| 摘要 |
The invention refers to a turbine-type combustion engine with compression ignition, designed to operate machines, equipment and means of transportation. The turbine-type combustion engine is made up of a turbine shaft (1) consisting of two tubular parts joined tightly in the middle by means of two chamber carrier disks (2), at whose extremity four annular working chambers (3) are mounted tightly, in which some pistons (4) are sliding in a circular translation motion. These pistons are mounted tightly on the ends of two balancing crossbars (5), which oscillate on a selective locking spindle (6), on both sides of the eccentric of this spindle which passes freely through the tubular parts of the turbine shaft (1). The ends of the spindle (6) are connected tightly to the exterior casing (8). The centres of four communication bridges are connected freely to the balancing crossbars (5). The heads of these bridges are joined freely by means of some bridge-head bolts, and some links (12) with radial translation motion are connected freely to two of the diametrically opposed bolts. The small end of a radial connecting rod (14) is connected freely to one of the bolts (11) without a link, its head lying freely on the eccentric of the selective locking spindle (6).
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