| 摘要 |
<p>Two-stroke internal combustion rotary engine, comprised of and characterized by a system of two rotors (A and C) and the corresponding piston (B), all of which are situated inside the cylindrical cavity of the stationary block (I). (See figure 1). Said two rotors rotate mounted on two side plates of the body, rotor (C) concentrically end rotor (A) excentrically to the internal cylindrical surface of the block. The rotor (A) which projects with respect to the two side-plates of the block and to which may be coupled the power takeoff has, mounted in its elbow, the piston (B). By rotating said rotor (A) in the same direction as rotor (C) and two times faster, said piston is caused to move along the cylindrical cavity or cylinder of the latter rotor, thereby forming in the cylinder two variable volume chambers. With said two chambers operating in a combined way, one (I) as a chamber for the suction of the mixture and its transfer to chamber (II) and the latter as an explosion chamber providing for the phases of compression, explosion-expansion and exhaust end from which are scavenged the residual burnt gas; said engine operates performing all the phases of a conventional two-stroke cycle, with all its movable elements rotating at constant speed. (See the sequence of the cycle in figures 2-9, sheet 2).</p> |
