EP3615798B1 - Compressor device for the delivery of compressed air to a compressed air supply system - Google Patents

Compressor device for the delivery of compressed air to a compressed air supply system Download PDF

Info

Publication number
EP3615798B1
EP3615798B1 EP18716604.6A EP18716604A EP3615798B1 EP 3615798 B1 EP3615798 B1 EP 3615798B1 EP 18716604 A EP18716604 A EP 18716604A EP 3615798 B1 EP3615798 B1 EP 3615798B1
Authority
EP
European Patent Office
Prior art keywords
bearing
connecting rod
compressor
drive shaft
rod
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
EP18716604.6A
Other languages
German (de)
French (fr)
Other versions
EP3615798A1 (en
Inventor
Detlev Eggebrecht
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.)
ZF CV Systems Hannover GmbH
Original Assignee
Wabco GmbH
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 Wabco GmbH filed Critical Wabco GmbH
Publication of EP3615798A1 publication Critical patent/EP3615798A1/en
Application granted granted Critical
Publication of EP3615798B1 publication Critical patent/EP3615798B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04BPOSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B39/00Component parts, details, or accessories, of pumps or pumping systems specially adapted for elastic fluids, not otherwise provided for in, or of interest apart from, groups F04B25/00 - F04B37/00
    • F04B39/0005Component parts, details, or accessories, of pumps or pumping systems specially adapted for elastic fluids, not otherwise provided for in, or of interest apart from, groups F04B25/00 - F04B37/00 adaptations of pistons
    • F04B39/0022Component parts, details, or accessories, of pumps or pumping systems specially adapted for elastic fluids, not otherwise provided for in, or of interest apart from, groups F04B25/00 - F04B37/00 adaptations of pistons piston rods
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04BPOSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B27/00Multi-cylinder pumps specially adapted for elastic fluids and characterised by number or arrangement of cylinders
    • F04B27/04Multi-cylinder pumps specially adapted for elastic fluids and characterised by number or arrangement of cylinders having cylinders in star- or fan-arrangement
    • F04B27/053Multi-cylinder pumps specially adapted for elastic fluids and characterised by number or arrangement of cylinders having cylinders in star- or fan-arrangement with an actuating element at the inner ends of the cylinders
    • F04B27/0536Multi-cylinder pumps specially adapted for elastic fluids and characterised by number or arrangement of cylinders having cylinders in star- or fan-arrangement with an actuating element at the inner ends of the cylinders with two or more series radial piston-cylinder units
    • F04B27/0538Multi-cylinder pumps specially adapted for elastic fluids and characterised by number or arrangement of cylinders having cylinders in star- or fan-arrangement with an actuating element at the inner ends of the cylinders with two or more series radial piston-cylinder units directly located side-by-side
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04BPOSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B27/00Multi-cylinder pumps specially adapted for elastic fluids and characterised by number or arrangement of cylinders
    • F04B27/04Multi-cylinder pumps specially adapted for elastic fluids and characterised by number or arrangement of cylinders having cylinders in star- or fan-arrangement
    • F04B27/0404Details, component parts specially adapted for such pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04BPOSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B27/00Multi-cylinder pumps specially adapted for elastic fluids and characterised by number or arrangement of cylinders
    • F04B27/04Multi-cylinder pumps specially adapted for elastic fluids and characterised by number or arrangement of cylinders having cylinders in star- or fan-arrangement
    • F04B27/0404Details, component parts specially adapted for such pumps
    • F04B27/0442Supporting and guiding means for the pistons
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04BPOSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B27/00Multi-cylinder pumps specially adapted for elastic fluids and characterised by number or arrangement of cylinders
    • F04B27/04Multi-cylinder pumps specially adapted for elastic fluids and characterised by number or arrangement of cylinders having cylinders in star- or fan-arrangement
    • F04B27/053Multi-cylinder pumps specially adapted for elastic fluids and characterised by number or arrangement of cylinders having cylinders in star- or fan-arrangement with an actuating element at the inner ends of the cylinders
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04BPOSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B39/00Component parts, details, or accessories, of pumps or pumping systems specially adapted for elastic fluids, not otherwise provided for in, or of interest apart from, groups F04B25/00 - F04B37/00
    • F04B39/0027Pulsation and noise damping means
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04BPOSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B39/00Component parts, details, or accessories, of pumps or pumping systems specially adapted for elastic fluids, not otherwise provided for in, or of interest apart from, groups F04B25/00 - F04B37/00
    • F04B39/12Casings; Cylinders; Cylinder heads; Fluid connections
    • F04B39/121Casings

