Patent ID: 8171911
Filing Date: 2012-05-08
Classification: F01C,F04C

Abstract:
1. Rotary internal combustion engine comprising: a mechanism converting thermal energy of combustion gases to rotational motion; wherein said mechanism converting thermal energy of combustion gases to rotational motion comprises precisely one stationary link, and precisely three moving links; wherein said stationary link is the engine body; wherein said three moving links are: a main rotor; a secondary rotor; an intermediate rotor; wherein said engine body includes two cylindrical cavities placed therein; wherein the longitudinal axis of symmetry of one of said two cylindrical cavities included in the engine body is parallel to the longitudinal axis of symmetry of the other of said two cylindrical cavities included in the engine body; wherein the longitudinal axis of symmetry of one of said two cylindrical cavities included in the engine body is displaced relative the longitudinal axis of symmetry of the other of said two cylindrical cavities included in the engine body by a distance l>0; wherein said main rotor assumes the shape of a first circular cylinder with a first circular cavity and a number n>0 of fins or pistons placed in said first circular cavity of the main rotor; wherein said main rotor is mounted rotatably in the first one of said two cylindrical cavities included in the engine body to form with the engine body a rotary kinetic couple; wherein the axis of rotation of the main rotor relative the engine body coincides with the longitudinal axis of symmetry of the first one of said two cylindrical cavities included in the engine body; wherein the longitudinal axis of symmetry of said first circular cavity of the main rotor is parallel to the axis of rotation of the main rotor relative the engine body; wherein said secondary rotor assumes the shape of a second circular cylinder with a second circular cavity placed in said second circular cylinder forming said secondary rotor; wherein said secondary rotor is mounted rotatably in the other of said two cylindrical cavities included in the engine body to form with the engine body a rotary kinetic couple; wherein the axis of rotation of the secondary rotor relative the engine body coincides with the longitudinal axis of symmetry of the other of said two cylindrical cavities included in the engine body; wherein the longitudinal axis of symmetry of said second circular cavity of the secondary rotor is parallel to the axis of rotation of the secondary rotor relative the engine body; wherein one end of said intermediate rotor is mounted rotatably in the first circular cavity of the main rotor so that the intermediate rotor forms with the main rotor a rotary kinetic couple; wherein the axis of rotation of said intermediate rotor relative the main rotor coincides with the longitudinal axis of symmetry of said first circular cavity of the main rotor; wherein the axis of rotation of said intermediate rotor relative the main rotor is displaced relative the axis of rotation of the main rotor relative the engine body by a distance w>0; wherein the other end of said intermediate rotor is mounted rotatably in the second circular cavity of the secondary rotor so that the intermediate rotor and the secondary rotor form another rotary kinetic couple; wherein the axis of rotation of said intermediate rotor relative the secondary rotor coincides with the longitudinal axis of symmetry of the second circular cavity of the secondary rotor; wherein the axis of rotation of said intermediate rotor relative the secondary rotor is displaced relative the axis of rotation of the secondary rotor relative the engine body by a distance d>0; wherein the axis of rotation of said intermediate rotor relative the main rotor is displaced relative the axis of rotation of said intermediate rotor relative the secondary rotor by a distance m>0; wherein the number n of fins or pistons are placed on said intermediate rotor; wherein said intermediate rotor fins or pistons are mounted between said main rotor fins or pistons to form 2n combustion chambers.