Engine compressor unit

Abstract

An engine compressor unit including at least one rotary engine; and at least one rotary compressor for compressing at least one gaseous fluid; the rotary engine including an engine housing including at least one engine ring that is rotatably supported in the engine housing about an engine axis, at least one engine cylinder that is arranged in the engine ring, wherein an engine piston is arranged in the at least one engine cylinder so that the engine piston defines a combustion chamber of the at least one engine cylinder together with a wall of the at least one engine cylinder, wherein the engine piston is supported in the at least one engine cylinder by an engine connecting rod so that the engine piston is movable in the at least one engine cylinder in a linear manner.

Claims

1. An engine compressor unit, comprising: at least one rotary engine; and at least one rotary compressor for compressing at least one gaseous fluid; the at least one rotary engine including an engine housing including at least one engine ring that is rotatably supported in the engine housing about an engine axis; at least one engine cylinder that is arranged in the engine ring, wherein a respective engine piston is arranged in the at least one engine cylinder so that the respective engine piston defines a combustion chamber of the at least one engine cylinder together with a wall of the at least one engine cylinder, wherein the respective engine piston is supported in the at least one engine cylinder by an engine connecting rod so that the respective engine piston is movable in the at least one engine cylinder in a linear manner; at least one engine piston axis about which the respective engine piston is rotatable so that the respective engine piston moves on a circular path during an operation of the at least one rotary engine, wherein the at least one engine piston axis is oriented parallel to the engine axis and arranged offset from the engine axis so that the respective engine piston performs a cyclic up and down movement within the at least one engine cylinder during a rotation of the at least one engine ring about the engine axis, the at least one rotary compressor, including a compressor housing including at least one compressor ring that is rotatably supported in the compressor housing about a compressor axis, at least one compressor cylinder that is arranged in the at least one compressor ring, wherein a respective compressor piston is arranged in the at least one compressor cylinder so that the respective compressor piston defines a compression chamber of the at least one compressor cylinder together with a wall of the at least one compressor cylinder, wherein the respective compressor piston is supported in the at least one compressor cylinder by a compressor connecting rod so that the respective compressor piston is movable in the at least one compressor cylinder in a linear manner; at least one compressor piston axis about which the respective compressor piston is rotatable so that the respective compressor piston moves on a circular path during an operation of the at least one rotary compressor; and at least one supercharger tube that is configured to provide flow connection between a gas outlet opening of the rotary compressor and a gas inlet opening of the at least one rotary engine that is controlled by the respective engine piston, so that at least a portion of a gas that is compressed by the at least one rotary compressor is fed or feedable to the combustion chamber of the at least one engine cylinder by the at least one supercharger tube, wherein the compressor piston axis is oriented parallel to the compressor axis and arranged offset from the compressor axis so that the respective compressor piston performs a cyclic up and down movement within the at least one compressor cylinder during a rotation of the at least one compressor ring about the compressor axis, wherein the at least one rotary engine and the at least one rotary compressor are coupleable with each other by a transmission arrangement so that torque is transferable between the at least one rotary engine and the at least one rotary compressor, wherein the engine housing and the compressor housing each include a radially inward extending rise on an inner enveloping surface, and wherein each rise extends over a partial angular range of the engine housing and the compressor housing respectively, wherein the at least one engine cylinder includes a respective first valve arrangement that is configured to let the gas out of the combustion chamber during an operation of the at least one rotary engine, wherein the respective first valve arrangement engages the engine housing at least over a partial angle range of a revolution of the at least one engine cylinder about the engine axis, wherein the engagement forces a respective first valve element of the respective first valve arrangement from a first valve seat, so that a flow connection is opened or openable between the combustion chamber of the at least one engine cylinder and an ambient, wherein the at least one compressor cylinder includes a respective second valve arrangement that is configured to let the gas out of the compression chamber during operation of the at least one rotary compressor, wherein the respective second valve arrangement engages the compressor housing at least over a partial angle range of a revolution of the at cylinder about the compressor axis, and wherein the engagement forces a respective second valve element of the respective second valve arrangement from a second valve seat, so that a flow connection is opened or openable between the compression chamber of the at least one compressor cylinder and the at least one supercharger tube.

2. The engine compressor unit according to claim 1, wherein a transmission axis of the transmission arrangement is provided, wherein the transmission arrangement rotates about the transmission axis during operation of the engine compressor unit, and wherein the transmission axis coincides with the engine axis and the compressor axis.

