| 摘要 |
The subject of the invention is the internal combustion wing engine. The engine has a body (1), comprising an internal chamber in a form of a solid of revolution, preferably a cylinder or a sphere, in axis of which a divided shaft (2) is placed, preferably into two parts, on concentric segments (3, 4) of which the wings (5, 6, 7, 8) are mounted rigidly, opposite in pairs, parallel to a shaft (2) axle, fitted and sealed to the longitudinal cross section of an internal chamber of a body (1) and a part of a shaft (2), preferably provided with the distance projections (9) and a timing gear, comprising at least two circumferential blockades (12, 13), fixing temporal or constant position of at least one pair of wings (5, 6, 7, 8), while wings (5, 6, 7, 8) are formed in such a way, that they divide the capacity of an internal chamber of a body (1) into zones (I, II, III, IV) of a variable volume, and in the internal space of the chamber in the body (1) between blockades (12, 13) at least one spark-plug (14) is located.
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