Definitions

  • the invention relates to a compressor arrangement for a compressed air supply to a compressed air supply system, for operating a pneumatic system, comprising: a compressor, in particular a compressor, with at least one cylinder and at least one connecting rod in a connecting rod plane, the at least one connecting rod further having a compressor piston and at least one connecting rod bearing, a drive with an axis of rotation and a drive shaft, as well as a housing, the drive shaft being mounted in at least one drive shaft bearing and having a connecting rod end and an end remote from the connecting rod, and the drive shaft having a connecting rod receiving section arranged eccentrically to the axis of rotation of the drive at the connecting rod end.
  • the invention also relates to a compressed air supply system for operating a pneumatic system.
  • Compressors in particular compressors in compressed air supply systems in vehicles, are generally known.
  • a long service life robustness, efficiency and low-noise and low-vibration operation are important aspects.
  • crankshaft drive which allow the crankshaft drive to be adjusted to the motor shaft for the purpose of reducing the bearing play and thus the generation of noise are known.
  • DE 10 2005 009 445 B4 a compressor unit for generating compressed air in a vehicle, with a piston compressor and a motor for driving the piston compressor, the piston of which is driven by the motor via a connecting rod / crank drive arrangement via a motor shaft, characterized in that the crank drive is adjustable in the longitudinal direction of the motor shaft on the motor shaft when assembling the compressor unit.
  • a compressor arrangement of the DE 10 2004 020 104 A1 shows a double piston for a compressor, with an elongated piston carrier, which has a piston at each end, and with a connecting rod running approximately parallel to the piston carrier, which is rotatably mounted by means of a drive shaft bearing on a pin of the piston carrier and spaced therefrom by means of a connecting rod bearing an eccentric of a drive device can be mounted;
  • the drive shaft bearing and the connecting rod bearing therefore lie a distance above one another in approximately the same axial direction.
  • the piston carrier contains an intermediate space which is dimensioned to accommodate the connecting rod in a freely movable manner and in which the connecting rod is accommodated in a freely movable manner.
  • Direct mass balancing is characterized in that the piston has its center of gravity in its axis of rotation around the piston pin, a balance weight is attached to the connecting rod and the system of all oscillating parts is balanced so that the common center of gravity is in the axis of rotation of the crankshaft
  • the DE102013003513A1 describes a compressor arrangement for operating a compressed air supply system of a vehicle, comprising a compressor with an electric motor, which is formed as an electronically commutated, brushless direct current motor with a control circuit comprising power electronics and a pneumatic compressor, the electric motor being in the form of an external rotor motor.
  • the object relating to the compressor arrangement is achieved by the invention with a compressor arrangement of claim 1.
  • the object relating to the compressed air supply system is achieved by the invention with a compressed air supply system of claim 16.
  • the invention also leads to a vehicle of claim 17 with the compressor arrangement of claim 1 and / or the compressed air supply system of claim 16.
  • the invention is based on a compressor arrangement for a compressed air supply to a compressed air supply system, for operating a pneumatic system, comprising: a compressor, in particular a compressor, with at least one cylinder and at least one connecting rod in a connecting rod plane, the at least one connecting rod also having a compressor piston and at least one connecting rod bearing comprises, a drive with an axis of rotation and a drive shaft, as well as a housing, wherein the drive shaft is mounted in at least one drive shaft bearing and has a connecting rod-side end and an end remote from the connecting rod, and the drive shaft has a connecting rod receiving section arranged eccentrically to the axis of rotation of the drive at the connecting rod-side end having.
  • the at least one drive shaft bearing and the at least one connecting rod bearing are arranged in such a way that the at least one drive shaft bearing is at least partially located in the radial direction within the at least one connecting rod bearing.
  • overlap The case that the drive shaft bearing is completely in the interior of the connecting rod bearing is referred to as complete overlap.
  • the synergetic aim of the concept of the invention is to prevent negative mechanical effects such as vibrations, structure-borne noise and air-borne noise, both through the axially overlapping bearing arrangement and through the improved introduction of the connecting rod forces into the housing, as far as possible.
  • This is achieved in particular by the axial arrangement of the first bearing or A-bearing within the connecting rod bearing as well as the frame-fixed fastening of the inner ring of the A-bearing on the axle journal fixed to the frame.
  • tilting moments on the drive shaft bearings, in particular on a first bearing or A-bearing and axial forces acting on the drive shaft are reduced or avoided in an advantageous manner.
  • Low-noise and low-vibration operation is particularly important for vehicles in the passenger car sector, since here, in contrast to applications in the truck sector, the acoustic requirements are higher or more sensitive.
  • the concept preferably offers the basis for a compressor arrangement that functions in an improved manner, in particular a low-vibration and low-noise compressor arrangement.
  • these loads include, in particular, tilting moments acting on the connecting rod bearing, which occur in a conventional drive shaft bearing due to shaft bending.
  • the reduction or avoidance of such tilting moments by a bearing according to the concept of the invention leads to a better durability of the connecting rod; the connecting rod can be designed to be smaller and therefore lighter, especially in a constructive optimization.
  • the drive shaft in the compressor arrangement is mounted in the drive shaft bearing on the connecting rod end of the drive shaft in a bearing plane as the first bearing on a first bearing receiving section coaxially to the axis of rotation.
  • the development is based on the consideration that a distance in the axial direction between the bearing plane of the first bearing or A-bearing and the connecting rod plane leads to a bending moment, which in particular results in a deformation the drive shaft results.
  • a deformation can lead to possibly disadvantageous dynamic load conditions and the development of noise and vibrations.
  • Such noise and vibration developments can be further intensified by bearing play that may increase over the operating time.
  • Deformations of the drive shaft are due in particular to connecting rod forces which arise when the air is compressed by the movement of the compressor piston in the cylinder and which are passed into the drive shaft via the connecting rod bearing and / or the first bearing or A-bearing.
  • the bending moment is proportional to the connecting rod forces and the distance in the axial direction between the bearing plane and the connecting rod plane.
  • the development has recognized that when the distance in the axial direction between the bearing plane of the first bearing or A-bearing and the connecting rod plane of the connecting rod is reduced, the bending moment acting on the drive shaft is reduced.
  • a reduction can be achieved in particular if the first bearing or A-bearing is arranged in the radial direction within the connecting rod bearing.
  • a bending moment which is caused by connecting rod forces and acting on the drive shaft is completely avoided.
  • the drive shaft is mounted in the drive shaft bearing located on an end remote from the connecting rod as a second bearing on a second bearing receiving section located coaxially to the axis of rotation at the end remote from the connecting rod.
  • the bearings are arranged within the housing and / or on it.
  • the housing can comprise the compressor arrangement and / or the drive and / or further components and house them, and particularly advantageously in a modular manner means, in particular, for the compressor arrangement and drive to be designed individually but can be assembled.