3. The engine compressor unit according to claim 1, wherein the transmission arrangement is coupleable so that a torque transmission between the at least one rotary engine and the at least one rotary compressor is activatable and deactivatable.

4. The engine compressor unit according to claim wherein the at least one rotary engine or the at least one rotary compressor are supported by a common stationary crankshaft, and wherein a shaft axis of the common crankshaft and the piston axis of the at least one rotary engine or the piston axis of the at least one rotary compressor are arranged parallel to one another and offset from one another.

5. The engine compressor unit according to claim 4, wherein the at least one rotary engine and the at least one rotary compressor are supported axially offset from each other along the common stationary crankshaft, wherein the piston axis of the at least one rotary engine and the piston axis of the at least one rotary compressor are arranged parallel to each other and offset from each other at the common stationary crankshaft, and wherein the piston axis of the at least one rotary engine and the piston axis of the at least one rotary compressor are arranged in a plane that is orthogonal to the shaft axis of the common stationary crankshaft and are arranged opposite to one another relative to the shaft axis of the common stationary crankshaft.

6. The engine compressor unit according to claim 1, wherein the at least one rotary engine and the at feast one rotary compressor are combined in a common engine compressor housing.

7. The engine compressor unit according to claim 1, further comprising: a generator unit configured to convert mechanical energy into electrical energy or vice versa, wherein the generator unit includes at least one generator housing in which a rotor is rotatably supported about a generator shaft of the generator housing, and wherein the generator shaft is at least temporarily coupleable with the transmission arrangement in a force transferring manner.

8. The engine compressor unit according to claim 1, wherein the rise of the engine housing extends at least over a partial angle range of a complete revolution of the at least one engine cylinder about the engine axis on an inner enveloping surface of the engine housing, and wherein a radial distance between a peak of the rise of the engine housing and the engine axis is less than a radial distance between the inner enveloping surface of the engine housing and the engine axis.

9. The engine compressor unit according to claim 8, further comprising: a support groove which is circumferentially arranged and closed at the inner enveloping surface of the engine housing and which cooperates with the rise of the engine housing.

10. The engine compressor unit according to claim 9, wherein the at least one valve arrangement includes a running roller or a support slide through which the at least one valve arrangement cooperates with the support groove.

11. A compression refrigeration machine driven by the engine compressor unit according to claim 1.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) The rotary engine according to the invention is subsequently described in more detail with based on an embodiment with reference to drawing figures, wherein:

(2) FIG. 1 illustrates a cross section through a rotary engine of an engine compressor unit according to the invention;

(3) FIG. 2 illustrates a side view of the engine compressor unit according to the invention;

(4) FIG. 3 illustrates an isometric view of the engine compressor unit according to the invention;

(5) FIG. 4 illustrates a detail of a transmission device of the engine compressor unit according to the invention;

(6) FIG. 5 illustrates a detail of the transmission device together with the connecting rod of the rotary engine and a rotary compressor of the engine compressor unit according to the invention;

(7) FIG. 6 illustrates a cross section of an engine compressor housing of the engine compressor unit according to the invention; and

(8) FIG. 7 illustrates an isometric view of the engine compressor housing.

DETAILED DESCRIPTION OF THE INVENTION

(9) The embodiment illustrated in FIGS. 1-7 includes an engine compressor unit 1 according to the invention that is formed by a rotary engine 2 according to the invention and a rotary compressor 3. The rotary engine 2 and the rotary compressor 3 are coupled with one another in a force transferring manner by a transmission device 10. The transmission device 10 in the instant embodiment is made from a coupling arrangement which is formed by a plurality of rods which are oriented parallel to a transmission axis 9 of the engine compressor unit 1.

(10) The rotary engine 2 and the rotary compressor 3 are essentially configured identical. The rotary engine 2 includes an engine ring 4 which includes in this case a total of six cylinders 6. Within the cylinders 6 of the rotary engine 2 a respective engine piston 7 is supported linear moveable. An engine piston 7 and a respective associated cylinder 6 and its outer wall jointly define a combustion chamber 26 in which a combustion of a fuel, for example natural gas or gasoline occurs during an operation of the rotary engine 2. The individual engine pistons 7 are respectively connected by a connecting rod 8 with a connecting rod disc 34 in a force transferring manner. A respective connecting rod 8 is coupled by a piston link 30 with the respectively associated engine pistons 7. The piston links 30 facilitate rotating the connecting rods 8 relative to the associated engine piston 7. The rotating movement between the connecting rod 8 and the engine piston 7 is performed about a link axis of the piston link 30. In addition to the regular connecting rods 8 each of the connecting rod discs 34 is furthermore connected with a master connecting rod 32. The master connecting rod 32 is connected torque proof with the connecting rod disc 34. The master connecting rod 32 is also connected in a non-pivotable manner with the associated engine piston 7 so that a rotation of the engine piston 7 relative to the master connecting rod 32 is blocked.

