TH9898A - A power deformation machine with a rotating piston in a spherical housing. - Google Patents

Abstract

Machinery for power deformation consists of Rotor assembly with The first rotor section (124) with the first pair of pistons (137,138) and the second rotor section (125), along with the second pair of pistons (135,136), which can be swayed forward and back in a manner related to the first pair to the shaft. rotate (117) of a machine While the second rotor is not connected to the first rotor and can be rotated together around the axis of rotation. The first rotor can be rotated in the first trajectory of rotation. While the second rotor part can move in a second way of motion which deflects the trajectory of such rotation. Set the first and second rotor sections inward for a common spherical volume. Arrange a guide device (116) for centering the second rotor part (125) in the second path of rotation within the rotor assembly (124,125) in the rigid connection to the machine housing.

Claims (4)

1. Machinery for deformation of power consists of Rotor assembly with The first rotor section (124) with the first pair of pistons (19,20,137, 138) and the second rotor section. (125) with the second pair of pistons (33,34,135,136), which has been adapted to move in a spherical socket. (10b, 110b) in the mechanical enclosures (17,117), which is characterized by a double and definite forward and backward rocking motion. Which is relative to the first pair of pistons And the first rotor section (19-21,124) is attached to the drive shaft or driven (17,117), while the aforementioned second rotor (33-35,125) cannot be rotated to the first rotor. Such (19-21,124) in order to perform a joint movement request The rotational axis (17a, 117a) of such a spindle (17,117), the first rotor can rotate in the first trajectory of the rotational rotation in the plane perpendicular to it. Whereas the aforementioned second rotor section can be rotated together with and can be rocked in a manner related to the first rotor segment. And the second rotor, which is led by a lead assembly (38,119) can be rotated in the second trajectory of the inclined rotation by the method or the device of the stationary guide (16,116) to the angle v in relation to the aforementioned first trajectory of rotation has a special characteristic. That Such first and second rotor sections are assigned. (19-21,33-35,124,125) inward of a common spherical volume corresponding to the spherical inner surface in the hood of such machines (10,110) and such stationary conductors (16,116 ) For introducing the aforementioned second rotor segment (33,35,125) in a forward and backward rocking motion. It is centered within the rotor assembly as a long stator with one end being rigidly attached to the mechanical cover (10,110). 1 has a special characteristic that The stationary guide device (16,116) is aligned with the rotating shaft (17,117) and extends through the mechanical cover from the bearing attached to the inner end of the rotating shaft ( 17,117) to the stationary installation on the opposite end of the cover of the said machine (10,110) 3. The machine in one of Clause 1 or 2 is characterized by that The stationary guide device (16,116) consists of a shaft assembly. It has been formed with two rod-shaped ends (16b, 16c, 16c, 116e) on opposite sides of the predominantly spherical middle (16c, 116g) and will provide the middle section. (16d, 116g) is attached to the annular guide groove (41,112) for supporting the guide assembly (guide ring 38,119), which will be rotatable in the said groove and by means of a pin process or device. (38,39,120a, 120b) and the corresponding bore or the same process or attachment attached to the third rotor (33-35,125) 4.Machine in Clause 1 or 3. Any one of them has a special characteristic that The stationary guide device (16,116) extends through the center portion of the first rotor section (19-21,124). The first rotor will be rotated mounting in relation to the fixed guide device. At (16,116) at the opposite end 5. The machine in any of the Clause 1 or 4 claims has a special characteristic that The first rotor section (124) passes end-to-end from the second rotor segment (125) through the radial outer rotor portion. (125a, 135,125b ", 136) The first (124) and second (125) rotor sections are mutually designated to the sliding oil sockets. Which is sealed close to the working chamber (131-134) and surrounds the stationary pilot device (116) and the associated lead assembly (119) and the process or connection device (121) from there to the rotor part. Second (125) 6. The machine in any one of Clause 1 or 5 has a special characteristic that The first rotor part (124) shall be determined inward of the region forming a hollow ball-shaped part in a spherical socket (110b) of the hood of such machine. Between the two spherical segments (125a ", 125b") of the annular outer portion of the aforementioned second rotor segment (125) The two opposite sections of the piston-forming portion (135,136) of that second rotor section (125) are formed. As a connecting device Outside, between the spherical segments (125a ", 125b") of the said second rotor section. In the area between the axial ends (137, 138) of the said rotor section (124) 7. The machine in claim 6 has the special characteristics that The first rotor section (124) in the axial direction relative to the axis of rotation (117a) has the middle section forming a casing. And the two opposite ball-shaped ends (137,138) with cut-off ends. These ends are mutually designated to the chamber (131-134) in The area between the ring-shaped segments of the sphere. (125a ", 125b") of the second rotor section (125) and an external piston connection device. (135,136), which is connected like a ring to the ring-shaped portion of the sphere. 