  • the development is based on the idea that a reversal of the fastening arrangement of the first bearing or A-bearing, namely the stationary or frame-fixed fastening of the inner ring and a rotatable mounting of the outer ring, a transfer of the connecting rod forces into the Housing allows.
  • This is particularly the case because it is possible to fasten the first bearing or A-bearing fixed to the frame by means of an axle journal fixed to the frame at a small axial distance from the wall of the housing. Due to the small axial distance, an improved absorption of the connecting rod forces is possible, in particular without bending moments caused by connecting rod forces and particularly preferably without deforming the drive shaft or the axle journal.
  • the first bearing is firmly seated on the journal and is firmly seated in the first bearing receiving section and connects the journal and the first bearing receiving section rotatably relative to one another.
  • the bearing outer ring of the first bearing is fixed to the bearing receiving section of the Drive shaft connected. In this way, a rotational relative movement between the axle journal fixed to the frame and the drive shaft around the axis of rotation is made possible.
  • the compressor has several, in particular a first connecting rod and a second connecting rod.
  • this can mean that gas, in particular air, is compressed in two or more compression chambers.
  • a two-stage compressor is implemented by arranging two cylinders, the cylinders each having a compressor piston and a connecting rod. These are in particular driven by a drive shaft and are preferably arranged such that the overall system is in a practically balanced state.
  • a two-stage compressor leads in particular to the advantages of higher achievable efficiencies and compression pressures.
  • first connecting rod and the second connecting rod are arranged in such a way that the first connecting rod is arranged at a first bearing distance and the second connecting rod is arranged at a second bearing distance in the axial direction, ie in the direction of the axis of rotation, to the bearing plane.
  • first and the second bearing spacing can be selected depending on the structural requirements in such a way that, in particular, deformations of the drive shaft and loads on connecting rods and bearings can be minimized as far as possible.
  • one connecting rod absorbs greater forces than the other, bending moments acting on the drive shaft can be minimized by reducing the bearing spacing from the connecting rod absorbing the greater forces.
  • the setting of the bearing spacing can be used in an advantageous manner to produce a shaft bending, in particular to compensate for a deformation of the axle journal.
  • This is in the drawing in Fig. 3 shown by way of example and in connection with the Fig. 3 further explained by way of example in the context of a preferred embodiment.
  • first connecting rod and the second connecting rod are arranged in such a way that the bearing plane is centered in the axial direction between a first connecting rod plane (already here for clarification: denoted by P1 in the drawing) and a second connecting rod plane (already here for clarification: designated in the drawing with P2).
  • first and the second connecting rod planes are arranged at an axial distance of the same amount, but in the opposite direction to the bearing plane.
  • the compressor has a first connecting rod which is arranged in the bearing plane of the first bearing, the bearing distance between the connecting rod plane and the bearing plane is practically zero.
  • a two-stage compressor can also be implemented within a cylinder with a compressor piston that can be pressurized on both sides.
  • the compressor has a first connecting rod which is arranged at an axial bearing spacing from the first bearing.
  • This deformation, in particular a bend in the drive shaft can be used advantageously, for example, to compensate for a deformation of the axle journal.
  • the first connecting rod and the compressor piston are rigidly connected to one another, in particular the compressor is designed as a wobble piston compressor.
  • the connecting rod and the compressor piston are essentially constructed in one piece. This leads to the advantage that fewer moving parts have to be used to couple the drive and compressor piston and, if necessary, no guide elements are required for the piston to absorb lateral forces introduced by the connecting rod. Any gaps between the cylinder and the compressor piston resulting from the wobble kinematics are sealed in such an embodiment by means of suitable seals, in particular piston sleeve seals.
  • the compressor is designed as a single-stage compressor. Specifically, this means that the gas, in particular the air, is compressed in a compression chamber.
  • This compression chamber is formed by the interior of the cylinder and the side of the compressor piston opposite the connecting rod.
  • the compressor is designed as a multi-stage compressor, in particular a two-stage compressor. Specifically, this means that the gas, in particular the air, is compressed in two or more compression chambers.
  • a multi-stage compressor can be realized by the arrangement of several, in particular two, pistons, the pistons each having a compressor piston and a connecting rod. These are in particular driven by a drive shaft and are preferably arranged such that the overall system is in a practically balanced state.
  • the gas can be compressed in two compression chambers, for example, which are each formed by a cylinder and a compression piston that can be pressurized on both sides.
  • the side of the compressor piston opposite the connecting rod together with the interior of the cylinder located on this side of the compressor piston forms the first compression chamber.
  • the side facing the connecting rod together with the interior of the cylinder located on that side of the compressor piston also forms the second compression chamber.
  • the connecting rod bearing is formed as a roller bearing, in particular a ball bearing, needle roller bearing, cylindrical roller bearing, barrel bearing or similar roller bearing.
  • Needle and cylindrical roller bearings and generally roller bearings with cylindrical rolling elements have a generally high radial load capacity due to the line contact with the running surface.
  • ball bearings Due to the osculation in the rolling contacts, ball bearings have a relatively high axial and radial load-bearing capacity.
  • barrel bearings Due to the spherical design of the rolling elements and a spherical outer ring raceway, barrel bearings also allow a certain pendulum movement between the inner and outer ring. This makes it insensitive to misalignment and misalignment of the drive shaft with respect to the housing.
  • the first bearing and / or the second bearing is formed as a plain bearing. Specifically, this can be achieved with a lubricated or lubrication-free plain bearing. This leads in an advantageous manner to a low-maintenance, particularly preferably maintenance-free, design of the rotatable connection, since it - apart from the relative movement between shaft and bearing - has no moving parts, in particular no rolling elements.
  • the first bearing and / or the second bearing is non-positively fastened, in particular by a tolerance ring.
  • the tolerance ring can be formed by a metal spring ring, or a ring made of rubber or plastic with a suitable cross section, or a further suitable, compressible connecting element.
  • the first bearing or A-bearing and / or the second bearing or B-bearing can alternatively and / or additionally also in other ways, for example positively by a locking ring arranged in the axial direction or non-positively or frictionally by thermal Shrink, be fixed.
  • the attachment by means of a fastening element such. B.
  • a tolerance ring can refer to both the inside of the inner ring and the outside of the outer ring of the respective bearing. Consequently, for the first bearing, for example, both a tolerance ring arranged between the cavity and the outer ring of the first bearing and between a tolerance ring arranged between the axle journal and the inner ring would be possible.
  • the invention also leads to a compressed air supply system for operating a pneumatic system.
  • This compressed air supply system has: an aforementioned compressor arrangement, an air dryer and a valve arrangement.
  • the invention also leads to the solution of the object on a vehicle with a compressed air supply system and a pneumatic system, the compressed air supply system having a compressor arrangement according to the concept of the invention.
