EP3402973B1 - Method for operating an axial piston motor, and axial piston motor - Google Patents

Method for operating an axial piston motor, and axial piston motor Download PDF

Info

Publication number
EP3402973B1
EP3402973B1 EP17703309.9A EP17703309A EP3402973B1 EP 3402973 B1 EP3402973 B1 EP 3402973B1 EP 17703309 A EP17703309 A EP 17703309A EP 3402973 B1 EP3402973 B1 EP 3402973B1
Authority
EP
European Patent Office
Prior art keywords
compressor
axial piston
valve
piston motor
compressor outlet
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
EP17703309.9A
Other languages
German (de)
French (fr)
Other versions
EP3402973A1 (en
Inventor
Ulrich Rohs
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
GETAS Gesellschaft fuer Themodynamische Antriebssysteme mbH
Original Assignee
GETAS Gesellschaft fuer Themodynamische Antriebssysteme mbH
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by GETAS Gesellschaft fuer Themodynamische Antriebssysteme mbH filed Critical GETAS Gesellschaft fuer Themodynamische Antriebssysteme mbH
Publication of EP3402973A1 publication Critical patent/EP3402973A1/en
Application granted granted Critical
Publication of EP3402973B1 publication Critical patent/EP3402973B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B33/00Engines characterised by provision of pumps for charging or scavenging
    • F02B33/02Engines with reciprocating-piston pumps; Engines with crankcase pumps
    • F02B33/06Engines with reciprocating-piston pumps; Engines with crankcase pumps with reciprocating-piston pumps other than simple crankcase pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01BMACHINES OR ENGINES, IN GENERAL OR OF POSITIVE-DISPLACEMENT TYPE, e.g. STEAM ENGINES
    • F01B3/00Reciprocating-piston machines or engines with cylinder axes coaxial with, or parallel or inclined to, main shaft axis
    • F01B3/04Reciprocating-piston machines or engines with cylinder axes coaxial with, or parallel or inclined to, main shaft axis the piston motion being transmitted by curved surfaces
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B33/00Engines characterised by provision of pumps for charging or scavenging
    • F02B33/02Engines with reciprocating-piston pumps; Engines with crankcase pumps
    • F02B33/28Component parts, details or accessories of crankcase pumps, not provided for in, or of interest apart from, subgroups F02B33/02 - F02B33/26
    • F02B33/30Control of inlet or outlet ports
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00Other engines
    • F02B75/26Engines with cylinder axes coaxial with, or parallel or inclined to, main-shaft axis; Engines with cylinder axes arranged substantially tangentially to a circle centred on main-shaft axis
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00Other engines
    • F02B75/28Engines with two or more pistons reciprocating within same cylinder or within essentially coaxial cylinders
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00Other engines
    • F02B75/28Engines with two or more pistons reciprocating within same cylinder or within essentially coaxial cylinders
    • F02B75/282Engines with two or more pistons reciprocating within same cylinder or within essentially coaxial cylinders the pistons having equal strokes

Definitions

  • the invention relates to a method for operating an axial piston motor, in which fuel and compressed fuel burned continuously to working fluid in a combustion chamber and successively working cylinders is fed, in which working piston back and forth, which in turn drive an output and compressor pistons, which in compressor cylinders out and run here, in which the combustion medium is compressed, wherein the fuel medium is sucked in via compressor inlet valves and the compressed fuel medium is supplied via compressor outlet valves of the compressor cylinders of the combustion chamber.
  • the invention relates to an axial piston motor with a continuous compressed combustion medium and fuel combustion medium combustion chamber, with working cylinders, which are connected by means of cyclically openable and closable weft connections with the combustion chamber and in which working piston reciprocate, with compressor cylinders, in which compressor piston out and at least one combustion medium supply line leading from compressor discharge valves of the compressor cylinders to the combustion chamber, at least one of the compressor discharge valves having a closure member opening away from the compressor cylinder and cooperating with a valvetrain.
  • Such operating methods or axial piston motors are for example from the EP 1 035 310 A2 or from the WO 2011/00943 A2 known.
  • the outlet valve remains closed as long as the pressure in the compressor piston is below the pressure in the pressure chamber or under the pressure of the corresponding Brennmediumzutechnisch.
  • the closure part of the compressor outlet valve formed by the ceramic ball opens and strikes against an adjusting screw. This opens the way into the pressure chamber.
  • WO 2011/009453 A2 discloses such a passive control of the compressor outlet valve with a valve cover designed as a hemisphere, which interacts with a Ventildeckelantikfeder, so ultimately also this compressor outlet valve on the pressure difference between the compressor cylinder and Brennmediumzutechnisch is controlled, the spring force of the Ventildeckelantikfeder ultimately acts only parallel to this pressure difference.
  • the DE 602 25 683 T2 discloses a desmodromic valve control in which a valve is forcibly opened and closed.
  • the most effective possible compression in a generic method for operating an axial piston motor if this is characterized in that at least one of the compressor exhaust valves positively controlled closed and opened via a built-up in the respective compressor cylinder compressor pressure.
  • the combustion medium from the compressor cylinder is supplied to the combustion chamber, and in the compressor cylinder is sufficient to find compressor pressure, while it can be ensured via the positively controlled closure that no fuel medium flows back into the compressor cylinder, which would accordingly lead to losses.
  • the closing operation of the at least one of the compressor discharge valves is initiated before the associated compressor piston reaches its top dead center. Although compressed at this time then still compressed fuel medium from the compressor cylinder to the combustion chamber. In the vicinity of the upper Tonas but this is done only with a relatively low volume mass flow, so that by the closing compressor outlet valve due smaller valve throughput is not critical and the flow impeded only slightly.
  • the closing operation of the at least one of the compressor outlet valves is initiated at the latest 5 °, preferably at the latest 7 °, before the associated compressor piston reaches its top dead center.
  • the closure part of the compressor outlet valve has to accelerate and travel a certain distance until finally the compressor outlet valve is closed.
  • the closing process is initiated in time, it can be ensured that the corresponding compressor outlet valve is closed in good time, especially taking into account tolerances.
  • the forced or positively controlled closing after the closing operation is initiated, under certain circumstances by the moving mass of one of the compressor exhaust valves ultimately made, which in particular allows compliance with any tolerances, especially since the compressor outlet is kept closed by the pressure difference, and the associated Compressor piston has reached its top dead center.
  • the corresponding compressor outlet valve is actively pressed down to the point at which it is tightly closed or is in contact with a pressure system.
  • the at least one of the compressor outlet valves is closed when the associated compressor piston reaches its top dead center.
  • any possible backflow of combustion medium from the combustion medium supply line which - as already indicated above - can also be interrupted by a second compressor stage, can be prevented in the respective compressor cylinder.
  • a loss of compressed fuel medium can be reduced to a minimum or avoided altogether.
  • the at least one of the compressor outlet valves is released before the compression process in the respective compressor cylinder. This can happen, for example, already during the suction. In particular, this can already be done at the latest 12 °, preferably at the latest 10 °, after the associated compressor piston has reached its top dead center, since in the end the pressure difference between the fuel supply line and the compressor cylinder ensures that the corresponding compressor outlet valve remains tightly closed.
  • the at least one of the compressor outlet valves can be driven mechanically, which allows a particularly precise and structurally simple to implement drive form.
  • the at least one of the compressor outlet valves is driven in synchronism with the output of the axial piston motor, it being understood that, depending on the respective operating state, the phases between the output of the axial piston motor and the drive of the compressor outlet valve may be adapted.
  • valve train is mechanically formed, which allows a simple and precise control of the closure part.
  • valve train may have a pressure system which acts on the closure part, whereby a valve gear which acts only against the opening direction of the closure member, structurally particularly simple can be provided.
  • valve train can be released in the opening direction, that the pressure application is removed from the closure part.
  • the pressure system and the limiting system can be located on a common control module, so that displaced by shifting the control module, the pressure system or the limiting system in a corresponding position and in this way the corresponding compressor outlet valve can be controlled.
  • the pressure system and the limiting system on the control module are integrally formed with each other, which requires a structurally particularly simple design.
  • control assembly may be displaceable between a load position and a release position, wherein in the load position preferably the pressure system and in the unloading position, preferably the limiting system are each positioned so that they can interact with the closure part.
  • the pressure application device acts on the closure part in a corresponding pressing manner
  • relief position only the limiting system limits the valve travel in the opening direction.
  • a corresponding shift can for example take place in that the control module is subjected to a corresponding sliding movement.
  • a tilting or rotational movement for example, a rocker arm or the like may be provided, through which the control module between the loading position and the unloading position changes and each offers the pressure system or the limiting system the closure part for interaction.
  • the pressure system and the limiting system can also be designed identically, which can be realized in particular for example in An horrstkovn, anchors or rocker arms.
  • the pressure system, the limiting system and / or the control module are sprung.
  • the forces acting on the closure member can be minimized, so that its life is increased, which is particularly advantageous if the closure part in lightweight construction, for example, made of very light materials or hollow inside.
  • this also ensures a safe closing of the valve, regardless of unavoidable manufacturing tolerances.
  • the closure part may also have a suspension, which is effective for the pressure system, the limiting system or the control module, in order to ensure a corresponding discharge in this way.
  • a suspension can serve as a tolerance compensation if the pressure system presses on the same even when the valve is closed and rests against this.
  • the pressure system can be spaced from the closure part with the compressor outlet valve closed, in order to allow a tolerance compensation in this way. This is possible in particular if it is ensured in another way that the compressor outlet valve is reliably closed, which can be ensured, for example, by the inherent mass of the compressor outlet valve and / or the pressure difference via the compressor outlet valve or with other measures, such as by means of magnetic forces , The above-mentioned suspension can then still be used for material-relieving purposes.
  • the combustion chamber can, as is well known from the prior art, be effective in two stages and a preburner, which essentially serves to thermally treat the main part of the fuel, before this in a main combustion chamber with the combustion medium, which is usually air represents, is brought into contact. It is understood that differently configured combustion chambers can be readily used in corresponding axial piston engines.
  • the Brennmediumzutechnisch can also be constructed relatively complex.
  • the Brennmediumzutechnisch has a plurality of parallel lines, which then for example, extend separately from individual compressor cylinders to the combustion chamber.
  • the Brennmediumzutechnisch also, As already indicated above, comprise further compressor stages and thus first open into another compressor cylinder, and then to lead from the compressor outlet valve or compressor outlet valves to the combustion chamber.
  • pressure chambers may be provided as constituents of the combustion medium supply line, in which the combustion medium provided by the compressor cylinders is first collected and then fed into one or more supply lines to the combustion chamber.
  • the combustion medium supply line may also comprise one or more heat exchangers with which the combustion medium is heated prior to entry into the combustion chamber, wherein the exhaust gas from the working cylinders or its thermal energy is preferably used here, as already known from the prior art.
  • the one of the Kompressaulaulassventile a poppet valve whose valve cover is the closure member and acts on the Ventilschafft the valve gear.
  • a corresponding axial piston motor structurally simple and accurate implement.
  • a ball of a ball valve or also a corresponding hemisphere can optionally be used as the closure part, as long as a corresponding valve drive is also provided here.
  • the valve drive may in particular have a cam disk or camshaft that is synchronized with an output of the axial piston motor.
  • a corresponding synchronization structurally simple and precise realize, in which case it is particularly possible to drive the closure member mechanically or via a mechanically designed valve train.
  • an electrical, hydraulic or pneumatic signal can be generated, which can then be used in accordance with the synchronization of the valve train.
  • valve train also drives further compressor outlet valves or compressor inlet valves, which requires a correspondingly effective design or a very low structural complexity.
  • the directions of movement of the pistons in the compressor and working cylinders are aligned parallel to the output shaft and the output.
  • the combustion chamber is arranged centrally to the working cylinders, so that to each of the working cylinder an identical or very similar distance is covered and the axial piston motor works very uniformly.
  • compressor cylinder head 17 may be in the in FIGS. 3 and 4 shown axial piston motor 10 are used and has at least one Brennmediumeinlass 46 and a Brennmediumauslass 47 to compressor cylinders 40.
  • the compressed in the compressor cylinders 40 by reciprocating compressor piston 45 compressed combustion medium is collected in a manifold 48, in which the Brennmediumauslässe 47 of the individual compressor cylinder 40 open.
  • a multi-part Brennmediumzutechnisch 56 which is formed in this embodiment in three parts corresponding to a number of heat exchangers 55, through the heat exchanger 55 to a combustion chamber 20, wherein the manifold 48 is to count the Brennmediumzutechnisch 56.
  • the Brennmediumzu effet 56 may be simpler or more complex and, for example, still lead to other compressor stages or be interrupted by other compressor stages, which may also have these appropriate valves and Brennmediumeinlässe and / or -auslässe.
  • shot connections 25 each extend to working cylinders 30 which are represented by firing channels 26 which can be opened and closed periodically between the combustion chamber 20 and the respective working cylinders 30.
  • this can be realized for example by rotating around the working cylinder Burt McCullumn slide, by control piston or by coaxial with the combustion chamber 20 arranged rotary rotary valve or the like.
  • working piston 35 reciprocate, each connected via a connecting rod 51, each with a compressor piston 45, wherein the connecting rods 51 interact with a cam 52 of an output 50, which is arranged on an output shaft 53.
  • the connecting rod 51 interacts with the cam 52 of the output 50 via a connecting rod bearing 57 (see FIG. 7 ).
  • the compressor cylinder 40, compressor piston 45, working cylinder 30, working piston 35 and connecting rod 51 are arranged in a star shape coaxially around the combustion chamber 20 and the output shaft 53.
  • the axial piston motor 10 comprises a housing 16, which has a working cylinder head 15 with the shot channels 26 and lines for exhaust gas 36 and not shown in detail but well known exhaust valves to one side.
  • the housing 16 carries the compressor cylinder head 17th
  • the exhaust gas 36 is passed into the heat exchanger 55 and its thermal energy is fed into the heat exchanger 55 to the located in the Brennmediumzutechnisch 56, compressed combustion medium before it is used in the combustion chamber 20, which operates continuously, for burning fuel.
  • the schematic representation of FIGS. 3 and 4 merely indicated a single-stage combustion chamber. It is understood that here also a multi-stage combustion, in particular with a preburner for the preparation of the fuel, can be provided.
  • the Brennmediumauslass 47 provided in the compressor cylinder head 17 can be opened and closed by means of a compressor outlet valve 42.
  • the compressor outlet valve 42 designed as a poppet valve 80 comprises as valve 70 a closure part 71, which is formed by a valve cover 81 of the poppet valve 80, and an opposite 75, which is formed by the compressor cylinder head 17 itself and represents the valve seat 83 of the poppet valve 80.
  • the poppet valve 80 further includes a valve stem 82 which is guided by a valve guide 89 so that the valve 70 can be safely opened and closed. In this case, the valve guide 89 is seated in the compressor cylinder head 17th
  • valve train 60 As a valve train 60 is a control assembly 65 which is mounted on a sleeve-like control assembly guide 88 in the compressor cylinder head 17 radially displaceable relative to the output shaft 53 and is pressed by a pressure spring 87 against a cam 61, wherein the control assembly 65 carries a cam follower ball 85 which to reduce friction losses on the cam 61 runs.
  • the pressure spring 87 is supported, on the one hand, on the control assembly guide 88 and, on the other hand, on a sleeve 84 in which the control assembly 65 is fastened, so that the control assembly 65 is actuated via the cam disk 61 synchronously with the rotation of the output shaft 53, since the cam disk 61 acts on the Output shaft 53 is placed.
  • a control ball 86 is provided between the valve stem 82 and the control assembly 65 to reduce friction losses.
  • the control assembly 65 has a limiting device 73 and a pressure system 74, which are provided at different positions of the control assembly 65 seen radially with respect to the output shaft 53. Depending on the curved path of the cam disk 61, the limiting system 73 or the pressing system 74 can then be brought into an interaction position with the control ball 86 by the cam disk 61.
  • the pressing system 74 is provided so close to the valve seat 83 that the valve cover 81 is pressed against the valve seat 83 and the compressor outlet valve 42 is closed when the pressing system 74 is disposed in its interaction position with respect to the control ball 86, as this in FIG. 1 is shown.
  • valve cover 81 can open from its valve seat 83 in an opening direction 72 when the gas pressure in the compressor cylinder 40 exceeds the gas pressure in the Brennmediumauslass 47, as this in FIG. 2 is shown as an example.
  • control assembly 65 and the valve train 60 releases the valve 70 in the opening direction 72 when the limiting system 73 is arranged in its interaction position with the control ball 86.
  • the valve can then open itself controlled by the gas pressure. If, on the other hand, the pressure drive 74 of the control assembly 65 is brought into the interaction position with the control ball 86 by the valve drive 60, the valve 70 is forcibly closed.
  • the limiting device 73 and the pressure device 74 are provided on a resilient arm of the control assembly 65, so that the control assembly 65 resiliently interacts with the closure member 71 of the valve 70. This relieves on the one hand the material of the valve 70 and on the other hand serves to ensure the closing of the valve 70 a secure fit of the closure member 71 on its opposite 75, especially taking into account unavoidable manufacturing tolerances.
  • the geometries between the pressure device 74 and the valve stem 82, the control ball 86 and the valve seat 83 are coordinated such that the pressure device 74, when brought in its position of interaction to the control ball 86, with closed compressor outlet valve 42 of the Control ball 86 remains spaced so as to take into account any tolerances in this way.
  • the compressor outlet valve 42 closes ballistically, ie by its own movement and mass, when it has been accelerated by the control assembly 65 in the closing direction accordingly.
  • the pressure difference across the compressor outlet valve 42 also acts valve-closing, and the top dead center of the corresponding compressor piston 45 has been reached. It is understood that in an alternative embodiment, if necessary, the pressure system 74 may rest against the control ball 86 in its interaction position, even when the compressor outlet valve 42 is closed, when the suspension is sufficiently matched to the tolerances.
  • a magnet 90 is used with an armature 91 as a valve drive 60, which also interact with a designed as a poppet valve 80 valve 70.
  • the valve guide 89 is embedded in an aluminum support 93, which on the side of the armature 91, which faces away from the magnet 90, carries a stop 94, against which springs 92 press the armature 91. If the magnet 90 is acted upon by a current, then the armature 91 is against the spring force of the springs 92 and against the opening direction 72 pulled against the magnet 90. If the magnet 90 is turned off, the springs 92 can push the armature 91 in the opening direction 72 against the stop 94 again.
  • the region of the compressor cylinder head 17 surrounding the aluminum carrier 93 has cooling ribs 95.
  • This arrangement also makes it possible for the closure part 71 of the valve 70 to open freely in the opening direction and only conditionally due to the gas pressure difference between the compressor cylinder 40 and the fuel medium vent 47, while it can be closed via the magnet 90.
  • the shaft of the armature 91 which comes into contact with the closure part 71 of the valve 70 serves both as a limiting device 73 and as a pressure system 74, whereby the compressor outlet valve 42 or the valve 70 is forcibly closed by tightening the armature 91 against the opening direction 72 of the valve 70 can be.
  • valve stem 81 and the valve seat 83 and the shaft of the armature 91 are matched in their geometries with one another such that the contact pressure system 74 rests against the valve stem 81 even when the compressor outlet valve 42 is closed.
  • a small gap between the armature 91 and magnet 90 can remain for tolerance compensation.
  • a ballistic closing of the compressor outlet valve 42 can also be provided here by the valve shaft 81 or the shaft of the armature 91 being correspondingly shorter, so that the pressure system 74 does not bear against the valve stem 81 when the compressor outlet valve 42 is closed.
  • FIGS. 7 and 8 arrangements shown show possible embodiments of compressor inlet valves 41, which are also controlled by the cam disk 61, which acts there as a camshaft 62, however.
  • the respective compressor inlet valve 41 is actuated via an actuating lever 99.

