New low-friction, high efficiency engines made possible by the patented J-Clutch
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The J-Drive engine is an innovative internal combustion engine design made possible by Friction Physics' patented J-Clutch. The rugged and durable J-Clutch replaces the crankshaft with a rack-and-pinion power linkage named the J-Drive. After years of engineering and computer modeling J-Drive engines are ready for prototyping. Note that the technology disclosed here is protected by United States and international patents, both granted and pending.
Inline J-Drive Engine, Model J-10 prices-1
The Model J-10 is suited for trucking, marine and construction applications. Performance characteristics are similar to the boxer type, J9. Four cylinder models are shown here. Two cylinder, six cylinder, eight cylinder+ configurations are straight forward implementations.


Boxer Model J-9, aircraft configuration

Specifications and Thermodynamics

Friction Physics developed a detailed computer engine model that was proofed against standard aircraft engine performance. The Lycoming O-360 A1A was chosen to represent the current state of technology. Extensive performance data for the O-360 are available. After validation of the computer model against the O-360, Friction Physics presents simulation results for the model J-9 engine.

J-Drive engines provide:
  • greater fuel efficiency
  • greater power
  • far cooler operation
  • lower manufacturing cost

Model J-9 Dimensions vs. O-360

Click on image to play or expand. The J-Drive Engine Cycle Weight Advantage
Characteristic O-360 Simulation O-360 Published Model J-9 notes
bore 5.125 in 5.125 in 5.125 in combustion cylinder/piston diameter
displacement 361 cu-in 361 cu-in 506 cu-in For Model J-9, displacement is volume of chamber when valves close, not a measure of piston sweep
compression stroke 4.375 in 4.375 in 5.3 in
power stroke 4.375 in 4.375 in 6.24 in J-Drive extended power stroke
Compression Ratio 8.5 : 1 8.5 : 1 7 : 1
Fuel Type AVGAS 100LL automotive
percent Atkinson 0 0 26% by volume
weight 258 lbs ~370 lbs
power to weight ratio 0.7 HP/lb ~0.7 HP/lb


Full Power, Sea Level Performance

(click to expand) P-V Diagram O-360 vs. J-9 Model J-9 piston velocity/position curve
Characteristic O-360 Simulation O-360 Published Model J-9 notes
Power 180 HP 180 HP 260 HP
Fuel Rate 16.2 gal/hr 15-16 gal/hr 15 gal/hr
HP per (gal/hr) rate 10.8 HP/gal ~11.2 HP/gal 18 HP/gal inverse of gal/HP
EGT 1440 °F 1300 to 1400 °F 1215 °F Exhaust Gas Temp.
CHT 363 °F 350 to 435 °F 331 °F Cylinder Head Temp.
Engine Speed 2700 RPM 2700 RPM 1625 Cycles/min
power strokes/min 5400 5400 6500
mixture (Φ) 1.4 "full rich" 0.65 mixture equivalency ratio (ϕ)
Air/Fuel ratio 10.5 - 22.6 14.7 is stoichiometric
% fuel energy to shaft 25.3% - 40% fuel conversion efficiency
% burned fuel energy to exhaust 46.6% 44% 45% heat energy in expelled exhaust gas
power to engine heat 64 kilowatts - 60 kilowatts friction and conduction
BMEP 1012 kPa - 815 kPa Brake Mean Effective Pressure

75% Power Cruise at 5000 feet altitude

Characteristic O-360 Simulation O-360 Published Model J-9 notes
Power 135 HP 135 HP 190 HP
Fuel Rate 9.8 gal/hr 9.5-10 gal/hr 11 gal/hr
HP per (gal/hr) rate 13.75 HP/gal 17.6 HP/gal inverse of gal/HP
EGT 1406 °F 1350 to 1450 °F 1000 °F Exhaust Gas Temp.
CHT 353 °F 350 to 435 °F 275 °F Cylinder Head Temp.
Engine Speed 2400 RPM 2400 RPM 1610 Cycles/min
mixture (Φ) 1.1 rich of peak 0.55 mixture equivalency ratio (ϕ)
Air/Fuel ratio 13.36 - 26.7 14.7 is stoichiometric
% fuel energy to shaft 31.2% 29-30% 41% fuel conversion efficiency
% fuel energy to exhaust 43% 44% 42% heat energy in expelled exhaust gas
power to engine heat 63 kilowatts - 51 kilowatts friction and conduction
BMEP 850 kPa - 598 kPa Brake Mean Effective Pressure