  • a compressor arrangement according to the concept of the invention is particularly advantageous in the case of cars, since high acoustic requirements prevail in the field of cars and low-noise and low-vibration operation of the compressor arrangement is of great importance or is advantageous.
  • Fig. 1 shows a compressor arrangement with a compressor 100 according to a particularly preferred embodiment of the invention.
  • a first connecting rod 140 with a first compressor piston 150 is moved up and down in an oscillating manner and practically along the axis of symmetry of the first cylinder 170.
  • the first compressor piston 150 is shown near top dead center, ie at the top end of the stroke path H. Due to the fact that the embodiment shown here is a wobble piston compressor, that is, the first connecting rod 140 and the first compressor piston 150 are rigidly connected, the oscillating movement is predominantly, but not completely, translational.
  • the first connecting rod 140 and the first compressor piston 150 therefore perform a tumbling movement corresponding to the kinematics during the upward and downward movement.
  • a second connecting rod 141 with a second compressor piston 151 is moved up and down in a second cylinder 171 in an oscillating manner and practically along the symmetry axis of the second cylinder 171 for the purpose of compressing air.
  • a multi-stage compressor can also be formed by a single-piston compressor which, by means of appropriately graduated pistons and cylinders or by a piston that can be pressurized on more than one side, forms a plurality of compression chambers.
  • the drive shaft 220 is supported in a housing 440 by means of a first, connecting-rod-side drive shaft bearing or A-bearing 360 and a second, connecting-rod-remote drive shaft bearing or B-bearing 362.
  • Both the A-bearing 360 and the B-bearing 362 can be fastened by means of a tolerance ring 164, not shown here.
  • This fastening which in particular serves as a fixed bearing seat, can relate both to the inside of the respective bearing 360, 362 and to the outside of the respective bearing 360, 362.
  • the two cylinders 170, 171 are arranged practically opposite one another with regard to the axis of rotation A.
  • these are advantageously arranged in such a way that the linear inertial forces of the system of moving masses, in particular the connecting rods, compressor pistons and sleeves, cancel each other out during the movement.
  • this canceling function of an opposing piston can be achieved by a counterweight. If the number of cylinders or pistons is greater than two, the cylinders must be similar to achieve a mass balance be arranged around the axis of rotation A, that the inertial forces balance each other out.
  • the connecting rods 140, 141 each have a connecting rod eye on their sides opposite the compressor piston 150, 151, which is used to hold a connecting rod bearing 160, 161.
  • the connecting rod bearing 160, 161 also serves to connect the connecting rod 140, 141 in a rotatable manner to a connecting rod receiving section 320 of a drive shaft 220.
  • the connecting rod receiving section 320 is integrally connected to the drive shaft 220; Nevertheless, it is just as possible for the connecting rod receiving section 320 and the drive shaft 220 to be designed in two pieces and to be joined together via a corresponding positive, non-positive or material connection.
  • the drive shaft 220 furthermore has, at an end PS on the connecting rod side, next to the outer connecting rod receiving section 320, an inner first bearing receiving section 380.
  • the outer connecting rod receiving section 320 has a cylindrical outer shape which receives the inner ring of the connecting rod bearings 160, 161.
  • the inner first bearing receiving section 330 has a cylindrical inner shape and is used to receive the first bearing or A-bearing 360.
  • Both connecting rod bearings 160, 161 and the first bearing or A-bearing 380 and the second bearing or B-bearing 382 can be attached to the drive shaft 220 in a number of ways. In particular, this fastening can take place in a form-fitting manner, for example by means of suitable fastening elements, in a force-fitting manner by shrinking on, or by a combination of the aforementioned or other operating principles.
  • the A-bearing 360 is also connected to the housing 440 via a journal 450 fixed to the frame.
  • the axle journal 450 particularly advantageously enables connecting rod forces to be introduced into the wall of the housing 440 as directly as possible, without significant bending moments or significant deformations occurring as a result of bending moments.
  • Deformations of the journal 450 that actually occur can be reduced to a negligible level by appropriate dimensioning of the journal 450, in particular by increasing the journal diameter AD and / or reducing the journal lever AH.
  • the first connecting rod bearing 160 is arranged in a first connecting rod plane P1 and the second connecting rod bearing 161 in a second connecting rod plane P2 in relation to the A-bearing 360 in such a way that the bearing plane LE of the A-bearing 360 is axially centered between the connecting rod planes P1 and P2 .
  • the connecting rod receiving section 320 is arranged eccentrically to the axis of rotation A of the drive shaft 220. This means that the axis of symmetry of the first bearing receiving section 380 lying on the axis of rotation A is arranged parallel but offset to the cylinder axis of the cylindrical connecting rod receiving section 320 lying on the eccentric axis Ex of the connecting rod bearings 160, 161.
  • the drive shaft 220 serves to transmit the rotary movement generated by a drive 200 to the connecting rods 140, 141.
  • the drive shaft 220 is driven by an electric motor 290.
  • the A-bearing 360 is arranged in the axial direction centrally between the connecting rod planes P1 and P2. In this way, bending moments acting on the drive shaft 220 are significantly reduced or avoided, since practically all connecting rod forces act essentially within the bearing plane LE and thus practically no or only a small lever arm can arise for a bending moment acting on the drive shaft 220.
  • FIG. 2A to 2C a situation with a single connecting rod bearing 260 ′ and a single drive shaft bearing 260 is shown schematically in the present case.
  • This situation also symbolizes an in Fig. 1 or Fig. 3 illustrated embodiment.
  • the axial distance with which the drive shaft bearing 260 protrudes into the connecting rod bearing interior 190 is referred to here as the overlap UD.
  • the UD overlap results from the in Figure 2A apparent embodiment, from the width BP of the connecting rod bearing 260 ', the width BA of the drive shaft bearing 260 and the axial distance SA.
  • the overlap UD is comparatively small, in particular the drive shaft bearing 260 protrudes less into the connecting rod bearing interior 190 at a distance UD that is less than half its axial width BA.
  • This case of a "simple" overlap UD can be expressed by the following relationship: UD ⁇ 0.5 * BA.
  • FIG 2B a further possible arrangement of connecting rod bearing 260 'and drive shaft bearing 260 is shown.
  • the drive shaft bearing 260 protrudes into the connecting rod bearing interior 190 as a result of an enlarged overlap UD ', the enlarged overlap UD' being greater than half the axial width BA of the drive shaft bearing 260.
  • This case of the enlarged and, in this respect, "predominant" overlap UD ' can be expressed using the following relationship: 0.5 * BA ⁇ UD ' ⁇ BA.
  • Figure 2C shows a third possible bearing arrangement in which the axial center plane EP of the connecting rod bearing 260 'and the axial center plane EA of the drive shaft bearing 260 coincide in a bearing plane E particularly advantageously.
  • the creation of bending moments is avoided in a particularly advantageous manner.
  • FIGS 3A-3D show different arrangements of A-bearings and connecting rod bearings or connecting rod bearings according to the concept of the invention.
  • Figure 3A shows a bearing arrangement according to a development in which A-bearing 360 and connecting rod bearing 160 practically exactly overlap in the axial direction.
  • the connecting rod force FP introduced from a connecting rod 140, not shown here, via the connecting rod bearing 160 to the connecting rod receiving section 320 of the drive shaft 220 is transmitted directly, in particular without bending moment, to the A-bearing 360 and thus via the journal 450 into the wall of the housing 440 becomes.
  • FIG 3B shows a bearing arrangement according to a further development of the invention.