Description

Die Erfindung betrifft ein Verfahren zum Betrieb eines Axialkolbenmotors, bei welchem Kraftstoff und komprimiertes Brennmedium kontinuierlich zu Arbeitsmedium in einer Brennkammer verbrannt und sukzessive Arbeitszylindern zugeführt wird, in welchen Arbeitskolben hin und her laufen, die wiederum einen Abtrieb und Verdichterkolben antreiben, welche in Verdichterzylindern hin und her laufen, in denen das Brennmedium komprimiert wird, wobei das Brennmedium über Verdichtereinlassventile angesaugt und das komprimierte Brennmedium über Verdichterauslassventile von den Verdichterzylindern der Brennkammer zugeführt wird. Ebenso betrifft die Erfindung einen Axialkolbenmotor mit einer kontinuierlichen komprimiertes Brennmedium und Kraftstoff zu Arbeitsmedium verbrennenden Brennkammer, mit Arbeitszylindern, welche mittels zyklisch öffnen- und schließbarer Schussverbindungen mit der Brennkammer verbunden sind und in welchen Arbeitskolben hin und her laufen, mit Verdichterzylindern, in welchen Verdichterkolben hin und her laufen, die von den Arbeitskolben angetrieben sind, und mit wenigstens einer Brennmediumzuleitung, die von Verdichterauslassventilen der Verdichterzylindern zu der Brennkammer führt, wobei wenigstens eines der Verdichterauslassventile ein sich von dem Verdichterzylinder weg öffnendes und mit einem Ventiltrieb zusammenwirkendes Verschlussteil aufweist.The invention relates to a method for operating an axial piston motor, in which fuel and compressed fuel burned continuously to working fluid in a combustion chamber and successively working cylinders is fed, in which working piston back and forth, which in turn drive an output and compressor pistons, which in compressor cylinders out and run here, in which the combustion medium is compressed, wherein the fuel medium is sucked in via compressor inlet valves and the compressed fuel medium is supplied via compressor outlet valves of the compressor cylinders of the combustion chamber. Likewise, the invention relates to an axial piston motor with a continuous compressed combustion medium and fuel combustion medium combustion chamber, with working cylinders, which are connected by means of cyclically openable and closable weft connections with the combustion chamber and in which working piston reciprocate, with compressor cylinders, in which compressor piston out and at least one combustion medium supply line leading from compressor discharge valves of the compressor cylinders to the combustion chamber, at least one of the compressor discharge valves having a closure member opening away from the compressor cylinder and cooperating with a valvetrain.