(11) During operation of the rotary engine 2 the engine ring 4 rotates about an engine axis 5. The rotation of the engine ring 4 is predetermined by the kinematics of the rotary engine 2 as will be described in more detail infra.

(12) As already described supra the instant rotary engine 2 includes a total of six cylinders 6 and consequently six engine pistons 7 and six connecting rods 8, 32. All connecting rods 8 of the rotary engine 2 are coupled to the same connecting rod disc 34. The individual connecting rods 8 are thus arranged in one plane and are not arranged offset from each other along the engine axis 5. During a rotation of the engine ring 4 one of the cylinders 6 or the associated master connecting rod 32 performs a guide function. The master connecting rod 32 is connected torque proof at a center of the connecting rod disc 34.

(13) The center of the connecting rod disc 34 is arranged on a piston axis 11 of the rotary engine 2. The piston axis 11 describes an axis about which the engine pistons 7 orbit during the rotation of the engine ring 4. An associated circular path 40 is illustrated in FIG. 1. The piston axis 11 is oriented parallel to the engine axis 5 of the rotary engine 2 and offset relative to the engine axis 5 by an eccentricity 41. The eccentricity 41 between the engine axis 5 and the piston axis 11 causes a linear stroke movement of the engine pistons 7 within the cylinders 6 to be converted into a rotating movement of the engine ring 4 during operation of the rotary engine 2. This principle is known under the designation rotary engine. In order to impart a torque upon the connecting rod plate 34 the individual connecting rods 8 are not aligned parallel to a connecting axis of the piston axis 11 and the respective piston link 30 of the respective engine piston 7 but pivoted relative to the this connection axis. This applies for all connecting rods 8 besides the master connecting rod 32 which is coupled directly in a straight line with the piston axis 11. This arrangement is necessary to reduce a degree of freedom of the connecting rod plate 34 from a number of 2 to a number of 1 and to force the individual engine pistons 7 to move on their circular path 40.

(14) The rotary compressor 3 has a configuration that is identical in principle to the rotary engine 2. In the illustrated embodiment the rotary compressor 3 also includes six cylinders 14 which are arranged in a compressor ring 12 of the rotary compressor 3. Within the cylinders 14 of the rotary compressor 3 compressor pistons 15 are supported in a linear moveably manner. The compressor pistons 15 are in turn connected by a connecting rod 16 at a connecting rod disc 34 which is a separate connecting rod disc. Put differently the connecting rods 8 of the rotary engine 2 and the connecting rods 16 of the rotary compressor 3 are arranged at different connecting rod discs 34. Also the rotary compressor includes a master connecting rod 32.

(15) The illustrated rotary engine 2 is operated as a two stroke engine, wherein the associated engine piston 7 performs two strokes within the cylinder 6 during a full revolution of a cylinder 6 of the rotary engine 2 by 360 about the engine axis 5. In the position of the rotary engine 2 illustrated in FIG. 1 the right cylinder 6 is in an ignition position in which the engine piston 7 is arranged in an upper reversal position. In this upper reversal position of the engine piston 7 the combustion chamber 26 of the cylinder 6 has a minimum volume. During a complete revolution of the cylinder 6 or the engine ring 4 about the engine axis 5 the engine piston 7 is rotated about the piston axis 11 once completely and thus moved from its upper reversal position into its lower reversal position and back again. The lower reversal position of an engine piston 7 is shown for the cylinder 6 that is illustrated on a left side of FIG. 1.

(16) Two stroke operations of the rotary engine 2 have the effect that a respective ignition occurs per revolution of the engine ring 4 in each other cylinder 6. Thus, it is irrelevant as a matter of principle whether the ignition is performed by a spark plug, for example in a gasoline engine, or self-acting, e.g. in a diesel engine. During a revolution of a respective cylinder 6 about the piston axis 5 the cylinder 6 or its combustion chamber 26 is emptied and recharged completely.

