Rotary internal combustion engine

1) “Internal Combustion Engine, Rotary Engine Type, with Distinct Conception, Durability and Performance, Applied to all Types of Vehicle or Industrial Equipment”, being this engine (A) formed by a housing specifically defined by a main block (4), which is composed in its superior part by an intake nozzle (Ad) and a depletion nozzle (Ex) and in its inferior part by spark plugs (5), where this main block (4) is closed in its anterior part by an anterior plate (3), fixed through a plurality of fixation elements (1), such as hexagonal head bolts, being the frontal part of this main block (4) is closed by a posterior plate (21) through a plurality of fixation elements (23), such as hexagonal head bolts, being this main block (4) is characterized by having a cylindrical cavity (4a) that receives the assembly of a jacket component (6), which is also perfectly cylindrical, where it receives the assembly of a set of components, such as rotor component (13) in the form of a cylindrical solid, containing in its anterior and posterior ends an axial seal set (12) and an axial seal set axial (14), respectively, where to the rotor (13) is superposed a complementary component (11), such as a rotor cover and bearing base of connection with the anterior cam (8a), fixed through a plurality of fixation elements (10), such as hexagonal head bolts, being the rotor (13) presents fissures (3a), with polygonal profile composed by an initial trapezoidal conformation followed by a transition to the cylindrical form, which have the sliding guide elements (15) of connection of the divisors (17), with the rotor (13), where these fissures (13a) are disposed in a radial form among themselves in this rotor (13), also having this rotor (13) as reference point the neck (13b), whose interior receives a satellite gear element (13c) fixed to this one;

• being the fissures (13a) of the rotor (13) receive the assembly of the divisor set (17), which is composed by at least two divisor components (17a), (17b) and (17c), which fit among themselves in an intercalated form among the ring-like elements (17a′), (17b′) and (17c′), respectively, being each divisor component receives an assembly of a radial seal component (18), which makes the tangency of the internal wall of the jacket component (6), forming the radial sealing among these divisors (17a), (17b) and (17c) and the referred jacket (6), and also receives a set of axial seals (16) in the lateral faces, which makes the tangency of the plates of anterior closing (3) and the plate of posterior closing (21), forming the axial sealing among the divisors components (17a), (17b) and (17c) and the plates of anterior closing (3) and the plate of posterior closing (21), being each divisor component (17a), (17b) and (17c) is connected to the rotor (13) through its respective pivoted sliding guide element (15), which perfectly fit in the cylindrical cavities in the ends of the fissures (13a) of the rotor (13);
• also having a main axis component (8), formed by an axis of crankshaft type, containing cams (18a) and (18b), respectively, being the rotor (13) is to assembled over the cams (18a) and (18b), in a way of presenting free turn through an anterior bearing component (7) and a posterior bearing component (9), whose cams drive the movement of translation of the rotor (13), being this main axis is structured and stabilized by the fixed posterior bearing (22) and fixed anterior bearing (2) components, assembled in the central part of the posterior plate (21) and of the anterior plate (3), respectively, also being the rotor (13) has a rotation movement around its own axis, whose rotation movement is due to the interference of the satellite gear (13c), fixed to it, with the stationary planetary gear (20) fixed to any static element of the set that forms the engine (A).