8. The machine in Clause 1-7 of any claim has the special characteristics that Such second rotor part hinge (125) is connected to the pilot assembly (119) which is rotatable on the said stationary guide device (116) by means of a process or device of a centered interconnect device. And along a radial (121) which passes across Pass the middle layer of the first rotor section (124) in the socket between the first rotor segment (124) and the stationary guide device (116) and the associated lead assembly (119) 9. Machine in claim 1. -8 Any of the above has a special characteristic that Provide the aforementioned mechanical caps (110) with a pair of slots (161,164,162,163) at each opposite end, which are separated from each other relative to the angle of rotation. The cavity is inwardly positioned in the trajectory of movement of the peripheral edge of the spherical external surface of one associated end (137,138) of the first rotor segment (124) and is Adapt to get off Covered and opened by such ends (137,138) in different positions of rotation or rotation area of such rotor assembly. The circular external surface, which is fixed on the tip (137,138) of the first rotor section (124) and is symmetrical with the axis of rotation (117a) of the rotor assembly, has a longer section than its width. At the very least, 1 0. Mechanical In Clause 9, the machine is in the form of a pump, a compressor, an identical two-stroke internal combustion engine or a uniform two-stroke. It is characterized by the fact that the engine cover (110b) of the engine cover (110) is determined by the rotor assembly process and equipment (124,125) to four separate working chambers (131-134), which are connected in a separate manner. Each and alternately in pairs with the two strokes of the engine twice per revolution of the rotating assembly. In contact with one of the corresponding pairs of four channels (161,163,162,164) from which the first (161) and third (163) open the first and third compartments respectively. While the second channel (162) and the fourth (164) make the third and fourth compartment ejections, respectively 1. 1. Machinery in Clause 9. The machine is in the form of a four-stroke internal combustion engine. There is a special characteristic that the engine hood (110b) (110) is determined by the rotor assembly process or equipment (124,125) to four separate working chambers (131-134), which are connected in a separate manner. Each other and take turns in pairs with the corresponding two-stroke of the four-stroke engine. In contact with two pairs of channels (161,164,162,163) from which the first compartment (161) provides an inlet for the first operating room, and the second (162) provides an ejection chamber for the compressed air. From the second working chamber to the connecting chamber (150), which is radially positioned outside the third operating room (163), the inlet from the connection room (150) to the third operating room is formed. It is the expansion chamber, while the fourth compartment (164) leads to the exit from the fourth operating room into Exit 1. 2. The engine in claim 11 has special characteristics that outside the cooling case (106) of the engine. It forms an external combustion chamber with associated fuel injectors (150d, 150e) and the preferred method and combustion equipment (150f \ ') form the combustion chamber (150). Hollow (150a), which is the distance from the engine cover (110) and the cooler casing (106) 1 3. The engine in claim 12 has a special characteristic that It has provided the combustion chamber (150) with an internal layer of heat-resistant ceramic material. And which should be used then the next layer is a heat insulating ceramic material 1 4. The machine in any of the Claims 1 to 4 has a special characteristic that The first rotor (124), in the form of two hollow bodies (124a, 124b) forms a casing. It was prepared with the first pair of discrete rotating pistons (137,138) and rigidly connected to the rotating shaft (117), and surrounded by the aforementioned second rotor section ( 125), which is in the form of a two-piece annular assembly (125a, 125b) and is prepared with a second pair of pistons (135,136), which are both pivoting and rocking forward and back. And the intermediate transverse connection device (121) is connected to the stationary guide assembly (116) by a rotating guide ring (119), and the two such rotor sections (124,125) are defined as Together In such a way that the fluid and that should be used, and also to prevent gas. The working room (131-134) of the mechanical shield from the transverse connection device (121) and the aforementioned stationary guide device (116), which has an inward position and the corresponding guide ring ( 119)