 Fax 0375-41491

[email protected]