  • the connecting rod bearing 160 is arranged on the connecting rod receiving section 320 and the A bearing 360 in the A bearing receiving section 380 in such a way that there is an offset in the axial direction between the connecting rod bearing 160 and the A bearing 360. Consequently, the connecting rod plane P of the connecting rod bearing 160 and the bearing plane LE of the A-bearing 360 lie parallel to one another in the axial direction at a bearing spacing LA.
  • a bending moment caused by the connecting rod forces which is formed from the connecting rod force FP and a lever arm with the length LA, acts on the connecting rod receiving section 320 of the drive shaft 220.
  • Such a bearing arrangement can advantageously be used to compensate for a deformation of the axle journal 450 caused by a bending moment by a deformation of the drive shaft 220 specifically caused by the bearing spacing LA.
  • the bending moment acting on the journal 450 results from the bearing force acting on the A-bearing 360 and the journal lever AH. This connection is shown below in Fig. 4 explained in more detail.
  • FIG. 3C a bearing arrangement according to a further development of the invention is shown by way of example.
  • This training is about a compressor with two cylinders 170, 171, not shown here, and correspondingly two connecting rods 140, 141, also not shown here.
  • the corresponding connecting rod bearings 160, 161 are arranged axially next to one another on the connecting rod receiving section 320.
  • the A-bearing 360 is arranged within the A-bearing receiving section 180 and on the axle journal 450 such that the bearing plane LE lies centrally in the axial direction between the connecting rod planes P1, P2.
  • the central arrangement of the A-bearing 360 in the axial direction between the connecting rod bearings 160, 161 represents a compromise for minimizing the bending moments caused by connecting rod forces FP1, FP2, since due to the arrangement of the connecting rod planes P1 and P2 outside the bearing plane LG it is not completely free of bending moments Storage of the drive shaft 220 is possible.
  • the first connecting rod bearing 160 is arranged displaced by a first bearing spacing LA1 in the negative axial direction, that is to say in the direction of the wall of the housing 440 on which the journal 450 is attached.
  • the second connecting rod bearing 161 is arranged in the positive axial direction, ie in the direction of the free end of the journal 450, by a second bearing spacing LA2, which in this case is equal to the first bearing spacing LA1 in terms of amount.
  • Figure 3D shows a bearing arrangement according to yet another development of the invention.
  • the A-bearing 360 is arranged in relation to the connecting rod bearings 160, 161 in such a way that the bearing distances LA1 and LA2 are each of different sizes.
  • connecting rods 140, 141 that are approximately equally loaded in terms of amount, this means that one of the resulting total connecting rod forces conducted into drive shaft 220 from both connecting rods 140, 141 and thus both connecting rod bearings 160, 161 does not essentially act within bearing plane E.
  • the resulting, deliberately induced deformation can, analogous to that in Figure 3B Bearing arrangement described, can be used to compensate for the deformation of the journal 450.
  • an in Figure 3D Bearing arrangement shown can be used specifically to take into account and compensate for this fact. It is assumed here, for example, that the connecting rod force FP2 acting on the second connecting rod bearing 161 is greater than the connecting rod force FP1 acting on the first connecting rod bearing 160. Consequently, the axial position of the A-bearing 360 is shifted in the direction of the more heavily loaded connecting rod bearing, in this case the connecting rod bearing 161, so that the second bearing spacing LA2 is smaller than the first bearing spacing LA1.
  • critical deformation refers to a deformation that leads directly or indirectly to one or more of the disadvantages mentioned at the beginning, in particular with regard to noise and vibration development as well as wear behavior.
  • Fig. 4 shows in a schematic representation a deflection of a drive shaft 220 and an axle journal 450.
  • a connecting rod force FP that acts on the connecting rod bearing 160 is transmitted to the drive shaft 220 and thus to the A bearing 360.
  • This force is finally conducted via the A-bearing 360 into the journal 450, where it leads to a bending moment due to the distance between the housing 440 and the A-bearing 360, which in turn results in a deformation of the journal 450, namely a pin deflection ZA .
  • the arrangement of A-bearing 360 and connecting rod bearing 160 ensures that a bending moment acts on drive shaft 220.
  • This bending moment is opposite to the bending moment acting on the stub axle.
  • This advantageously ensures that the drive shaft 220 is deformed in such a way that the forces acting on the B-bearing 362 are as small as possible, in particular transverse forces and Overturning moments act.
  • the deformation of the drive shaft 220 thus partially or completely compensates for the pin deflection ZA.
  • Fig. 5 shows a greatly simplified, schematic overview of a compressed air supply system 500 with a compressor arrangement 1000 according to the concept of the invention for supplying a pneumatic system 600.
  • the compressed air supply system 500 has an air intake 0 for sucking in fresh air, which continues to carry fluid, in particular gas, with an inlet of the compressor 100 , connected is.
  • the compressor 100 is driven by a drive 200 via a drive shaft 220.
  • the compressed fresh air is also made available via a compressed air source 1, to which a branch 510 is connected.
  • a vent 3 is connected to this junction 510 via a vent valve 520.
  • an air dryer 520 is connected to the junction 510, which also leads to a compressed air connection 2.
  • a compressed air reservoir 560 and the pneumatic system 600 are also connected to this via a gallery 570.
  • the pneumatic system 600 can, for example, be an air suspension system or another pneumatic system, in particular a vehicle.
  • individual valves, throttles and similar adjusting means as well as individual components, in particular the pneumatic system are not shown in this illustration for reasons of clarity and simplicity.
  • Fig. 6 shows a schematic representation of a vehicle 800 - in the present case in the form of a car - with a compressed air supply system 500 and a pneumatic system 600.
  • vehicle 800 in the passenger car sector, low-noise and low-vibration operation is of great importance because here, in contrast to applications in trucks -Area, the acoustic requirements are higher or more sensitive.
  • the car vehicle 800 shown here by way of example, without restricting its applicability for trucks or other commercial vehicles, has four wheels 801, 802, 803 and 804, of which the two front wheels are shown here due to the sectional view.
  • the pneumatic system 600 has four air springs 601, 602, 603 and 604, of which the two front air springs are shown here analogously to the wheels due to the sectional view.
  • the air springs 601, 602, 603 and 604, which are respectively assigned to the wheels 801, 802, 803 and 804, are supplied with compressed air from the compressed air supply system 500 as part of the pneumatic system 600.
  • the compressed air supply system 500 is connected in a fluid-conducting manner via the gallery 570 to the components of the pneumatic system 600, in this case the air springs 601, 602, 603 and 604 shown here.
  • the compressed air supply system 500 is shown greatly simplified in this illustration, so that only the compressed air reservoir 560 and the compressor 100 according to the concept of the invention are visible.
  • the compressor 100 according to the concept of the invention can, however, in a modification not shown here, additionally or alternatively be used independently of the compressed air supply system.
  • the concept preferably offers the basis for a compressor arrangement that functions in an improved manner, in particular a low-vibration and low-noise compressor arrangement. Furthermore, a reduction in forces and / or moments and, in particular, a reduction in the dynamic loads and vibrations associated with the forces and / or moments lead to a gentler mode of operation, which has a positive effect on the efficiency and longevity of the compressor arrangement.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Compressor (AREA)
  • Compressors, Vaccum Pumps And Other Relevant Systems (AREA)