Derartige Betriebsverfahren bzw. Axialkolbenmotoren sind beispielsweise aus der EP 1 035 310 A2 bzw. aus der WO 2011/00943 A2 bekannt. Hierbei offenbart die EP 1 035 310 A2 eine Keramikkugel, die durch den in einer Druckkammer bzw. in einer Brennmediumzuleitung herrschenden Druck gegen ihren Ventilsitz gedrückt wird und als Verschlussteil eines Verdichterauslassventils dient. Auf diese Weise bleibt das Auslassventil solange verschlossen, solange der Druck im Verdichterkolben unter dem Druck in der Druckkammer bzw. unter dem Druck der entsprechenden Brennmediumzuleitung liegt. Steigt der Druck in dem Verdichterzylinder über den Druck in der Brennmediumzuleitung bzw. der Druckkammer, so öffnet das durch die Keramikkugel gebildete Verschlussteil des Verdichterauslassventils und schlägt gegen eine Stellschraube an. Hierdurch wird der Weg in die Druckkammer geöffnet. Auch die WO 2011/009453 A2 offenbart eine derartige passive Ansteuerung des Verdichterauslassventils mit einem als einer Halbkugel ausgebildeten Ventildeckel, der mit einer Ventildeckelandruckfeder wechselwirkt, sodass letztlich auch dieses Verdichterauslassventil über die Druckdifferenz zwischen Verdichterzylinder und Brennmediumzuleitung gesteuert ist, wobei die Federkraft der Ventildeckelandruckfeder letztlich lediglich parallel zu dieser Druckdifferenz wirkt.Such operating methods or axial piston motors are for example from the EP 1 035 310 A2 or from the WO 2011/00943 A2 known. This reveals the EP 1 035 310 A2 a ceramic ball, which is pressed by the pressure prevailing in a pressure chamber or in a Brennmediumzuleitung pressure against its valve seat and serves as a closure part of a compressor outlet valve. In this way, the outlet valve remains closed as long as the pressure in the compressor piston is below the pressure in the pressure chamber or under the pressure of the corresponding Brennmediumzuleitung. If the pressure in the compressor cylinder rises above the pressure in the combustion medium supply line or the pressure chamber, then the closure part of the compressor outlet valve formed by the ceramic ball opens and strikes against an adjusting screw. This opens the way into the pressure chamber. Also the WO 2011/009453 A2 discloses such a passive control of the compressor outlet valve with a valve cover designed as a hemisphere, which interacts with a Ventildeckelandruckfeder, so ultimately also this compressor outlet valve on the pressure difference between the compressor cylinder and Brennmediumzuleitung is controlled, the spring force of the Ventildeckelandruckfeder ultimately acts only parallel to this pressure difference.

Die DE 602 25 683 T2 offenbart eine desmodromische Ventilsteuerung, bei welcher ein Ventil zwangsweise geöffnet und geschlossen wird.The DE 602 25 683 T2 discloses a desmodromic valve control in which a valve is forcibly opened and closed.

Es ist Aufgabe vorliegender Erfindung, ein Verfahren zum Betrieb eines Axialkolbenmotors und einen Axialkolbenmotor bereitzustellen, bei welchen die Verdichtung möglichst effektiv erfolgt.It is an object of the present invention to provide a method for operating an axial piston motor and an axial piston motor, in which the compression takes place as effectively as possible.

Die Aufgabe der Erfindung wird durch ein Verfahren zum Betrieb eines Axialkolbenmotors und einen Axialkolbenmotor mit den Merkmalen der unabhängigen Ansprüche gelöst. Weitere, ggf. auch unabhängig hiervon, vorteilhafte Ausgestaltungen finden sich in den Unteransprüchen sowie der nachfolgenden Beschreibung.The object of the invention is achieved by a method for operating an axial piston motor and an axial piston motor having the features of the independent claims. Further, possibly also independent thereof, advantageous embodiments can be found in the subclaims and the following description.

So kann eine möglichst effektive Verdichtung bei einem gattungsgemäßen Verfahren zum Betrieb eines Axialkolbenmotor erfolgen, wenn sich dieses dadurch auszeichnet, dass wenigstens eines der Verdichterauslassventile zwangsgesteuert geschlossen und über einen sich in den jeweiligen Verdichterzylinder aufbauenden Verdichterdruck geöffnet wird. Auf diese Weise wird das Brennmedium aus dem Verdichterzylinder der Brennkammer zugeführt, sowie in dem Verdichterzylinder ausreichend Verdichterdruck zu finden ist, während über die zwangsgesteuerte Schließung sichergestellt werden kann, dass kein Brennmedium in den Verdichterzylinder zurückströmt, was dementsprechend zu Verlusten führen würde.Thus, the most effective possible compression in a generic method for operating an axial piston motor, if this is characterized in that at least one of the compressor exhaust valves positively controlled closed and opened via a built-up in the respective compressor cylinder compressor pressure. In this way, the combustion medium from the compressor cylinder is supplied to the combustion chamber, and in the compressor cylinder is sufficient to find compressor pressure, while it can be ensured via the positively controlled closure that no fuel medium flows back into the compressor cylinder, which would accordingly lead to losses.

Es versteht sich, dass eine derartige Verfahrensführung auch für eine mehrstufigen Verdichtung, bei welchem das den Verdichter verlassende Brennmedium nicht unmittelbar der Brennkammer sondern mittelbar über eine weitere Verdichtungsstufe, wie bei beispielsweise einen weiteren Verdichterzylinder, der Brennkammer zugeführt wird, geeignet ist.It goes without saying that such a process control is also suitable for a multi-stage compression in which the fuel leaving the compressor is not directly the combustion chamber but indirectly via a further compression stage, such as another compressor cylinder, the combustion chamber is supplied.

Bei dem vorstehend erläuterten Verfahren sind Verdichtung und Arbeit getrennt, sodass eine Verdichtung bei möglichst niedrigen Temperaturen erfolgen kann.In the method described above, compaction and work are separated, so that a compression can be carried out at the lowest possible temperatures.

Vorzugsweise wird der Schließvorgang des wenigstens einen der Verdichterauslassventile eingeleitet, bevor der zugehörige Verdichterkolben seinen oberen Totpunkt erreicht. Zwar strömt zu diesem Zeitpunkt dann noch verdichtetes Brennmedium aus dem Verdichterzylinder zu der Brennkammer. In der Nähe des oberen Tonpunktes erfolgt dieses jedoch nur mit einem verhältnismäßig geringen Volumenmassestrom, sodass der durch das sich schließende Verdichterauslassventil bedingt kleinere Ventildurchsatz unkritisch ist und die Strömung nur unwesentlich behindert.Preferably, the closing operation of the at least one of the compressor discharge valves is initiated before the associated compressor piston reaches its top dead center. Although compressed at this time then still compressed fuel medium from the compressor cylinder to the combustion chamber. In the vicinity of the upper Tonpunktes but this is done only with a relatively low volume mass flow, so that by the closing compressor outlet valve due smaller valve throughput is not critical and the flow impeded only slightly.

Vorzugsweise wird der Schließvorgang des wenigstens einen der Verdichterauslassventile spätesten 5°, vorzugsweise spätestens 7°, bevor der zugehörige Verdichterkolben seinen oberen Totpunkt erreicht, eingeleitet.Preferably, the closing operation of the at least one of the compressor outlet valves is initiated at the latest 5 °, preferably at the latest 7 °, before the associated compressor piston reaches its top dead center.

Hierbei ist insbesondere zu berücksichtigen, dass zum Schließen des Verdichterauslassventils das Verschlussteil des Verdichterauslassventils beschleunigt und eine gewisse Wegstrecke zurücklegen muss, bis dann letztlich das Verdichterauslassventil geschlossen ist. Indem der Schließvorgang rechtzeitig eingeleitet wird, kann sichergestellt werden, dass das entsprechende Verdichterauslassventil auch rechtzeitig, insbesondere auch unter Berücksichtigung von Toleranzen, geschlossen ist.It should be noted in particular that to close the compressor outlet valve, the closure part of the compressor outlet valve has to accelerate and travel a certain distance until finally the compressor outlet valve is closed. By the closing process is initiated in time, it can be ensured that the corresponding compressor outlet valve is closed in good time, especially taking into account tolerances.

Hierbei kann das zwangsweise bzw. zwangsgesteuerte Schließen, nachdem der Schließvorgang eingeleitet ist, unter Umständen durch die bewegte Masse des einen der Verdichterauslassventile letztlich erfolgen, was insbesondere ein Einhalten von etwaigen Toleranzen ermöglicht, zumal das Verdichterauslassventil durch die Druckdifferenz geschlossen gehalten wird, sowie der zugehörige Verdichterkolben seinen oberen Totpunkt erreicht hat. Insofern ist es nicht zwingend notwendig, dass das entsprechende Verdichterauslassventil bis zu dem Punkt, zu welchem es dicht geschlossen ist, aktiv angedrückt wird bzw. mit einer Andruckanlage in Kontakt steht. Insofern ist es von Vorteil, wenn wenigstens eine der Verdichterauslassventile nach dem Einleiten des Schließvorgangs frei durch seine Eigenmasse, quasi ballistisch, geschlossen wird.In this case, the forced or positively controlled closing, after the closing operation is initiated, under certain circumstances by the moving mass of one of the compressor exhaust valves ultimately made, which in particular allows compliance with any tolerances, especially since the compressor outlet is kept closed by the pressure difference, and the associated Compressor piston has reached its top dead center. In this respect, it is not absolutely necessary that the corresponding compressor outlet valve is actively pressed down to the point at which it is tightly closed or is in contact with a pressure system. In this respect, it is advantageous if at least one of the compressor outlet valves is freely closed by its own mass, virtually ballistic, after the initiation of the closing process.

Dementsprechend ist es vorteilhaft, wenn das wenigstens eine der Verdichterauslassventile geschlossen ist, wenn der zugehörige Verdichterkolben seinen oberen Totpunkt erreicht. Hierdurch kann wirkungsvoll ein etwaiges Zurückströmen an Brennmedium aus der Brennmediumzuleitung, welche - wie bereits vorstehen angedeutet ist - auch durch eine zweite Verdichterstufe unterbrochen sein kann, in den jeweiligen Verdichterzylinder unterbunden werden. Auf diese Weise kann, da unmittelbar nach dem Erreichen des oberen Totpunktes der Verdichterkolbens ansaugend wirkt, ein Verlust an komprimiertem Brennmedium auf ein Minimum reduziert bzw. gänzlich vermieden werden.Accordingly, it is advantageous if the at least one of the compressor outlet valves is closed when the associated compressor piston reaches its top dead center. As a result, any possible backflow of combustion medium from the combustion medium supply line, which - as already indicated above - can also be interrupted by a second compressor stage, can be prevented in the respective compressor cylinder. In this way, since immediately after reaching the top dead center of the compressor piston acts suction, a loss of compressed fuel medium can be reduced to a minimum or avoided altogether.

Dadurch, dass das wenigstens eine der Verdichterauslassventile über den sich in den jeweiligen Verdichterzylinder aufbauenden Verdichterdruck geöffnet wird, kann sofort, wenn ausreichend Druck in dem Verdichterzylinder vorliegt, Brennmedium zu der Brennkammer hin gefördert werden.Due to the fact that the at least one of the compressor outlet valves is opened above the compressor pressure which builds up into the respective compressor cylinder, it is possible immediately if there is sufficient pressure in the compressor cylinder, combustion medium are conveyed to the combustion chamber.