(17) In the illustrated embodiment charging can be performed in a particularly simple manner by a gas inlet opening 25, wherein each other cylinder 26 respectively includes one gas inlet opening. The gas inlet openings 25 are arranged at the cylinders 6 so that they are only released when the respective engine piston 7 is arranged in its lower reversal position. This position of a respective engine piston 7 is particularly advantageous for filling the combustion chamber 26 since the engine piston 7 moves back towards its upper reversal position after the lower reversal position so that a volume of the combustion chamber 26 is continuously reduced. The reduction of the volume of the combustion chamber 26 leads to a compression of the gas arranged in the combustion chamber and therefore to a significant pressure rise in the combustion chamber 26. This provides combustion conditions for a next ignition when the engine piston 7 is provided in its upper reversal position.

(18) The engine compressor unit 1 according to the invention has a peculiar feature in the illustrated embodiment. For starters the rotary engine 2 as well as the rotary compressor 3 are respectively configured with an identical number of cylinders 6, 14. Furthermore the cylinders 6, 14 are respectively arranged in pairs. This means that each of the cylinders 6 of the rotary engine 2 corresponds to a cylinder 14 of the rotary compressor 3 so that they do not have any angular offset relative to the engine axis 5 or the compressor axis 13 or the transmission axis 9. Put differently the individual cylinders 6, 14 are arranged along the transmission axis 9 of the engine compressor unit without an offset behind one another or in alignment with each other. Due to the torque proof coupling of the engine ring 4 with the compressor ring 12 the relative alignment of the cylinders 6, 14 with each other remains constant during the operation of the engine compressor unit 1.

(19) This embodiment facilitates to flow connect the rotary compressor 3 and the rotary engine 2 with one another through supercharger tubes 23. This embodiment is based on the idea to use the rotary compressor 3 so to speak as a supercharger for the rotary engine 2. For this purpose the rotary compressor 3 respectively includes a gas outlet opening 24 at its cylinders 14 or at outer ends of the cylinders 14 that are oriented away from the gas outlet opening 24. The gas outlet opening 24 is used for conducting gas that has been compressed by the rotary compressor 3 from the associated compression chamber of the respective cylinder 14. The gas thus compressed can now be conducted by the respectively associated supercharger tube 23 directly to the corresponding gas inlet opening 25 of the associated cylinder 6 of the rotary engine 2. This configuration facilitates to supercharge the rotary engine 2 and thus significantly improve efficiency of the rotary engine 2. For connecting the supercharger tubes 23 to the respectively corresponding cylinders 6, 14 of the rotary engine 2 and the rotary compressor 3 it is not required that the cylinders 6, 14 are arranged exactly without offset relative to the transmission axis 9, however this configuration is advantageous in order to be able to connect the supercharger tubes 23 in a simpler manner.

(20) The supercharger tubes 23 are respectively configured by a straight tube element, wherein a deflection of gas flowing through a supercharger tube 23 does not occur. The supercharger tubes 23 have a variable cross section over their axial length.

(21) In a particularly advantageous embodiment of the engine compressor unit 1 an atomized or gaseous fuel can be introduced into a respective supercharger tube 23 so that filling a combustion chamber 26 of an associated cylinder 6 of the rotary engine 2 is performed using the gas flow of the gas compressed by the rotary compressor 3.

(22) As evident in particular from FIG. 2 the rotary engine 2 and the rotary compressor 3 are arranged axially offset along the transmission axis 9. The rotary engine 2 and the rotary compressor 3 are connected for this purpose with one another by a transmission device 10. The connection between the rotary engine 2 and the rotary compressor 3 is thus performed in a torque transferring manner so that the rotation of the rotary engine 2 is transferred directly to the rotary compressor 3. Thus, the transmission arrangement 10 has plural struts which extend parallel to the transmission axis 9 and establish a fixed connection between the rotary engine 2 and the rotary compressor 3. The transmission arrangement 10 is visible quite well in particular in FIG. 3.