Description

Die Erfindung betrifft eine Verdichteranordnung für eine Druckluftzuführung einer Druckluftversorgungsanlage, zum Betreiben einer Pneumatikanlage, aufweisend: einen Verdichter, insbesondere Kompressor, mit mindestens einem Zylinder und mindestens einem Pleuel in einer Pleuelebene, wobei das mindestens eine Pleuel weiter einen Verdichterkolben und mindestens ein Pleuellager aufweist, einen Antrieb mit einer Drehachse und einer Antriebswelle, sowie einem Gehäuse, wobei die Antriebswelle in mindestens einem Antriebswellenlager gelagert ist und ein pleuelseitiges Ende und ein pleuelfernes Ende aufweist, und die Antriebswelle einen exzentrisch zur Drehachse des Antriebs am pleuelseitigen Ende angeordneten Pleuel-Aufnahmeabschnitt aufweist.The invention relates to a compressor arrangement for a compressed air supply to a compressed air supply system, for operating a pneumatic system, comprising: a compressor, in particular a compressor, with at least one cylinder and at least one connecting rod in a connecting rod plane, the at least one connecting rod further having a compressor piston and at least one connecting rod bearing, a drive with an axis of rotation and a drive shaft, as well as a housing, the drive shaft being mounted in at least one drive shaft bearing and having a connecting rod end and an end remote from the connecting rod, and the drive shaft having a connecting rod receiving section arranged eccentrically to the axis of rotation of the drive at the connecting rod end.

Die Erfindung betrifft auch eine Druckluftversorgungsanlage zum Betreiben einer Pneumatikanlage.The invention also relates to a compressed air supply system for operating a pneumatic system.

Verdichter, insbesondere Verdichter in Druckluftversorgungsanlagen in Fahrzeugen, sind allgemein bekannt. Allgemein stellen bei der Verbesserung eines solchen Verdichters eine hohe Lebensdauer, Robustheit, Effizienz sowie ein geräusch- und vibrationsarmer Betriebs wichtige Aspekte dar.Compressors, in particular compressors in compressed air supply systems in vehicles, are generally known. In general, when improving such a compressor, a long service life, robustness, efficiency and low-noise and low-vibration operation are important aspects.

Verdichter, welche die Einstellbarkeit des Kurbeltriebs auf die Motorwelle zwecks Reduzierung des Lagerspiels und somit der Geräuschentwicklung vorsehen, sind bekannt. So beschreibt DE 10 2005 009 445 B4 ein Kompressoraggregat zur Erzeugung von Druckluft in einem Fahrzeug, mit einem Kolbenkompressor und einem Motor zum Antrieb des Kolbenkompressors, wobei dessen Kolben über eine Pleuel/Kurbeltrieb-Anordnung von dem Motor über eine Motorwelle angetrieben wird, dadurch gekennzeichnet, dass der Kurbeltrieb beim Zusammenbau des Kompressoraggregates in Längsrichtung der Motorwelle auf der Motorwelle justierbar ist.Compressors which allow the crankshaft drive to be adjusted to the motor shaft for the purpose of reducing the bearing play and thus the generation of noise are known. So describes DE 10 2005 009 445 B4 a compressor unit for generating compressed air in a vehicle, with a piston compressor and a motor for driving the piston compressor, the piston of which is driven by the motor via a connecting rod / crank drive arrangement via a motor shaft, characterized in that the crank drive is adjustable in the longitudinal direction of the motor shaft on the motor shaft when assembling the compressor unit.

Eine Verdichteranordnung der DE 10 2004 020 104 A1 zeigt einen Doppelkolben für einen Verdichter, mit einem länglichen Kolbenträger, der an jedem Ende einen Kolben aufweist, und mit einem etwa parallel zum Kolbenträger verlaufenden Pleuel, das mittels eines Antriebswellenlagers auf einem Bolzen des Kolbenträgers drehbar gelagert ist und im Abstand davon mittels eines Pleuellagers auf einem Exzenter einer Antriebseinrichtung lagerbar ist; Antriebswellenlager und Pleuellager liegen also in etwa in gleicher axialer Richtung ein Abstand übereinander. Der Kolbenträger enthält in einem mittleren Bereich, der sich zwischen beiden Kolben erstreckt, einen zur frei beweglichen Aufnahme des Pleuels bemessenen Zwischenraum, in dem das Pleuel frei beweglich aufgenommen ist.A compressor arrangement of the DE 10 2004 020 104 A1 shows a double piston for a compressor, with an elongated piston carrier, which has a piston at each end, and with a connecting rod running approximately parallel to the piston carrier, which is rotatably mounted by means of a drive shaft bearing on a pin of the piston carrier and spaced therefrom by means of a connecting rod bearing an eccentric of a drive device can be mounted; The drive shaft bearing and the connecting rod bearing therefore lie a distance above one another in approximately the same axial direction. In a central region which extends between the two pistons, the piston carrier contains an intermediate space which is dimensioned to accommodate the connecting rod in a freely movable manner and in which the connecting rod is accommodated in a freely movable manner.

