초록 ▼

A rotary engine has a cycloid rotor and a sealing grid including a face seal that rotates with the rotor, and including other seals that do not rotate with the rotor. As the rotor rotates within a housing, the rotor, housing and seal grid form at least one working chamber between them, the chamber u

A rotary engine has a cycloid rotor and a sealing grid including a face seal that rotates with the rotor, and including other seals that do not rotate with the rotor. As the rotor rotates within a housing, the rotor, housing and seal grid form at least one working chamber between them, the chamber undergoing a change from initial volume V1 to V2, which is less than V1, thus compressing a working medium, and subsequently expanding to volume V3, which may be larger than V1, such that the chamber volume is a smooth and continuous function of rotor's rotational angle.

대표청구항 ▼

1. An improved engine of the type including a cycloidal rotor having N lobes and a housing having a corresponding set of N+1 lobe-receiving regions for successively receiving the lobes as the rotor rotates about an axis relative to the housing, the housing having (i) a pair of sides axially disposed

1. An improved engine of the type including a cycloidal rotor having N lobes and a housing having a corresponding set of N+1 lobe-receiving regions for successively receiving the lobes as the rotor rotates about an axis relative to the housing, the housing having (i) a pair of sides axially disposed on first and second sides of the rotor, and (ii) a peak disposed between each pair of adjacent lobe-receiving regions, and (iii) an intake port and an exhaust port, wherein the improvement comprises: a plurality of peak seals, at least one of the plurality of peak seals disposed on each peak and configured to maintain contact with the rotor throughout a period of rotation of the rotor, each peak seal being radially biased against the rotor throughout the rotation of the rotor, due to a cycloidal geometry of the rotor and the lobe-receiving portions;a first passageway defined in the rotor to communicate cyclically between the intake port and a working chamber, the first passageway configured to allow air to enter from a radial face of the rotor into the working chamber, the working chamber defined as a volume lying between two peak seals, the housing and the rotor;a second passageway, distinct from the first passageway, defined in the rotor to communicate cyclically between the exhaust port and the working chamber, the second passageway configured to allow exhaust gas to exit from the working chamber through the radial face of the rotor;a first face seal, disposed between the first side of the housing and the rotor, configured to seal the working chamber; anda second face seal, disposed between the second side of the housing and the rotor, configured to seal the working chamber;wherein the first face seal is disposed near an outer edge of the rotor, the outer edge defined by an intersection of an axial face of the rotor with the radial face of the rotor,wherein the passageways and the face seals are configured to cause each face seal to maintain contact with both the rotor and one of the sides of the housing through all angular positions of the rotor while avoiding communication with either of the ports. 2. The engine according to claim 1, wherein each peak seal has a contact region with the rotor, and the contact region is curved with a radius of curvature equal to a radius of curvature of a theoretical roller, which theoretical roller is uniquely defined by the geometry of the rotor and the geometry of the lobe-receiving regions. 3. The engine according to claim 1, wherein the second face seal is disposed near a second outer edge of the rotor, the second outer edge defined by an intersection of a second axial face of the rotor with the radial face of the rotor. 4. The engine according to claim 1, wherein the first face seal is disposed on the axial face of the rotor, and the axial face includes a landing at the outer edge, wherein the landing is between the outer edge and the first face seal, the engine further comprising a button seal disposed so as to contact the rotor and the first face seal at the landing. 5. The engine according to claim 1, wherein, at a first angle of the rotor within the housing, the working chamber forms a compression chamber having a maximum compression chamber volume, and at a second angle of the rotor within the housing, the working chamber forms an expansion chamber having a maximum expansion chamber volume, the maximum expansion chamber volume being at greater than or equal to 1.0 times the maximum compression chamber volume. 6. The engine according to claim 5, wherein the maximum expansion chamber volume is at least 3 times the maximum compression chamber volume. 7. The engine according to claim 1, further comprising a plurality of lubricant channels in at least one of the sides, each of the plurality of the lubricant channels disposed so as to deliver lubricant to a corresponding one of the plurality of peak seals. 8. The engine according to claim 1, further comprising a lubricant channel in at least one of the sides, the lubricant channel disposed so as to continuously deliver lubricant to a corresponding one of the face seals. 9. The engine according to claim 1, wherein the housing has a working cavity, and a combustion chamber in fluid communication with the working cavity, wherein the engine further comprises:a piston disposed on the housing and configured to controllably enter into and withdraw from the combustion chamber;the rotor rotatably mounted within the working cavity, so as to form a working chamber of variable volume with the housing, at different angles of rotation of the rotor within the working cavity; anda controller synchronized to the angle of rotation of the rotor to controllably cause the piston to enter into and withdraw from the combustion chamber, so as to cause the combined volume of the working chamber and the combustion chamber to be constant over a range of angles of rotation of the rotor. 