(23) In order to operate the engine compressor unit 1 according to the invention the rotary engine 2 is started and thus set in motion. The motion of the rotary engine 2 includes a rotation of the engine ring 4 about the engine axis 5. The circular motion of the engine ring 4 about the engine axis 5 is visible quite well in FIG. 1 based on the circular path 39 that is drawn in dashed lines. Due to the eccentricity 41 between the engine axis 5 and the piston axis 11 also the engine piston 7 rotate. Thus, the stroke movement of the engine pistons 7 forces the rotation of the engine ring 4 since the engine pistons 7 can only escape the axial force imparted upon them by rotating about the piston axis 11 and thus move the engine ring 4 along. Due to the eccentricity 41 the engine pistons 7 continuously perform lift movements in their respective cylinders 6. The engine pistons 7 thus move on a circular path 40 illustrated in FIG. 1, wherein a center of the circular path 40 is offset from a center of the circular path 39 by the eccentricity 41.

(24) The movement of the engine ring 4 is initiated by the combustion of a fuel in the combustion chamber 26 of the cylinder 6. The engine axis 5 and the piston axis 11 remain in place during operation of the rotary engine 2, this means they do not perform a movement. This means that the connecting rod disc 34 at which the individual connecting rods 8 and the master connecting rod 32 are connected also rotates about the piston axis 11. The master connecting rod 32 is connected at a center of the connecting rod disc 34, wherein a connection between the master connecting rod 32 and the connecting rod disc 34 is performed in a force transmitting manner. The remaining connecting rods 8 are respectively pivot ably connected with the connecting rod disc 34. Thus, the remaining connecting rods 8 are statically configured as pendulum rods since they are pivotably connected by piston links 30 at the engine piston 7 as well as pivot ably connected at the connecting rod disc 34.

(25) The rotation generated by the rotary engine 2 is transmitted directly to the rotary compressor 3 due to the transmission device 10. The rotary compressor 3 now functions in a manner that is exactly inverse to the rotary engine 2. This means that no fuel is provided for driving the rotary compressor 3, but a desired substance shall be removable from the rotary compressor 3. This is typically a compressed gas. In order to facilitate this a gas is supplied to the cylinders 14 of the compressor ring 12, wherein the gas is compressed in compressor chambers of the compressor ring 12 by the stroke movements of the compressor pistons 15. The lift movement of the compressor pistons 15 within the cylinders 14 of the compressor ring 12 follows the same principle as the stroke movement of the rotary engine 2. This means also the rotary compressor 3 includes respective connecting rods 8, 32 which cause a movement of the compressor pistons 15 within the cylinder 14 of the rotary compressor 3 during the rotation of the compressor ring 12. Thus, also the rotary compressor 3 includes an eccentrically arranged connecting rod disc 34 which is arranged offset by an eccentricity 41 relative to a compressor axis 13 of the rotary compressor 3.

(26) In the illustrated embodiment of the engine compressor unit 1 according to the invention the rotary engine 2 and the rotary compressor 3 are arranged along a common transmission axis 9. This means the engine axis 5 and the compressor axis 13 about which the engine ring 4 or the compressor ring 12 rotate coincide. For this configuration it is particularly advantageous to arrange the rotary engine 2 and the rotary compressor 3 on a common carrier shaft. Since the rotary engine 2 as well as the rotary compressor 3 is so to speak a kinematic ally inverted version of a typical piston engine the carrier shaft can also be considered as a crankshaft 18 that remains in place. The crankshaft 18 is visible quite well in FIG. 4 compared to a typical crank shaft of a reciprocating piston engine the crank shaft 18 is stationary during operation of the engine compressor unit 1. This means that the shaft as such as well as its elbows which are configured as pins 33 remain stationary during operation of the engine compressor unit 1. The connecting rod discs 34 of the rotary engine 2 and of the rotary compressor 3 are arranged at the pins 33 and rotate around them. Put differently center axes of the pins 33 coincide with the piston axes 11, 17 of the rotary engine 2 or the rotary compressor 3. A representation of the crank shaft 18 which includes the connecting rods 34 of the rotary engine 2 and of the rotary compressor 3 is derivable from FIG. 5.

(27) The crankshaft 18 is not used for transmitting torques between the rotary engine 2 and the rotary compressor 3. This is exclusively performed by the transmission device 10 that has been described supra. The shoulders of the crank shaft 18, this means the pins 33 are arranged offset relative to the transmission axis 9. As a consequence the engine piston 7 and the compressor pistons 15 are in their respective upper reversal position or lower reversal position at different points in time during operation of the engine compressor unit 1. In the illustrated embodiment the pins 33 of the crankshaft 18 are arranged directly opposite to the transmission axis 9 so that the corresponding compressor piston 15 is provided precisely in its lower reversal position when the respective engine piston 7 is in its upper reversal position. It is appreciated that the associated compressor piston 15 is in its upper reversal position when the engine piston 7 is in its lower reversal position.