Damit ein entsprechendes, druckgesteuertes Öffnen des entsprechenden Verdichterauslassventils zuverlässig gewährleistet werden kann, ist es von Vorteil, wenn das wenigstens eine der Verdichterauslassventile vor dem Kompressionsvorgang in dem jeweiligen Verdichterzylinder freigegeben wird. Dieses kann beispielsweise schon während des Ansaugens geschehen. Insbesondere kann dieses bereits spätestens 12°, vorzugsweise spätestens 10°, nachdem der zugehörige Verdichterkolben seinen oberen Totpunkt erreicht hat, erfolgen, da letztlich dann schon die Druckdifferenz zwischen Brennmediumzuleitung und Verdichterzylinder dafür sorgt, dass das entsprechende Verdichterauslassventil dicht geschlossen bleibt.So that a corresponding, pressure-controlled opening of the corresponding compressor outlet valve can be reliably ensured, it is advantageous if the at least one of the compressor outlet valves is released before the compression process in the respective compressor cylinder. This can happen, for example, already during the suction. In particular, this can already be done at the latest 12 °, preferably at the latest 10 °, after the associated compressor piston has reached its top dead center, since in the end the pressure difference between the fuel supply line and the compressor cylinder ensures that the corresponding compressor outlet valve remains tightly closed.

Insbesondere kann das wenigstens eine der Verdichterauslassventile mechanisch angetrieben werden, was eine besonders präzise und baulich einfach umzusetzende Antriebsform ermöglicht.In particular, the at least one of the compressor outlet valves can be driven mechanically, which allows a particularly precise and structurally simple to implement drive form.

Vorzugsweise ist es, wenn das wenigstens eine der Verdichterauslassventile synchron zu dem Abtrieb des Axialkolbenmotors angetrieben wird, wobei es sich versteht, dass in Abhängigkeit von dem jeweiligen Betriebszustand ggf. die Phasen zwischen dem Abtrieb des Axialkolbenmotors und dem Antrieb des Verdichterauslassventils angepasst werden können.It is preferable if the at least one of the compressor outlet valves is driven in synchronism with the output of the axial piston motor, it being understood that, depending on the respective operating state, the phases between the output of the axial piston motor and the drive of the compressor outlet valve may be adapted.

Bei einem gattungsgemäßen Axialkolbenmotor kann eine möglichst effektive Verdichtung erfolgen, wenn sich dieser dadurch auszeichnet, dass sich das mit einem Ventiltrieb zusammenwirkende Verschlussteil gegen eine Begrenzungsanlage öffnet und der Ventiltrieb in Öffnungsrichtung freigebar ist. Dieses ermöglicht einerseits ein gezieltes Schließen des Verschlussteils, wenn dieses vorteilhaft ist und andererseits ein Öffnen des Verschlussteils, wenn in dem Verdichterzylinder ausreichend Druck herrscht.In a generic Axialkolbenmotor the most effective possible compression, if this is characterized in that the cooperating with a valve drive closure member opens against a limiting system and the valve train is free in the opening direction. This allows on the one hand a targeted closing of the closure part, if this is advantageous and on the other hand, an opening of the closure part, if sufficient pressure prevails in the compressor cylinder.

Kumulativ bzw. alternativ erfolgt eine möglichst effektive Verdichtung bei einem gattungsgemäßen Axialkolbenmotor, wenn dieser sich dadurch auszeichnet, dass sich das mit dem Ventiltrieb zusammenwirkende Verschlussteil gegen eine Begrenzungsanlage öffnet und der Ventiltrieb lediglich gegen die Öffnungsrichtung auf das Verschlussteil wirkt. Auch dieses ermöglicht einerseits ein zwangsweises Schließen des Verschlussteils, wenn dieses vorteilhaft erscheint, während sich das Verschlussteil öffnen kann, wenn in dem Verdichterzylinder ein ausreichender Druck an Brennmedium vorherrscht.Cumulatively or alternatively the most effective possible compression in a generic axial piston motor, if this is characterized in that the cooperating with the valve train closure member opens against a limiting system and the valve train acts only against the opening direction of the closure member. This, on the one hand, allows a compulsory closing of the closure part, if this appears advantageous, while the closure part can open, if a sufficient pressure on the combustion medium prevails in the compressor cylinder.

Auch bei dem gattungsgemäßen Axialkolbenmotor sind Verdichtung und Arbeit getrennt, so dass eine Verdichtung bei möglichst niedrigen Temperaturen erfolgen kann.Also in the generic axial piston engine compression and work are separated, so that compression can be carried out at the lowest possible temperatures.

Vorzugsweise ist der Ventiltrieb mechanisch ausgebildet, was eine einfache und präzise Ansteuerung des Verschlussteils ermöglicht.Preferably, the valve train is mechanically formed, which allows a simple and precise control of the closure part.

In einer konkreten Umsetzung kann der Ventiltrieb eine Andruckanlage aufweisen, die auf das Verschlussteil wirkt, wodurch ein Ventiltrieb, der lediglich gegen die Öffnungsrichtung auf das Verschlussteil wirkt, baulich besonders einfach bereitgestellt werden kann. In einer konkreten Umsetzung kann der Ventiltrieb dadurch in Öffnungsrichtung freigegeben werden, dass die Andruckanlage von dem Verschlussteil entfernt wird.In a concrete implementation of the valve train may have a pressure system which acts on the closure part, whereby a valve gear which acts only against the opening direction of the closure member, structurally particularly simple can be provided. In a concrete implementation of the valve train can be released in the opening direction, that the pressure application is removed from the closure part.

So können die Andruckanlage und die Begrenzungsanlage an einer gemeinsamen Steuerbaugruppe befindlich sein, sodass durch Verlagerung der Steuerbaugruppe die Andruckanlage bzw. die Begrenzungsanlage in eine entsprechende Position verlagert und auf diese Weise das entsprechende Verdichterauslassventil angesteuert werden können.Thus, the pressure system and the limiting system can be located on a common control module, so that displaced by shifting the control module, the pressure system or the limiting system in a corresponding position and in this way the corresponding compressor outlet valve can be controlled.

Vorzugsweise sind die Andruckanlage und die Begrenzungsanlage an der Steuerbaugruppe einstückig zueinander ausgebildet, was eine baulich besonders einfache Ausgestaltung bedingt.Preferably, the pressure system and the limiting system on the control module are integrally formed with each other, which requires a structurally particularly simple design.

Insbesondere kann die Steuerbaugruppe zwischen einer Belastungsposition und einer Entlastungsposition verlagerbar sein, wobei in der Belastungsposition vorzugsweise die Andruckanlage und in der Entlastungsposition vorzugsweise die Begrenzungsanlage jeweils derart positioniert sind, dass sie mit dem Verschlussteil wechselwirken können. Hierdurch kann gewährleistet werden, dass in der Belastungsposition die Andruckanlage entsprechend andrückend auf das Verschlussteil wirkt, während in der Entlastungsposition lediglich die Begrenzungsanlage den Ventilweg in Öffnungsrichtung begrenzt. Eine entsprechende Verlagerung kann beispielsweise dadurch erfolgen, dass die Steuerbaugruppe einer entsprechenden Schiebebewegung unterzogen wird. Ebenso kann beispielsweise eine Kipp- oder Drehbewegung, beispielsweise auch eines Kipphebels oder ähnliches, vorgesehen sein, durch welche die Steuerbaugruppe zwischen der Belastungsposition und der Entlastungsposition wechselt und jeweils die Andruckanlage bzw. die Begrenzungsanlage dem Verschlussteil zur Wechselwirkung anbietet.In particular, the control assembly may be displaceable between a load position and a release position, wherein in the load position preferably the pressure system and in the unloading position, preferably the limiting system are each positioned so that they can interact with the closure part. In this way, it can be ensured that in the loading position the pressure application device acts on the closure part in a corresponding pressing manner, while in the relief position, only the limiting system limits the valve travel in the opening direction. A corresponding shift can for example take place in that the control module is subjected to a corresponding sliding movement. Likewise, for example, a tilting or rotational movement, for example, a rocker arm or the like may be provided, through which the control module between the loading position and the unloading position changes and each offers the pressure system or the limiting system the closure part for interaction.

Ggf. können die Andruckanlage und die Begrenzungsanlage auch identisch ausgebildet sein, was insbesondere beispielsweise bei Andruckstempeln, Ankern oder Kipphebeln realisierbar ist.Possibly. The pressure system and the limiting system can also be designed identically, which can be realized in particular for example in Andruckstempeln, anchors or rocker arms.

Vorzugsweise sind die Andruckanlage, die Begrenzungsanlage und/oder die Steuerbaugruppe gefedert. Hierdurch lassen sich die auf das Verschlussteil wirkenden Kräfte minimieren, sodass dessen Lebensdauer erhöht ist, was insbesondere dann von Vorteil ist, wenn das Verschlussteil in Leichtbauweise, beispielsweise aus sehr leichtem Materialen oder innen hohl, ausgebildet ist. Insbesondere hinsichtlich der Andruckanlage kann hierdurch auch ein sicheres Schließen des Ventils gewährleistet werden, unabhängig von unvermeidbaren Fertigungstoleranzen. Alternativ bzw. kumulativ hierzu kann auch das Verschlussteil eine Federung aufweisen, welche zu der Andruckanlage, der Begrenzungsanlage bzw. zu der Steuerbaugruppe wirksam ist, um auf diese Weise eine entsprechende Entlastung zu gewährleisten. Auch kann ggf. eine Federung als Toleranzausgleich dienen, wenn die Andruckanlage auch bei geschlossenem Ventil auf dasselbe drückt und an diesem anliegt.Preferably, the pressure system, the limiting system and / or the control module are sprung. As a result, the forces acting on the closure member can be minimized, so that its life is increased, which is particularly advantageous if the closure part in lightweight construction, for example, made of very light materials or hollow inside. In particular, with regard to the pressure application system, this also ensures a safe closing of the valve, regardless of unavoidable manufacturing tolerances. Alternatively or cumulatively thereto, the closure part may also have a suspension, which is effective for the pressure system, the limiting system or the control module, in order to ensure a corresponding discharge in this way. Also, if necessary, a suspension can serve as a tolerance compensation if the pressure system presses on the same even when the valve is closed and rests against this.

Kumulativ bzw. alternativ zu einer Federung kann die Andruckanlage bei geschlossenem Verdichterauslassventil von dessen Verschlussteil beabstandet sein, um auf diese Weise einen Toleranzausgleich zu ermöglichen. Dieses ist insbesondere dann möglich, wenn auf andere Weise sichergestellt ist, dass das Verdichterauslassventil betriebssicher geschlossen ist, was beispielsweise durch die Eigenmasse des Verdichterauslassventils und/oder die Druckdifferenz über das Verdichterauslassventil oder auch mit anderen Maßnahmen, wie beispielsweise mittels magnetischer Kräfte, gewährleistet werden kann. Die vorstehend genannte Federung kann dann immer noch zu materialentlastenden Zwecken genutzt werden.Cumulatively or alternatively to a suspension, the pressure system can be spaced from the closure part with the compressor outlet valve closed, in order to allow a tolerance compensation in this way. This is possible in particular if it is ensured in another way that the compressor outlet valve is reliably closed, which can be ensured, for example, by the inherent mass of the compressor outlet valve and / or the pressure difference via the compressor outlet valve or with other measures, such as by means of magnetic forces , The above-mentioned suspension can then still be used for material-relieving purposes.

Die Brennkammer kann, wie an sich aus dem Stand der Technik bereits hinlänglich bekannt, zweistufig wirksam sein und eine Vorbrenner, welcher im Wesentlichen dazu dient, den Hauptteil des Kraftstoffs thermisch aufzubereiten, bevor dieser in einer Hauptbrennkammer mit dem Brennmedium, welches in der Regel Luft darstellt, in Kontakt gebracht wird. Es versteht sich, dass auch anders ausgestaltete Brennkammern bei entsprechenden Axialkolbenmotoren ohne weiteres zum Einsatz kommen können.The combustion chamber can, as is well known from the prior art, be effective in two stages and a preburner, which essentially serves to thermally treat the main part of the fuel, before this in a main combustion chamber with the combustion medium, which is usually air represents, is brought into contact. It is understood that differently configured combustion chambers can be readily used in corresponding axial piston engines.