Weiterhin sind Verfahren zum direkten Massenausgleich bei Kolbenmaschinen bekannt. DE 2424562 A1 beschreibt ein Verfahren des direkten Massenausgleichs. Der direkte Massenausgleich ist dadurch gekennzeichnet, dass der Kolben seinen Schwerpunkt in seiner Drehachse um den Kolbenbolzen hat, am Pleuel ein Ausgleichsgewicht angebracht wird und das System aller oszillierender Teile so ausgewuchtet wird, dass der gemeinsame Schwerpunkt sich in der Drehachse der Kurbelwelle befindetMethods for direct mass balancing in piston engines are also known. DE 2424562 A1 describes a method of direct mass balancing. Direct mass balancing is characterized in that the piston has its center of gravity in its axis of rotation around the piston pin, a balance weight is attached to the connecting rod and the system of all oscillating parts is balanced so that the common center of gravity is in the axis of rotation of the crankshaft

Die DE102013003513A1 beschreibt eine Verdichteranordnung zum Betreiben einer Druckluftversorgungsanlage eines Fahrzeugs, aufweisend einen Verdichter mit einem Elektromotor, der als ein elektronisch kommutierter, bürstenloser GleichstromMotor mit einer Ansteuerschaltung umfassend eine Leistungselektronik gebildet ist und einem pneumatischen Kompressor, wobei der Elektromotor in Form eines Außenläufer-Motors gebildet ist.The DE102013003513A1 describes a compressor arrangement for operating a compressed air supply system of a vehicle, comprising a compressor with an electric motor, which is formed as an electronically commutated, brushless direct current motor with a control circuit comprising power electronics and a pneumatic compressor, the electric motor being in the form of an external rotor motor.

Das Konzept, insbesondere die eingangs dargestellten Bauformen von Verdichteranordnungen, sind noch verbesserungswürdig, insbesondere hinsichtlich eines geräusch- und vibrationsarmen Betriebs sowie der Langlebigkeit des Verdichters.The concept, in particular the designs of compressor arrangements presented at the beginning, are in need of improvement, in particular with regard to low-noise and low-vibration operation and the longevity of the compressor.

Wünschenswert ist es daher, die Funktion einer Verdichteranordnung, insbesondere der mechanischen Kopplung von Antrieb und Verdichter, insbesondere hinsichtlich dieser Aspekte, nämlich eines geräusch- und vibrationsarmen Betriebs, zu verbessern.It is therefore desirable to improve the function of a compressor arrangement, in particular the mechanical coupling of drive and compressor, in particular with regard to these aspects, namely low-noise and low-vibration operation.

An dieser Stelle setzt die Erfindung an, deren Aufgabe es ist, in verbesserter Weise eine Anordnung, insbesondere eine Verdichteranordnung, eine Druckluftversorgungsanlage und ein Fahrzeug, anzugeben, die insbesondere die o. g. Probleme adressiert.This is where the invention comes in, the object of which is to provide an arrangement, in particular a compressor arrangement, a compressed air supply system and a vehicle, in an improved manner, which in particular the above. Problems addressed.

Die Aufgabe, betreffend die Verdichteranordnung, wird durch die Erfindung mit einer Verdichteranordnung des Anspruchs 1 gelöst. Die Aufgabe, betreffend die Druckluftversorgungsanlage, wird durch die Erfindung mit einer Druckluftversorgungsanlage des Anspruchs 16 gelöst. Die Erfindung führt auch auf ein Fahrzeug des Anspruchs 17 mit der Verdichteranordnung des Anspruchs 1 und/oder der Druckluftversorgungsanlage des Anspruchs 16.The object relating to the compressor arrangement is achieved by the invention with a compressor arrangement of claim 1. The object relating to the compressed air supply system is achieved by the invention with a compressed air supply system of claim 16. The invention also leads to a vehicle of claim 17 with the compressor arrangement of claim 1 and / or the compressed air supply system of claim 16.

Die Erfindung geht aus von einer Verdichteranordnung für eine Druckluftzuführung einer Druckluftversorgungsanlage, zum Betreiben einer Pneumatikanlage, aufweisend: einen Verdichter, insbesondere Kompressor, mit mindestens einem Zylinder und mindestens einem Pleuel in einer Pleuelebene, wobei das mindestens eine Pleuel weiter einen Verdichterkolben und mindestens ein Pleuellager aufweist, einen Antrieb mit einer Drehachse und einer Antriebswelle, sowie einem Gehäuse, wobei die Antriebswelle in mindestens einem Antriebswellenlager gelagert ist und ein pleuelseitiges Ende und ein pleuelfernes Ende aufweist, und die Antriebswelle einen exzentrisch zur Drehachse des Antriebs am pleuelseitigen Ende angeordneten Pleuel-Aufnahmeabschnitt aufweist.The invention is based on a compressor arrangement for a compressed air supply to a compressed air supply system, for operating a pneumatic system, comprising: a compressor, in particular a compressor, with at least one cylinder and at least one connecting rod in a connecting rod plane, the at least one connecting rod also having a compressor piston and at least one connecting rod bearing comprises, a drive with an axis of rotation and a drive shaft, as well as a housing, wherein the drive shaft is mounted in at least one drive shaft bearing and has a connecting rod-side end and an end remote from the connecting rod, and the drive shaft has a connecting rod receiving section arranged eccentrically to the axis of rotation of the drive at the connecting rod-side end having.

Erfindungsgemäß ist vorgesehen, dass das mindestens eine Antriebswellenlager und das mindestens eine Pleuellager derartig angeordnet sind, dass sich das mindestens eine Antriebswellenlager in radialer Richtung zumindest teilweise innerhalb des mindestens einen Pleuellagers befindet.According to the invention it is provided that the at least one drive shaft bearing and the at least one connecting rod bearing are arranged in such a way that the at least one drive shaft bearing is at least partially located in the radial direction within the at least one connecting rod bearing.

Damit ist vor allem gemeint, dass in einer Projektionsebene senkrecht zur Drehachse betrachtet - der Außendurchmesser des Antriebswellenlagers vollständig innerhalb des Innendurchmessers des Pleuellagers befindet; dies ist beispielhaft in Fig. 2A-2C dargestellt. Dies kann im Rahmen der Weiterbildung vor allem bedeuten, dass das Antriebswellenlager in axialer Richtung derartig entlang der Drehachse in Richtung des Pleuellagers oder des Antriebs --also seitlich-- verschoben ist, dass es sich hinsichtlich seiner axialen Ausdehnung ganz oder teilweise innerhalb des Pleuellager-Innenraums befindet. Insbesondere kann dies vorteilhaft auch bedeuten, dass das Antriebswellenlager derart entlang der Drehachse des Antriebs in Richtung des Pleuellagers verschoben angeordnet ist, dass es mit einem bestimmten, als Überdeckung bezeichneten, Abstand in einen Pleuellager-Innenraum des Pleuellagers hineinragt. Der Fall, dass sich das Antriebswellenlager vollständig im Pleuellager-Innenraum befindet, wird als vollständige Überdeckung bezeichnet.This primarily means that viewed in a projection plane perpendicular to the axis of rotation - the outside diameter of the drive shaft bearing is completely within the inside diameter of the connecting rod bearing; this is exemplified in Figures 2A-2C shown. In the context of the further development, this can primarily mean that the drive shaft bearing is in such a way in the axial direction is shifted along the axis of rotation in the direction of the connecting rod bearing or the drive - so laterally - that it is located wholly or partially within the interior of the connecting rod bearing with regard to its axial extent. In particular, this can advantageously also mean that the drive shaft bearing is arranged displaced along the axis of rotation of the drive in the direction of the connecting rod bearing that it protrudes into a connecting rod bearing interior of the connecting rod bearing at a certain distance, referred to as overlap. The case that the drive shaft bearing is completely in the interior of the connecting rod bearing is referred to as complete overlap.

