An internal
combustion rotary engine, self cooled, totally concentric and symmetric, dynamically
variable compression ratio, capable of developing multiple Otto cycles in each rotation, by means using modules, composed mainly by a solenoid
gate valve and three chambers operating at the rotor periphery, producing at low RPM, torsion of value near close at theoretical limit. High power / weight ratio, which increases substantially when number of modules increase, without
drive shaft length increase; plus reduced
internal friction, is a truly saver fuel
machine; with volumetric
asymmetry ratio between expansion and compression chambers, and that compression chambers working at beginning of the cycle at normal
atmospheric pressure, it gives a fast rise pressure peak, because of the almost wedged form of that chambers. Proper for many types of
combustion and class of fuels, including
hydrogen, liquefied
propane gas and efficient use of air compressed as
external energy supply. Excels in aircraft use.