Wie bereits vorstehend angedeutet, kann die Brennmediumzuleitung auch verhältnismäßig komplex aufgebaut sein. So ist es denkbar, dass die Brennmediumzuleitung mehrere parallel ausgebildete Leitungen aufweist, die dann beispielsweise separat von einzelnen Verdichterzylindern zu der Brennkammer reichen. Ebenso kann die Brennmediumzuleitung auch, wie bereits vorstehend angedeutet, weitere Verdichterstufen umfassen und mithin zunächst in einen weiteren Verdichterzylinder münden, um dann von dessen Verdichterauslassventil bzw. Verdichterauslassventilen zu der Brennkammer zu führen. Auch können nach den Verdichterzylindern Druckkammern als Bestandteile der Brennmediumzuleitung vorgesehen sein, in denen das von den Verdichterzylindern bereitgestellte Brennmedium zunächst gesammelt wird um dann in eine oder mehrere Zuleitungen zu der Brennkammer geführt zu werden. Auch kann die Brennmediumzuleitung einen oder mehrere Wärmetauscher umfassen, mit denen das Brennmedium vor Eintritt in die Brennkammer temperiert wird, wobei hier vorzugsweise, wie bereits aus dem Stand der Technik bekannt, das Abgas aus den Arbeitszylindern bzw. dessen thermische Energie genutzt wird.As already indicated above, the Brennmediumzuleitung can also be constructed relatively complex. Thus, it is conceivable that the Brennmediumzuleitung has a plurality of parallel lines, which then for example, extend separately from individual compressor cylinders to the combustion chamber. Likewise, the Brennmediumzuleitung also, As already indicated above, comprise further compressor stages and thus first open into another compressor cylinder, and then to lead from the compressor outlet valve or compressor outlet valves to the combustion chamber. Also, after the compressor cylinders, pressure chambers may be provided as constituents of the combustion medium supply line, in which the combustion medium provided by the compressor cylinders is first collected and then fed into one or more supply lines to the combustion chamber. The combustion medium supply line may also comprise one or more heat exchangers with which the combustion medium is heated prior to entry into the combustion chamber, wherein the exhaust gas from the working cylinders or its thermal energy is preferably used here, as already known from the prior art.

Vorzugsweise ist das eine der Verdichteraulassventile ein Tellerventil, dessen Ventildeckel das Verschlussteil ist und auf dessen Ventilschafft der Ventiltrieb wirkt. Auf diese Weise lässt sich ein entsprechender Axialkolbenmotor baulich einfach und präzise umsetzen. Andererseits versteht es sich, dass als Verschlussteil gegebenenfalls auch eine Kugel eines Kugelventils oder auch eine entsprechende Halbkugel zur Anwendung kommen kann, solange auch hier ein entsprechender Ventiltrieb vorgesehen ist.Preferably, the one of the Kompressaulaulassventile a poppet valve whose valve cover is the closure member and acts on the Ventilschafft the valve gear. In this way, a corresponding axial piston motor structurally simple and accurate implement. On the other hand, it goes without saying that a ball of a ball valve or also a corresponding hemisphere can optionally be used as the closure part, as long as a corresponding valve drive is also provided here.

Der Ventiltrieb kann insbesondere eine Nockenscheibe oder Nockenwelle, die mit einem Abtrieb des Axialkolbenmotors synchronisiert sind, aufweisen. Hierdurch lässt sich eine entsprechende Synchronisation baulich einfach und präzise realisieren, wobei es insbesondere dann möglich ist, das Verschlussteil mechanisch bzw. über einen mechanisch ausgebildeten Ventiltrieb anzutreiben. Andererseits versteht es sich, dass über die Nockenscheibe oder Nockenwelle auch ein elektrisches, hydraulisches oder pneumatisches Signal erzeugt werden kann, das dann entsprechend für die Synchronisation des Ventiltriebs genutzt werden kann.The valve drive may in particular have a cam disk or camshaft that is synchronized with an output of the axial piston motor. As a result, a corresponding synchronization structurally simple and precise realize, in which case it is particularly possible to drive the closure member mechanically or via a mechanically designed valve train. On the other hand, it is understood that on the cam or camshaft, an electrical, hydraulic or pneumatic signal can be generated, which can then be used in accordance with the synchronization of the valve train.

Vorzugsweise treibt der Ventiltrieb auch weitere Verdichterauslassventile bzw. Verdichtereinlassventile an, was eine entsprechend effektive Bauweise bzw. einen sehr geringen baulichen Aufwand bedingt.Preferably, the valve train also drives further compressor outlet valves or compressor inlet valves, which requires a correspondingly effective design or a very low structural complexity.

Als Axialkolbenmotor sind die die Bewegungsrichtungen der Kolben in den Verdichter- und Arbeitszylindern parallel zur Abtriebswelle bzw. zum Abtrieb ausgerichtet. Vorzugsweise ist die Brennkammer zentral zu den Arbeitszylindern angeordnet, so dass zu jedem dem Arbeitszylinder eine identische bzw. sehr ähnliche Wegstrecke zurückzulegen ist und der Axialkolbenmotor sehr gleichförmig arbeitet.As Axialkolbenmotor the directions of movement of the pistons in the compressor and working cylinders are aligned parallel to the output shaft and the output. Preferably, the combustion chamber is arranged centrally to the working cylinders, so that to each of the working cylinder an identical or very similar distance is covered and the axial piston motor works very uniformly.

Es versteht sich, dass die Merkmale der vorstehend bzw. in den Ansprüchen beschriebenen Lösungen gegebenenfalls auch kombiniert werden können, um die Vorteile entsprechend kumuliert umsetzen zu können.It is understood that the features of the solutions described above or in the claims can optionally also be combined in order to implement the advantages in a cumulative manner.

Weitere Vorteile, Ziele und Eigenschaften vorliegender Erfindung werden anhand nachfolgender Beschreibung von Ausführungsbeispielen erläutert, die insbesondere auch in anliegender Zeichnung dargestellt sind. In der Zeichnung zeigen:

Figur 1
einen schematischen Schnitt durch einen Verdichterzylinderkopf eines Axialkolbenmotors bei geschlossenem Verdichterauslassventil;
Figur 2
die Anordnung nach Figur 1 bei geöffnetem Verdichterauslassventil;
Figur 3
einen schematischen Querschnitt durch einen Axialkolbenmotor bei welchem der Verdichterzylinderkopf nach Figuren 1 und 2 zur Anwendung kommen kann;
Figur 4
einen schematischen Schnitt durch die Brennkammer und die Arbeitszylinder des Axialkolbenmotors nach Figur 3;
Figur 5
eine schematische Detaildarstellung eines weiteren Verdichterzylinderkopfs, der bei der Anordnung nach Figuren 3 und 4 zur Anwendung kommen kann, bei geschlossenem Verdichterauslassventil;
Figur 6
die Anordnung nach Figur 5 bei geöffnetem Verdichterauslassventil;
Figur 7
einen weiteren Verdichterzylinderkof, der bei dem Axialkolbenmotor nach Figuren 3 und 4 zur Anwendung kommen kann, im schematischen Schnitt; und
Figur 8
einen weiteren Verdichterzylinderkopf, der bei dem Axialkolbenmotor nach Figuren 3 und 4 zur Anwendung kommen kann, im schematischen Schnitt.
Further advantages, objects and features of the present invention will be explained with reference to the following description of exemplary embodiments, which are shown in particular in the appended drawing. In the drawing show:
FIG. 1
a schematic section through a compressor cylinder head of an axial piston motor with the compressor discharge valve closed;
FIG. 2
the arrangement after FIG. 1 with the compressor outlet valve open;
FIG. 3
a schematic cross section through an axial piston in which the compressor cylinder head after Figures 1 and 2 can be used;
FIG. 4
a schematic section through the combustion chamber and the working cylinder of the axial piston motor after FIG. 3 ;
FIG. 5
a schematic detail of another compressor cylinder head, which in the arrangement according to FIGS. 3 and 4 can be used when the compressor outlet valve is closed;
FIG. 6
the arrangement after FIG. 5 with the compressor outlet valve open;
FIG. 7
another compressor cylinder kof, which in the axial piston motor to FIGS. 3 and 4 can be used, in schematic section; and
FIG. 8
another compressor cylinder head, which in the axial piston motor to FIGS. 3 and 4 can be used, in schematic section.

Der in den Figuren 1 und 2 dargestellte Verdichterzylinderkopf 17 kann bei dem in Figuren 3 und 4 dargestellten Axialkolbenmotor 10 zur Anwendung kommen und weist zumindest einen Brennmediumeinlass 46 und einen Brennmediumauslass 47 zu Verdichterzylindern 40 auf.The in the Figures 1 and 2 shown compressor cylinder head 17 may be in the in FIGS. 3 and 4 shown axial piston motor 10 are used and has at least one Brennmediumeinlass 46 and a Brennmediumauslass 47 to compressor cylinders 40.

Das in den Verdichterzylindern 40 durch hin und her laufende Verdichterkolben 45 verdichtete Brennmedium wird in einem Sammelrohr 48 gesammelt, in welches die Brennmediumauslässe 47 der einzelnen Verdichterzylinder 40 münden.The compressed in the compressor cylinders 40 by reciprocating compressor piston 45 compressed combustion medium is collected in a manifold 48, in which the Brennmediumauslässe 47 of the individual compressor cylinder 40 open.

Von dem Sammelrohr 48 reicht eine mehrteilige Brennmediumzuleitung 56, die bei diesem Ausführungsbeispiel dreiteilig entsprechend einer Zahl an Wärmetauschern 55 ausgebildet ist, durch die Wärmetauscher 55 zu einer Brennkammer 20, wobei auch das Sammelrohr 48 zu der Brennmediumzuleitung 56 zu zählen ist. In abweichenden Ausführungsformen kann die Brennmediumzuleitung 56 einfacher oder komplexer aufgebaut sein und z.B. noch zu weiteren Verdichterstufen führen bzw. von weiteren Verdichterstufen unterbrochen sein, wobei ggf. auch diese entsprechende Ventile und Brennmediumeinlässe und/oder -auslässe aufweisen können.From the collecting tube 48 reaches a multi-part Brennmediumzuleitung 56, which is formed in this embodiment in three parts corresponding to a number of heat exchangers 55, through the heat exchanger 55 to a combustion chamber 20, wherein the manifold 48 is to count the Brennmediumzuleitung 56. In deviant Embodiments, the Brennmediumzuleitung 56 may be simpler or more complex and, for example, still lead to other compressor stages or be interrupted by other compressor stages, which may also have these appropriate valves and Brennmediumeinlässe and / or -auslässe.

Von der Brennkammer 20 ausgehend reichen jeweils Schussverbindungen 25 zu Arbeitszylindern 30, die durch zwischen der Brennkammer 20 und den jeweiligen Arbeitszylindern 30 periodisch öffen- und schließbare Schusskanäle 26 dargestellt sind. Je nach konkreter Umsetzung des Ausführungsbeispiels kann dieses beispielsweise durch um die Arbeitszylinder umlaufende Burt-McCullumn-Schieber, durch Steuerkolben oder durch koaxial zur Brennkammer 20 angeordnete rotierende Drehschieber oder ähnliches realisiert sein.Starting from the combustion chamber 20, shot connections 25 each extend to working cylinders 30 which are represented by firing channels 26 which can be opened and closed periodically between the combustion chamber 20 and the respective working cylinders 30. Depending on the concrete implementation of the embodiment, this can be realized for example by rotating around the working cylinder Burt McCullumn slide, by control piston or by coaxial with the combustion chamber 20 arranged rotary rotary valve or the like.