(28) The arrangement of the engine pistons 7 and the compressor pistons 15 relative to each other has the advantage that the rotary compressor 3 is usable as a supercharger for the rotary engine 2. This is based on the idea that the engine piston 7 is arranged in its lower reversal position and opens gas inlet openings 25 of the cylinder 6 in the associated cylinder 6. Simultaneously the compressor piston 15 of the associated cylinder 14 of the rotary compressor 3 is in its upper reversal position in which gas arranged in the compressor chamber is compressed by a maximum amount. In this position of the compressor piston 15 the gas outlet opening 24 of the cylinder 14 is opened so that the compressed gas can flow through the straight supercharger tube 23 directly from the gas outlet opening 24 to the gas inlet opening 25 of the cylinder 6 of the rotary engine 2. There the compressed gas flows into the combustion chamber 25 of the cylinder 6 and fills it. The subsequent rotation of the engine ring 4 then provides an additional compression of the gas charge including the fuel.

(29) It is conceivable as a matter of principle to provide the rotary engine 2 with a spark plug and to ignite the fuel or the fuel air mix with an ignition spark when the engine piston 7 is in its upper reversal position. Alternatively it is also conceivable to operate the rotary engine 2 with diesel fuel and to cause an ignition of the fuel solely by the temperature and the pressure in the combustion chamber.

(30) In the art there is a particular problem with engines in being able to open and close valves of the respective cylinders reliably and over a long service life. In the rotary engine 2 according to the invention the problem of valve control is solved by a forced control. For this purpose the rotary engine 2 includes a rise 21 on an inner enveloping surface 19 of its engine housing wherein the rise extends in a radial direction relative to the rise 21. The rise 21 is configured so that a radial distance between the engine axis 5 and a peak of the rise is less than a radial distance between the engine axis 5 and the inner enveloping surface 19 of the engine housing outside of the rise 21.

(31) In the illustrated embodiment the rise 21 extends over a partial angle range 20 of a complete revolution, this means 360 of the engine housing. The rise 21 is thus configured continuous so that there is no cross section leap between the inner surface 19 and the rise 21. The rise 21 is furthermore configured asymmetrical wherein a radially measured height of the rise 21 increases continuously from zero to a peak of the rise and then decreases to 0 again in the same way. Put differently the rise 21 includes an inlet portion.

(32) The configuration of the rise 21 follows the basic principle that a valve arrangement 27 that rotates in the engine housing is forced radially inward through engagement with the rise 21, this means in a direction towards the engine axis 5. This support of the valve arrangement is thus only performed due to the valve arrangement moving along the rise 21. Thus a purely mechanical control of the valve arrangement is provided.

(33) In the illustrated embodiment of the engine compressor unit 1 according to the invention which includes a rotary engine 2 according to the invention, the inner enveloping surface 19 of the engine compressor housing 22 which envelops the rotary engine and the rotary compressor 3 is provided with a support groove 35 which is configured circumferential and closed in itself at the inner enveloping surface 19 of the engine compressor housing 22. A corresponding running roller 29 is supported in the support groove 35 wherein the running roller is part of a valve arrangement 27. The valve arrangement 27 includes in addition to the running roller 29 a pin shaped shaft and a valve head 28. The valve head 28 is used directly for sealing an associated cylinder 6 of the rotary engine 2. The valve arrangements 27 can be derived in particular from FIG. 1 where they are illustrated engaging the associated engine ring 4. The illustrations according to FIGS. 6 and 7 illustrate the engine compressor housing 22 together with the valve arrangement 27 without illustrating the rotary engine 2 and the rotary compressor 3.

(34) During rotation of the rotary engine 2 the valve arrangement 27 with its running roller 29 is run along the support groove 35 wherein the running roller moves over the rise 21 once with each revolution. Thus, the valve head 28 of a valve arrangement 27 is lifted from its associated valve seat at the associated cylinder 6 once during a revolution of the rotary engine 2 and consequently the combustion chamber is flow connected with an ambient of the cylinder 6. Thus, it is possible to run gases out of the combustion chamber 26 of the cylinder 6. Advantageously an exhaust pipe 31 is arranged at an upper valve opening of each cylinder 6 of the engine ring 4 so that exhaust gases are let out in a controlled manner.