10. The engine according to claim 1, wherein the housing has a working cavity, wherein the engine further comprises:a shaft having an eccentric portion;the rotor having a first axial face, and a second axial face opposite the first axial face, the rotor disposed on the eccentric portion and within the working cavity, the rotor comprising a first cam on the first axial face, the first cam having an eccentricity corresponding to the eccentricity of the eccentric portion of the shaft; anda cover integral with, or fixedly attached to, the housing, the cover comprising a plurality or rollers, each roller engaged with the cam, wherein the cam guides the rotation of the rotor as the rotor rotates within the working cavity and orbits around the shaft. 11. The improved engine of claim 10, further comprising a second cam on the second axial face of the rotor. 12. An improved engine of the type including a rotor having N lobes and a housing having a corresponding set of N+1 lobe-receiving regions for successively receiving the lobes as the rotor rotates about its axis and orbits about an axis relative to the housing, the housing having (i) a pair of sides axially disposed on first and second sides of the rotor, and (ii) a peak disposed between each pair of adjacent lobe-receiving regions, and (iii) an intake port and an exhaust port, wherein the improvement comprises: a first passageway defined in the rotor to communicate cyclically between the intake port and a working chamber defined as a volume lying between two peak seals, the housing and the rotor, the first passageway configured to allow air to enter from a radial face of the rotor into the working chamber;a second passageway, distinct from the first passageway, defined in the rotor to communicate cyclically between the exhaust port and the working chamber, the second passageway configured to allow exhaust gas to exit from the working chamber through the radial face of the rotor;a sealing grid comprising a plurality of peak seals, at least one of the plurality of peak seals disposed on each peak and configured to maintain contact with the rotor, such peak seal being radially biased against the rotor; anda face seal, disposed on the rotor and configured to maintain contact with the sides of the housing and a chamfered portion of the rotor, and to seal the working chamber, such face seal being axially biased against the housing side;wherein the face seal is disposed near an outer edge of the rotor, the outer edge defined by an intersection of an axial face of the rotor with the radial face of the rotor,wherein the ports, passageways and face seal are configured to cause the face seal to maintain contact with both the rotor and one of the sides of the housing through all angular positions of the rotor while avoiding the face seal crossing over either of the ports. 13. The engine according to claim 12, wherein the face seal is a wire seal. 14. The engine according to claim 12, wherein the rotor is of a cycloidal geometry defined by a set of N+1 theoretical rollers, and each peak seal has a contact region with the rotor, and the contact region is curved with a radius of curvature approximating a radius of curvature of the theoretical roller that the peak seal replaces. 15. An improved engine of the type including a rotor having N lobes and a housing having a corresponding set of N+1 lobe-receiving regions for successively receiving the lobes as the rotor rotates about its axis and orbits about an axis relative to the housing, the housing having (i) a pair of sides axially disposed on first and second sides of the rotor, and (ii) a peak disposed between each pair of adjacent lobe-receiving regions, and (iii) an intake port and an exhaust port, wherein the improvement comprises: a first passageway defined in the rotor to communicate cyclically between the intake port and a working chamber defined as a volume lying between two peak seals, the housing and the rotor, the first passageway configured to allow air to enter from a radial face of the rotor into the working chamber;a second passageway, distinct from the first passageway, defined in the rotor to communicate cyclically between the exhaust port and the working chamber, the second passageway configured to allow exhaust gas to exit from the working chamber through the radial face of the rotor;a sealing grid comprising a plurality of peak seals, at least one of the plurality of peak seals disposed on each peak and configured to maintain contact with the rotor, such peak seal being radially biased against the rotor; anda face seal, disposed on the rotor and configured to maintain contact with the sides of the housing and to seal the working chamber, such face seal being axially biased against the housing side, where over the course of rotation the face seal does not cross over the intake or exhaust port, and 2×(N+1) button seals, one for each side of every peak, disposed within the housing side, axially biased toward the rotor and configured to maintain contact with the peak seal and the face seal,wherein the face seal is disposed near an outer edge of the rotor, the outer edge defined by an intersection of an axial face of the rotor with the radial face of the rotor,wherein the ports, passageways and face seal are configured to cause the face seal to maintain contact with both the rotor and one of the sides of the housing through all angular positions of the rotor while avoiding the face seal crossing over either of the ports. 16. The engine according to claim 15, wherein a profile of the face seal is generated as a cycloidal curve in which a radius of a theoretical roller used to generate the cycloidal curve is a radius of the button in the button seal. 17. The engine according to claim 15, wherein the rotor is of a cycloidal geometry defined by a set of N+1 theoretical rollers, and each peak seal has a contact region with the rotor, and the contact region is curved with a radius of curvature approximating a radius of curvature of the theoretical roller that the peak seal replaces.