In den Arbeitszylindern 30 laufen Arbeitskolben 35 hin und her, die jeweils über einen Pleuel 51 mit jeweils einem Verdichterkolben 45 verbunden sind, wobei die Pleuel 51 mit einer Kurvenscheibe 52 eines Abtriebs 50 wechselwirken, die auf einer Abtriebswelle 53 angeordnet ist. Der Pleuel 51 wechselwirkt mit der Kurvenscheibe 52 des Abtriebs 50 über ein Pleuellager 57 (siehe Figur 7).In the working cylinders 30 working piston 35 reciprocate, each connected via a connecting rod 51, each with a compressor piston 45, wherein the connecting rods 51 interact with a cam 52 of an output 50, which is arranged on an output shaft 53. The connecting rod 51 interacts with the cam 52 of the output 50 via a connecting rod bearing 57 (see FIG. 7 ).

Die Verdichterzylinder 40, Verdichterkolben 45, Arbeitszylinder 30, Arbeitskolben 35 und Pleuel 51 sind sternförmig koaxial um die Brennkammer 20 und die Abtriebswelle 53 angeordnet.The compressor cylinder 40, compressor piston 45, working cylinder 30, working piston 35 and connecting rod 51 are arranged in a star shape coaxially around the combustion chamber 20 and the output shaft 53.

Der Axialkolbenmotor 10 umfasst ein Gehäuse 16, welches zu einer Seite einen Arbeitszylinderkopf 15 mit den Schusskanälen 26 sowie Leitungen für Abgas 36 und nicht näher dargestellte aber an sich hinlänglich bekannte Abgasventile aufweist.The axial piston motor 10 comprises a housing 16, which has a working cylinder head 15 with the shot channels 26 and lines for exhaust gas 36 and not shown in detail but well known exhaust valves to one side.

Ebenso trägt das Gehäuse 16 den Verdichterzylinderkopf 17.Likewise, the housing 16 carries the compressor cylinder head 17th

Das Abgas 36 wird in die Wärmetauscher 55 geleitet und dessen thermische Energie in den Wärmetauscher 55 dem in der Brennmediumzuleitung 56 befindlichen, komprimierten Brennmedium zugeführt, bevor dieses in der Brennkammer 20, welche kontinuierlich arbeitet, zum Verbrennen von Kraftstoff genutzt wird. Zwar ist in der schematischen Darstellung der Figuren 3 und 4 lediglich eine einstufige Brennkammer angedeutet. Es versteht sich, dass hier auch eine mehrstufige Verbrennung, insbesondere mit einem Vorbrenner zur Aufbereitung des Kraftstoffs, vorgesehen sein kann.The exhaust gas 36 is passed into the heat exchanger 55 and its thermal energy is fed into the heat exchanger 55 to the located in the Brennmediumzuleitung 56, compressed combustion medium before it is used in the combustion chamber 20, which operates continuously, for burning fuel. Although in the schematic representation of FIGS. 3 and 4 merely indicated a single-stage combustion chamber. It is understood that here also a multi-stage combustion, in particular with a preburner for the preparation of the fuel, can be provided.

Der in dem Verdichterzylinderkopf 17 vorgesehene Brennmediumauslass 47 kann mittels eines Verdichterauslassventils 42 geöffnet und geschlossen werden.The Brennmediumauslass 47 provided in the compressor cylinder head 17 can be opened and closed by means of a compressor outlet valve 42.

Das als Tellerventil 80 ausgebildete Verdichterauslassventil 42 umfasst als Ventil 70 ein Verschlussteil 71, welches durch einen Ventildeckel 81 des Tellerventils 80 gebildet wird, sowie ein Gegenteil 75, welches durch den Verdichterzylinderkopf 17 selbst gebildet wird und den Ventilsitz 83 des Tellerventils 80 darstellt. Das Tellerventil 80 umfasst des Weiteren einen Ventilschafft 82, der von einer Ventilführung 89 geführt wird, sodass das Ventil 70 sicher geöffnet und geschlossen werden kann. Hierbei sitzt die Ventilführung 89 in dem Verdichterzylinderkopf 17.The compressor outlet valve 42 designed as a poppet valve 80 comprises as valve 70 a closure part 71, which is formed by a valve cover 81 of the poppet valve 80, and an opposite 75, which is formed by the compressor cylinder head 17 itself and represents the valve seat 83 of the poppet valve 80. The poppet valve 80 further includes a valve stem 82 which is guided by a valve guide 89 so that the valve 70 can be safely opened and closed. In this case, the valve guide 89 is seated in the compressor cylinder head 17th

Als Ventiltrieb 60 dient eine Steuerbaugruppe 65, die über eine hülsenartige Steuerbaugruppenführung 88 in dem Verdichterzylinderkopf 17 radial in Bezug zu der Abtriebswelle 53 verlagerbar gelagert ist und über eine Andruckfeder 87 gegen eine Nockenscheibe 61 gedrückt wird, wobei die Steuerbaugruppe 65 eine Nockenfolgerkugel 85 trägt, welche zur Verminderung von Reibungsverlusten auf der Nockenscheibe 61 läuft. Die Andruckfeder 87 stützt sich einerseits auf an der Steuerbaugruppenführung 88 und andererseits an einer Hülse 84 ab, in welcher die Steuerbaugruppe 65 befestigt ist, sodass die Steuerbaugruppe 65 über die Nockenscheibe 61 synchron zur Drehung der Abtriebswelle 53 angesteuert wird, da die Nockenscheibe 61 auf die Abtriebswelle 53 aufgesetzt ist.As a valve train 60 is a control assembly 65 which is mounted on a sleeve-like control assembly guide 88 in the compressor cylinder head 17 radially displaceable relative to the output shaft 53 and is pressed by a pressure spring 87 against a cam 61, wherein the control assembly 65 carries a cam follower ball 85 which to reduce friction losses on the cam 61 runs. The pressure spring 87 is supported, on the one hand, on the control assembly guide 88 and, on the other hand, on a sleeve 84 in which the control assembly 65 is fastened, so that the control assembly 65 is actuated via the cam disk 61 synchronously with the rotation of the output shaft 53, since the cam disk 61 acts on the Output shaft 53 is placed.

Zwischen dem Ventilschafft 82 und der Steuerbaugruppe 65 ist eine Steuerkugel 86 vorgesehen, um Reibungsverluste zu vermindern.Between the valve stem 82 and the control assembly 65, a control ball 86 is provided to reduce friction losses.

Die Steuerbaugruppe 65 weist eine Begrenzungsanlage 73 und eine Andruckanlage 74 auf, die radial in Bezug auf die Abtriebswelle 53 gesehen an verschiedenen Positionen der Steuerbaugruppe 65 vorgesehen sind. Durch die Nockenscheibe 61 können dann - je nach Kurvenbahn der Nockenscheibe 61 - die Begrenzungsanlage 73 oder die Andruckanlage 74 in eine Wechselwirkungsposition zu der Steuerkugel 86 gebracht werden.The control assembly 65 has a limiting device 73 and a pressure system 74, which are provided at different positions of the control assembly 65 seen radially with respect to the output shaft 53. Depending on the curved path of the cam disk 61, the limiting system 73 or the pressing system 74 can then be brought into an interaction position with the control ball 86 by the cam disk 61.

In axialer Richtung gesehen ist die Andruckanlage 74 so dicht an dem Ventilsitz 83 vorgesehen, dass der Ventildeckel 81 gegen den Ventilsitz 83 gepresst und das Verdichterauslassventil 42 geschlossen ist, wenn die Andruckanlage 74 in ihrer Wechselwirkungsposition in Bezug zu der Steuerkugel 86 angeordnet ist, wie dieses in Figur 1 dargestellt ist.Viewed in the axial direction, the pressing system 74 is provided so close to the valve seat 83 that the valve cover 81 is pressed against the valve seat 83 and the compressor outlet valve 42 is closed when the pressing system 74 is disposed in its interaction position with respect to the control ball 86, as this in FIG. 1 is shown.

Ist hingegen die Begrenzungsanlage 73 in ihrer Wechselwirkungsposition in Bezug auf die Steuerkugel 86 angeordnet, so kann sich der Ventildeckel 81 von seinem Ventilsitz 83 in eine Öffnungsrichtung 72 öffnen, wenn der Gasdruck in dem Verdichterzylinder 40 den Gasdruck im Brennmediumauslass 47 übersteigt, wie dieses in Figur 2 exemplarisch dargestellt ist.If, however, the limiting system 73 is arranged in its interaction position with respect to the control ball 86, the valve cover 81 can open from its valve seat 83 in an opening direction 72 when the gas pressure in the compressor cylinder 40 exceeds the gas pressure in the Brennmediumauslass 47, as this in FIG. 2 is shown as an example.

Insoweit gibt die Steuerbaugruppe 65 bzw. der Ventiltrieb 60 das Ventil 70 in Öffnungsrichtung 72 frei, wenn die Begrenzungsanlage 73 in ihrer Wechselwirkungsposition zu der Steuerkugel 86 angeordnet ist. Das Ventil kann dann durch den Gasdruck gesteuert sich selbst öffnen. Wird andererseits durch den Ventiltrieb 60 die Andruckanlage 74 der Steuerbaugruppe 65 in Wechselwirkungsposition zu der Steuerkugel 86 gebracht, so wird das Ventil 70 zwangsweise geschlossen.In that regard, the control assembly 65 and the valve train 60 releases the valve 70 in the opening direction 72 when the limiting system 73 is arranged in its interaction position with the control ball 86. The valve can then open itself controlled by the gas pressure. If, on the other hand, the pressure drive 74 of the control assembly 65 is brought into the interaction position with the control ball 86 by the valve drive 60, the valve 70 is forcibly closed.

Die Begrenzungsanlage 73 sowie die Andruckanlage 74 sind an einem federnden Arm der Steuerbaugruppe 65 vorgesehen, sodass die Steuerbaugruppe 65 federnd mit dem Verschlussteil 71 des Ventils 70 wechselwirkt. Dieses entlastet einerseits das Material des Ventils 70 und dient andererseits dazu, beim Schließen des Ventils 70 einen sicheren Sitz des Verschlussteils 71 an seinem Gegenteil 75 zu gewährleisten, insbesondere auch unter Berücksichtigung unvermeidbarer Fertigungstoleranzen.The limiting device 73 and the pressure device 74 are provided on a resilient arm of the control assembly 65, so that the control assembly 65 resiliently interacts with the closure member 71 of the valve 70. This relieves on the one hand the material of the valve 70 and on the other hand serves to ensure the closing of the valve 70 a secure fit of the closure member 71 on its opposite 75, especially taking into account unavoidable manufacturing tolerances.