(35) Closing the valve, this means pressing the valve head 28 onto its associated valve seat is performed after moving over the rise 21 self-acting solely due to the prevailing centrifugal forces. A mechanical reset for example by a spring element is not required. Put differently the valve arrangement 27 is supported during its rotation in the engine compressor housing 22 by the centrifugal force with its running roller 29 in the support groove 35 and only when moving over the rise 21 the valve arrangement is forced radially inward in a direction of the engine axis 5 which implements the described opening mechanism.

(36) It is evident in particular form FIG. 7 that also the rotary compressor 3 is configured with a respective rise 21. Support groove 35 and the associated valve arrangement 27. Due to the offset arrangement of the piston axes 7, 11 of the rotary engine 2 and the rotary compressor 3 the rises 21 in the engine compressor housing 22 are arranged offset according to the angle offset of the piston axes 7, 11. In this embodiment the rises 21 are arranged opposite to each other relative to the transmission axis 9 in the engine compressor housing 22. The control of the valve arrangement 27 of the rotary compressor 3 facilitates releasing the gas compressed in the respective compressor chamber and thus its outflow from the gas outlet opening 24 into the supercharger tube 23.

(37) In order to let out the exhaust gases through the exhaust pipes 31 the engine compressor housing 22 includes openings 36 that are positioned accordingly and which are distributed over a circumference of the engine compressor housing 22 according to FIG. 7. The crankshaft 18 of the engine compressor unit 1 is fixated by a form locking element 37 in opposite face walls of the engine compressor housing 22 and supported torque proof. The form locking has the effect that the crank shaft 18 is fixated at the engine compressor housing 22 and does not perform a rotation about the transmission axis 9.

(38) In the illustrated embodiment of an engine compressor unit 1 the rotary compressor 3 is exclusively used for supercharging the rotary engine 2. It is appreciated that the rotary compressor 3 is not required for operating the rotary engine 2 but very, advantageous. The axial arrangement of rotary machines along a common axis has the essential advantage that it is conceivable to combine additionally rotary machines with the illustrated engine compressor unit or for example with an isolated rotary engine 2. Thus, it is for example conceivable to provide torque transfer from the illustrated engine compressor unit 1 onto another rotary compressor by gears so that the additional rotary compressor can be operated in analogy to the described rotary compressor 3. It is conceivable for example that an additional rotary compressor of this type operates as a compressor in an otherwise typical compression refrigeration machine 43. This means put differently that the engine compressor unit 1 can be used as a drive element for an air conditioner. As described supra the engine compressor unit can be used to drive a generator unit 42.

(39) In a combination of plural rotary machines on a common axis it can be particularly advantageous when a torque transferring engagement of the respective rotary engine or of plural rotary engines that are coupled with each other and the associated rotary compressor is configured optionally activatable and deactivatable. This can be performed for example by a clutch so that a user of the respective engine compressor unit can activate or deactivate one or plural rotary compressors at will. It is also conceivable to provide plural rotary engines wherein one or plural additional rotary engines are switched on in addition to the first rotary engine as a function of power requirement.

(40) The features presented in the instant embodiment of the rotary engine 2 and of the entire engine compressor unit 1 can be implemented independently from the other features of a respective rotary engine or an engine compressor unit at the discretion of a person skilled in the art. Put differently the individual variants that are combined with one another in the illustrated embodiment do not depend from each other.

REFERENCE NUMERALS AND DESIGNATIONS

(41) 1 engine compressor unit 2 rotary engine 3 rotary compressor 4 engine ring 5 engine axis 6 cylinder 7 engine piston 8 connecting rod 9 transmission axis 10 transmission arrangement 11 piston axis 12 compressor ring 13 compressor axis 14 cylinder 15 compressor piston 16 connecting rod 17 piston axis 18 crank shaft 19 inner enveloping surface 20 partial angle range 21 rise 22 engine compressor housing 23 supercharger tube 24 gas outlet opening 25 gas inlet opening 26 combustion chamber 27 valve arrangement 28 valve head 29 running roller 30 piston link 31 exhaust pipe 32 master connecting rod 33 pin 34 connecting rod disc 35 support groove 36 opening 37 form locking element 38 roller bearing 39 circular path 40 circular path 41 eccentricity 42 generator unit 43 compression refrigeration machine