Bei diesem Ausführungsbeispiel sind die Geometrien zwischen der Andruckanlage 74 und dem Ventilschaft 82, der Steuerkugel 86 bzw. dem Ventilsitz 83 derart aufeinander abgestimmt, dass die Andruckanlage 74, wenn sie in ihrer Wechselwirkungsposition zu der Steuerkugel 86 gebracht ist, bei geschlossenem Verdichterauslassventil 42 von der Steuerkugel 86 beabstandet verbleibt, um auf diese Weise etwaigen Toleranzen zu berücksichtigen. Das Verdichterauslassventil 42 schließt an sich ballistisch, also durch seine eigen Bewegung und Masse, wenn es entsprechend durch die Steuerbaugruppe 65 in Schließrichtung beschleunigt wurde. Im Übrigen wirkt auch die Druckdifferenz über dem Verdichterauslassventil 42 ventilschließend, sowie der obere Totpunkt des entsprechenden Verdichterkolbens 45 erreicht ist. Es versteht sich, dass in einer alternativen Ausführungsform ggf. die Andruckanlage 74 in ihrer Wechselwirkungsposition auch bei geschlossenem Verdichterauslassventil 42 an der Steuerkugel 86 anliegen kann, wenn die Federung ausreichend auf die Toleranzen abgestimmt ist.In this embodiment, the geometries between the pressure device 74 and the valve stem 82, the control ball 86 and the valve seat 83 are coordinated such that the pressure device 74, when brought in its position of interaction to the control ball 86, with closed compressor outlet valve 42 of the Control ball 86 remains spaced so as to take into account any tolerances in this way. The compressor outlet valve 42 closes ballistically, ie by its own movement and mass, when it has been accelerated by the control assembly 65 in the closing direction accordingly. Incidentally, the pressure difference across the compressor outlet valve 42 also acts valve-closing, and the top dead center of the corresponding compressor piston 45 has been reached. It is understood that in an alternative embodiment, if necessary, the pressure system 74 may rest against the control ball 86 in its interaction position, even when the compressor outlet valve 42 is closed, when the suspension is sufficiently matched to the tolerances.

Bei dem in Figuren 5 und 6 dargestellten Ausführungsbeispiel dient ein Magnet 90 mit einem Anker 91 als Ventiltrieb 60, welche ebenfalls mit einem als Tellerventil 80 ausgestalteten Ventil 70 wechselwirken.At the in FIGS. 5 and 6 illustrated embodiment, a magnet 90 is used with an armature 91 as a valve drive 60, which also interact with a designed as a poppet valve 80 valve 70.

Die Ventilführung 89 ist in einem Aluminiumträger 93 eingelassen, welcher an der Seite des Ankers 91, welche dem Magneten 90 abgewandt ist, einen Anschlag 94 trägt, gegen welchen Federn 92 den Anker 91 drücken. Wird der Magnet 90 mit einem Strom beaufschlagt, so wird der Anker 91 entgegen der Federkraft der Federn 92 und entgegen der Öffnungsrichtung 72 gegen den Magneten 90 gezogen. Wird der Magnet 90 ausgeschaltet, so können die Federn 92 den Anker 91 in Öffnungsrichtung 72 wieder gegen den Anschlag 94 drücken.The valve guide 89 is embedded in an aluminum support 93, which on the side of the armature 91, which faces away from the magnet 90, carries a stop 94, against which springs 92 press the armature 91. If the magnet 90 is acted upon by a current, then the armature 91 is against the spring force of the springs 92 and against the opening direction 72 pulled against the magnet 90. If the magnet 90 is turned off, the springs 92 can push the armature 91 in the opening direction 72 against the stop 94 again.

Im Bereich des Aluminiumträgers 93 weist der den Aluminiumträger 93 umgebenden Bereich des Verdichterzsylinderkopfs 17 Kühlrippen 95 auf.In the area of the aluminum carrier 93, the region of the compressor cylinder head 17 surrounding the aluminum carrier 93 has cooling ribs 95.

Auch diese Anordnung ermöglicht es, dass das Verschlussteil 71 des Ventils 70 in Öffnungsrichtung frei und nur durch die Gasdruckdifferenz zwischen Verdichterzlinder 40 und Brennmediumauslauss 47 bedingt öffnen kann, während es über den Magneten 90 geschlossen werden kann. Hierbei dient der mit dem Verschlussteil 71 des Ventils 70 in Kontakt kommende Schaft des Ankers 91 sowohl als Begrenzungsanlage 73 als auch als Andruckanlage 74, wobei durch Anziehen des Ankers 91 entgegen der Öffnungsrichtung 72 des Ventils 70 das Verdichterauslassventil 42 bzw. das Ventil 70 zwangsweise geschlossen werden kann.This arrangement also makes it possible for the closure part 71 of the valve 70 to open freely in the opening direction and only conditionally due to the gas pressure difference between the compressor cylinder 40 and the fuel medium vent 47, while it can be closed via the magnet 90. In this case, the shaft of the armature 91 which comes into contact with the closure part 71 of the valve 70 serves both as a limiting device 73 and as a pressure system 74, whereby the compressor outlet valve 42 or the valve 70 is forcibly closed by tightening the armature 91 against the opening direction 72 of the valve 70 can be.

Bei diesem Ausführungsbeispiel sind der Ventilschaft 81 bzw. der Ventilsitz 83 und der Schaft des Ankers 91 derart in ihren Geometrien aufeinander abgestimmt, dass die Andruckanlage 74 auch bei geschlossenem Verdichterauslassventil 42 an dme Ventilschaft 81 anliegt. Hier kann zum Toleranzausgleich ein kleiner Spalt zwischen Anker 91 und Magnet 90 verbleiben. Alternativ kann auch hier ein ballistisches Schließen des Verdichterauslassventils 42 vorgesehen sein, indem der Ventilschaft 81 bzw. der Schaft des Ankers 91 entsprechend kürzer ausgebildet werden, so dass die Andruckanlage 74 bei geschlossenem Verdichterauslassventil 42 nicht an dem Ventilschaft 81 anliegt.In this embodiment, the valve stem 81 and the valve seat 83 and the shaft of the armature 91 are matched in their geometries with one another such that the contact pressure system 74 rests against the valve stem 81 even when the compressor outlet valve 42 is closed. Here, a small gap between the armature 91 and magnet 90 can remain for tolerance compensation. Alternatively, a ballistic closing of the compressor outlet valve 42 can also be provided here by the valve shaft 81 or the shaft of the armature 91 being correspondingly shorter, so that the pressure system 74 does not bear against the valve stem 81 when the compressor outlet valve 42 is closed.

Die in den Figuren 7 und 8 dargestellten Anordnungen zeigen mögliche Ausgestaltungen von Verdichtereinlassventilen 41, die ebenfalls über die Nockenscheibe 61, die dort jedoch als Nockenwelle 62 wirkt, angesteuert sind. Hierbei wird das jeweilige Verdichtereinlassventil 41 über einen Betätigungshebel 99 angesteuert. Bezugszeichenliste: 10 Axialkolbenmotor 60 Ventiltrieb 15 Arbeitszylinderkopf 61 Nockenscheibe 16 Gehäuse 62 Nockenwelle 17 Verdichterzylinderkopf 65 Steuerbaugruppe 20 Brennkammer 70 Ventil 25 Schussverbindung (exemplarisch beziffert) 71 Verschlussteil 72 Öffnungsrichtung 26 Schusskanal (exemplarisch beziffert) 73 Begrenzungsanlage 74 Andruckanlage 30 Arbeitszylinder (exemplarisch beziffert) 75 Gegenteil 35 Arbeitskolben 80 Tellerventil 36 Abgas 81 Ventildeckel 82 Ventilschaft 40 Verdichterzylinder 83 Ventilsitz 41 Verdichtereinlassventil 84 Hülse 42 Verdichterauslassventil 85 Nockenfolgerkugel 45 Verdichterkolben 86 Steuerkugel 46 Brennmediumeinlass 87 Andruckfeder 47 Brennmediumauslass 88 Steuerbaugruppenführung 48 Sammelrohr 89 Ventilführung 50 Abtrieb 90 Magnet 51 Pleuel 91 Anker 52 Kurvenscheibe 92 Feder 53 Abtriebswelle 93 Aluminiumträger 55 Wärmetauscher 94 Anschlag 56 Brennmediumzuleitung 95 Kühlrippen 57 Pleuellager 99 Betätigungshebel The in the FIGS. 7 and 8 arrangements shown show possible embodiments of compressor inlet valves 41, which are also controlled by the cam disk 61, which acts there as a camshaft 62, however. In this case, the respective compressor inlet valve 41 is actuated via an actuating lever 99. LIST OF REFERENCE NUMBERS 10 axial piston motor 60 valve train 15 Cylinder head 61 cam 16 casing 62 camshaft 17 Compressor cylinder head 65 control module 20 combustion chamber 70 Valve 25 Shot connection (numbered as an example) 71 closing part 72 opening direction 26 Shot channel (numbered as an example) 73 limiting investment 74 Andruckanlage 30 Working cylinder (numbered as an example) 75 opposite 35 working piston 80 poppet valve 36 exhaust 81 valve cover 82 valve stem 40 compression cylinder 83 valve seat 41 Compressor inlet valve 84 shell 42 Verdichterauslassventil 85 Cam follower ball 45 pistons compressor 86 trackball 46 Burning medium inlet 87 pressure spring 47 Brennmediumauslass 88 Control assembly guide 48 manifold 89 valve guide 50 output 90 magnet 51 pleuel 91 anchor 52 cam 92 feather 53 output shaft 93 aluminum support 55 heat exchangers 94 attack 56 Burning media inlet 95 cooling fins 57 connecting rod bearing 99 actuating lever

Claims (18)

  1. A method for operating an axial piston motor (10), in which fuel and compressed combustion medium are continuously burnt in a combustion chamber (20) to form working medium and successively fed to working cylinders (30) in which working pistons (35) run back and forth which in turn drive an output (50) and compressor pistons (45) which run back and forth in compressor cylinders (40) in which the combustion medium is compressed, the combustion medium being drawn in via compressor inlet valves (41), and the compressed combustion medium being fed to the combustion chamber (20) by the compressor cylinders (40) via compressor outlet valves (42), characterised in that at least one of the compressor outlet valves (42) is closed in a positively controlled manner and is opened by means of a compressor pressure building up in the respective compressor cylinder (40).
  2. The operating method according to claim 1, characterised in that the closing process of the at least one of the compressor outlet valves (42) is initiated before the associated compressor piston (45) reaches top dead centre.
  3. The operating method according to claim 2, characterised in that the closing process of the at least one of the compressor outlet valves (42) is initiated at the latest 5°, preferably at the latest 7°, before the associated compressor piston (45) reaches top dead centre.
  4. The operating method according to any one of claims 1 to 3, characterised in that the at least one of the compressor outlet valves (42) is closed when the associated compressor piston (45) reaches top dead centre.
  5. The operating method according to any one of claims 1 to 4, characterised in that the at least one of the compressor outlet valves (42) is closed freely by its own weight after initiation of the closing process.
  6. The operating method according to any one of claims 1 to 5, characterised in that the at least one of the compressor outlet valves (42) is released before the compression process.
  7. The operating method according to any one of claims 1 to 6, characterised in that the at least one of the compressor outlet valves (42) is driven mechanically.
  8. The operating method according to any one of claims 1 to 7, characterised in that the at least one of the compressor outlet valves (42) is driven synchronously with an output (50) of the axial piston motor (10).
  9. An axial piston motor (10) having: a combustion chamber (20), which continuously burns compressed combustion medium and fuel to form working medium; working cylinders (30), which are connected to the combustion chamber (20) by means of cyclically openable and closable firing connections (25) and in which working pistons (35) run back and forth; compressor cylinders (40), in which compressor pistons (45) run back and forth, which are driven by the working pistons (35); and at least one combustion medium feed line (56), which leads from compressor outlet valves (42) of the compressor cylinders (40) to the combustion chamber (20), at least one of the compressor outlet valves (42) having a closure part (71) which opens away from the compressor cylinder (40), characterised in that the closure part (71), which interacts with a valve drive (60), opens against a limiting structure (73), and the valve drive (60) can be released in the opening direction (72) and/or acts on the closure part (71) only counter to the opening direction (72).
  10. The axial piston motor (10) according to claim 9, characterised in that the valve drive (60) is mechanical.
  11. The axial piston motor (10) according to claim 9 or 10, characterised in that the valve drive (60) has a pressure application structure (74) which acts on the closure part (71).
  12. The axial piston motor (10) according to claim 11, characterised in that the pressure application structure (74) is spaced from the closure part (71) of the compressor outlet valve (42) when the latter is closed.
  13. The axial piston motor (10) according to claim 11 or 12, characterised in that the pressure application structure (74) and the limiting structure (73) are situated on a control assembly (65) and are preferably formed integrally with each other.
  14. The axial piston motor (10) according to claim 13, characterised in that the control assembly (65) can be displaced between a loading position and a non-loading position.
  15. The axial piston motor (10) according to any one of claims 9 to 14, characterised in that the pressure application structure, the limiting structure and/or the control assembly are spring-loaded.
  16. The axial piston motor (10) according to any one of claims 9 to 15, characterised in that one of the compressor outlet valves (42) is a poppet valve (80), the valve cover (81) of which is the closure part (71) and on the valve stem (82) of which the valve drive (60) acts.
  17. The axial piston motor (10) according to any one of claims 9 to 16, characterised in that the valve drive (60) has a cam disc (61) or a camshaft (62), which are synchronised with an output (50) of the axial piston motor (10).
  18. The axial piston motor (10) according to any one of claims 9 to 17, characterised in that the valve drive (60) also drives further compressor outlet valves (42) and/or compressor inlet valves (41).
EP17703309.9A 2016-01-12 2017-01-09 Method for operating an axial piston motor, and axial piston motor Active EP3402973B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102016100439.1A DE102016100439A1 (en) 2016-01-12 2016-01-12 Method for operating an axial piston motor and axial piston motor
PCT/DE2017/100010 WO2017121427A1 (en) 2016-01-12 2017-01-09 Method for operating an axial piston motor, and axial piston motor

Publications (2)

Publication Number Publication Date
EP3402973A1 EP3402973A1 (en) 2018-11-21
EP3402973B1 true EP3402973B1 (en) 2019-09-11

Family

ID=57965612

Family Applications (1)

Application Number Title Priority Date Filing Date
EP17703309.9A Active EP3402973B1 (en) 2016-01-12 2017-01-09 Method for operating an axial piston motor, and axial piston motor

Country Status (7)

Country Link
US (1) US10450945B2 (en)
EP (1) EP3402973B1 (en)
JP (1) JP2019505718A (en)
KR (1) KR20180100628A (en)
CN (1) CN108463618A (en)
DE (2) DE102016100439A1 (en)
WO (1) WO2017121427A1 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2019149297A1 (en) * 2018-01-31 2019-08-08 GETAS GESELLSCHAFT FüR THERMODYNAMISCHE ANTRIEBSSYSTEME MBH Axial piston motor
US10598089B1 (en) 2018-11-07 2020-03-24 Hts Llc Opposed piston engine with parallel combustion chambers
US11128197B2 (en) * 2019-09-20 2021-09-21 Hts Llc Linear electric device having reciprocating movement linked to rotational movement of a shaped cam

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US972504A (en) * 1908-03-23 1910-10-11 Walter F Brown Continuous-combustion heat-engine.
US3577729A (en) * 1969-03-11 1971-05-04 Glenn B Warren Reciprocating internal combustion engine with constant pressure combustion
US4133172A (en) * 1977-08-03 1979-01-09 General Motors Corporation Modified Ericsson cycle engine
DE19909689B4 (en) * 1999-03-05 2009-07-23 Rohs, Ulrich, Dr.-Ing. Piston engine with continuous combustion
WO2001016470A1 (en) 1999-08-31 2001-03-08 Richard Patton Internal combustion engine with regenerator and hot air ignition
ES2301630T3 (en) * 2001-05-10 2008-07-01 Philippe Schmidt COMMAND DEVICE OF THE KINEMATICS OF VALVES.
EP1499797A4 (en) * 2002-04-30 2005-05-18 Thomas Engine Co Llc Single-ended barrel engine with double-ended, double roller pistons
DE10360920B3 (en) * 2003-12-23 2005-09-22 Meta Motoren- Und Energie-Technik Gmbh reciprocating
MX2009008009A (en) * 2007-02-27 2009-08-07 Scuderi Group Llc Split-cycle engine with water injection.
US9879635B2 (en) 2007-11-12 2018-01-30 GETAS GESELLSCHAFT FüR THERMODYNAMISCHE ANTRIEBSSYSTEME MBH Axial piston engine and method for operating an axial piston engine
FR2947590B1 (en) 2009-07-02 2011-07-15 Snecma PROPELLER HUB
WO2011009453A2 (en) 2009-07-24 2011-01-27 GETAS GESELLSCHAFT FüR THERMODYNAMISCHE ANTRIEBSSYSTEME MBH Axial-piston motor, method for operating an axial piston motor, and method for producing a heat exchanger of an axial-piston motor
DE102011018846A1 (en) 2011-01-19 2012-07-19 GETAS GESELLSCHAFT FüR THERMODYNAMISCHE ANTRIEBSSYSTEME MBH Axial piston motor and method for operating an axial piston motor

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
None *

Also Published As

Publication number Publication date
DE112017000339A5 (en) 2018-09-20
US20190017432A1 (en) 2019-01-17
DE102016100439A1 (en) 2017-07-13
JP2019505718A (en) 2019-02-28
CN108463618A (en) 2018-08-28
US10450945B2 (en) 2019-10-22
WO2017121427A1 (en) 2017-07-20
KR20180100628A (en) 2018-09-11
EP3402973A1 (en) 2018-11-21

Similar Documents

Publication Publication Date Title
EP3402973B1 (en) Method for operating an axial piston motor, and axial piston motor
DE19544473C2 (en) Mechanical-hydraulic control for a gas exchange valve of an internal combustion engine
DE3318136A1 (en) CHARGING DEVICE FOR CHARGING COMBUSTION ENGINES
EP0093732A1 (en) Device in a pressure system.
DE2610508C2 (en)
DE102004004692A1 (en) Valve controlled expansion machine
EP2480761B1 (en) Gas expansion motor
DE102016119889A1 (en) Axial piston motor and method for operating an axial piston motor
DE102011116295A1 (en) Steam engine, has intake valve opening toward vapor chamber, and exhaust valve opening toward working chamber if difference in ambient pressure between working chamber and holes located below piston is very low
AT521166B1 (en) Free piston engine
EP3452704B1 (en) Two stroke engine
EP3918186A2 (en) Method for introducing highly precompressed combustion air into a combustion chamber of an internal combustion engine, high-pressure inlet valve therefor and internal combustion engine having such a high-pressure inlet valve
EP3359778B1 (en) Axial piston motor and method for operating an axial piston motor
DE19835403C2 (en) Method and device for supporting the opening movement of a valve working against overpressure
DE102017124411A1 (en) axial piston motor
EP1818516B1 (en) Rotary valve for a piston-cylinder unit
EP4245969B1 (en) Steam motor
DE3842802A1 (en) Double-piston assembly, especially internal combustion engine
WO2019149297A1 (en) Axial piston motor
EP1978230A2 (en) Thermal energy device, in particular for using low temperature heat sources
WO2020007419A1 (en) Axial piston engine
DE102004027967B4 (en) Gas exchange valve for an internal combustion engine
DE3938849A1 (en) IC engine with variable compression ratio - has second piston mounted in cylinder head
DE141165C (en)
DE19631290A1 (en) Supercharging device for multi=cylinder internal combustion engine

Legal Events

Date Code Title Description
STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: UNKNOWN

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE INTERNATIONAL PUBLICATION HAS BEEN MADE

PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE

17P Request for examination filed

Effective date: 20180803

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

AX Request for extension of the european patent

Extension state: BA ME

REG Reference to a national code

Ref country code: DE

Ref legal event code: R079

Ref document number: 502017002286

Country of ref document: DE

Free format text: PREVIOUS MAIN CLASS: F02B0033060000

Ipc: F02B0075280000

RIC1 Information provided on ipc code assigned before grant

Ipc: F02B 33/30 20060101ALI20190208BHEP

Ipc: F02B 75/28 20060101AFI20190208BHEP

Ipc: F02B 75/26 20060101ALI20190208BHEP

Ipc: F02B 33/06 20060101ALI20190208BHEP

Ipc: F02G 3/02 20060101ALI20190208BHEP

Ipc: F01B 3/04 20060101ALI20190208BHEP

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: GRANT OF PATENT IS INTENDED

DAV Request for validation of the european patent (deleted)
DAX Request for extension of the european patent (deleted)
INTG Intention to grant announced

Effective date: 20190402

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE PATENT HAS BEEN GRANTED

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

Free format text: NOT ENGLISH

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

REG Reference to a national code

Ref country code: AT

Ref legal event code: REF

Ref document number: 1178746

Country of ref document: AT

Kind code of ref document: T

Effective date: 20190915

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 502017002286

Country of ref document: DE

Ref country code: IE

Ref legal event code: FG4D

Free format text: LANGUAGE OF EP DOCUMENT: GERMAN

REG Reference to a national code

Ref country code: DE

Ref legal event code: R082

Ref document number: 502017002286

Country of ref document: DE

Representative=s name: REUTHER, MARTIN, DIPL.-PHYS., DE

REG Reference to a national code

Ref country code: NL

Ref legal event code: MP

Effective date: 20190911

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG4D

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190911

Ref country code: FI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190911

Ref country code: BG

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20191211

Ref country code: NO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20191211

Ref country code: HR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190911

Ref country code: LT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190911

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: ES

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190911

Ref country code: AL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190911

Ref country code: GR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20191212

Ref country code: LV

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190911

Ref country code: RS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190911

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: PL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190911

Ref country code: PT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200113

Ref country code: RO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190911

Ref country code: IT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190911

Ref country code: EE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190911

Ref country code: NL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190911

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SM

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190911

Ref country code: CZ

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190911

Ref country code: IS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200224

Ref country code: SK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190911

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 502017002286

Country of ref document: DE

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

PG2D Information on lapse in contracting state deleted

Ref country code: IS

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200112

Ref country code: DK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190911

26N No opposition filed

Effective date: 20200615

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MC

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190911

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

REG Reference to a national code

Ref country code: BE

Ref legal event code: MM

Effective date: 20200131

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: FR

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20200131

Ref country code: LU

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20200109

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: BE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20200131

Ref country code: CH

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20200131

Ref country code: LI

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20200131

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20200109

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 20210127

Year of fee payment: 5

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 20210109

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GB

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20210109

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: TR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190911

Ref country code: MT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190911

Ref country code: CY

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190911

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190911

REG Reference to a national code

Ref country code: DE

Ref legal event code: R119

Ref document number: 502017002286

Country of ref document: DE

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: DE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20220802

REG Reference to a national code

Ref country code: AT

Ref legal event code: MM01

Ref document number: 1178746

Country of ref document: AT

Kind code of ref document: T

Effective date: 20220109

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: AT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20220109

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190911