Insbesondere bei gleichzeitiger Anordnung des Antriebswellenlagers - in radialer Richtung betrachtet - innerhalb des Pleuellagers führt dies zu einer besonders vorteilhaften Ausbildung.In particular with the simultaneous arrangement of the drive shaft bearing - viewed in the radial direction - within the connecting rod bearing, this leads to a particularly advantageous design.

Insbesondere besteht das synergetische Ziel des Konzepts der Erfindung darin, negative, insbesondere durch Biegemomente hervorgerufene, mechanische Auswirkungen wie Vibrationen, Körperschall- und Luftschallentwicklung sowohl durch die sich axial überdeckende Lageranordnung als auch durch das verbesserte Einleiten der Pleuelkräfte in das Gehäuse möglichst zu unterbinden. Dies wird insbesondere erreicht durch die axiale Anordnung des ersten Lagers bzw. A-Lagers innerhalb des Pleuellagers sowie die gestellfeste Befestigung des Innenrings des A-Lagers am gestellfesten Achszapfen. Auf diese Weise werden nämlich insbesondere in vorteilhafter Weise Kippmomente auf die Antriebswellenlager, insbesondere auf ein erstes Lager bzw. A-Lager sowie auf die Antriebswelle wirkende Axialkräfte reduziert bzw. vermieden. Insbesondere bei Fahrzeugen im PKW-Bereich ist ein geräusch- und vibrationsarmer Betrieb von großer Bedeutung, da hier, im Unterschied zu Anwendungen im LKW-Bereich, die Akustikanforderungen höher bzw. sensibler sind.In particular, the synergetic aim of the concept of the invention is to prevent negative mechanical effects such as vibrations, structure-borne noise and air-borne noise, both through the axially overlapping bearing arrangement and through the improved introduction of the connecting rod forces into the housing, as far as possible. This is achieved in particular by the axial arrangement of the first bearing or A-bearing within the connecting rod bearing as well as the frame-fixed fastening of the inner ring of the A-bearing on the axle journal fixed to the frame. In this way, in particular, tilting moments on the drive shaft bearings, in particular on a first bearing or A-bearing and axial forces acting on the drive shaft, are reduced or avoided in an advantageous manner. Low-noise and low-vibration operation is particularly important for vehicles in the passenger car sector, since here, in contrast to applications in the truck sector, the acoustic requirements are higher or more sensitive.

Das Konzept bietet vorzugsweise die Basis für eine in verbesserter Weise funktionierende, insbesondere vibrations- und geräuscharme Verdichteranordnung.The concept preferably offers the basis for a compressor arrangement that functions in an improved manner, in particular a low-vibration and low-noise compressor arrangement.

Weiterhin führen eine Reduzierung von Kräften und/oder Momenten sowie insbesondere eine Reduzierung der mit den Kräften und/oder Momenten verbundenen dynamischen Belastungen und Vibrationen, zu einer schonenderen Betriebsweise, welche sich auf Effizienz und Langlebigkeit der Verdichteranordnung positiv auswirken. Zu diesen Belastungen zählen vorliegend insbesondere auf das Pleuellager wirkende Kippmomente, welche bei einer herkömmlichen Antriebswellenlagerung durch Wellenbiegung entstehen. Die Reduzierung bzw. das Vermeiden derartiger Kippmomente durch eine Lagerung gemäß dem Konzept der Erfindung führt zu einer besseren Haltbarkeit des Pleuels; das Pleuel kann dadurch insbesondere in einer konstruktiven Optimierung kleiner und somit leichter ausgelegt werden.Furthermore, a reduction in forces and / or moments and, in particular, a reduction in the dynamic loads and vibrations associated with the forces and / or moments lead to a gentler mode of operation, which has a positive effect on the efficiency and longevity of the compressor arrangement. In the present case, these loads include, in particular, tilting moments acting on the connecting rod bearing, which occur in a conventional drive shaft bearing due to shaft bending. The reduction or avoidance of such tilting moments by a bearing according to the concept of the invention leads to a better durability of the connecting rod; the connecting rod can be designed to be smaller and therefore lighter, especially in a constructive optimization.

Ebenfalls werden durch die insbesondere biegemomentfreie Lagerung der Antriebswelle gemäß dem Konzept der Erfindung auf den Verdichterkolben und insbesondere Dichtmanschette wirkende Radialkräfte reduziert. Hierdurch ergibt sich in vorteilhafter Weise eine höhere Lebensdauer der Verdichter- und Antriebskomponenten, insbesondere Pleuellager, Antriebswellenlager Verdichterkolben und/oder Manschette.Radial forces acting on the compressor piston and in particular the sealing collar are also reduced by the particularly bending moment-free mounting of the drive shaft according to the concept of the invention. This advantageously results in a longer service life of the compressor and drive components, in particular connecting rod bearings, drive shaft bearings, compressor pistons and / or cuff.

Vorteilhafte Weiterbildungen der Erfindung sind den Unteransprüchen zu entnehmen und geben im Einzelnen vorteilhafte Möglichkeiten an, das oben erläuterte Konzept im Rahmen der Aufgabenstellung sowie hinsichtlich weiterer Vorteile zu realisieren.Advantageous further developments of the invention can be found in the subclaims and indicate in detail advantageous options for realizing the concept explained above within the scope of the task and with regard to further advantages.

Im Rahmen einer besonders bevorzugten Weiterbildung ist bei der Verdichteranordnung die Antriebswelle in dem an einem pleuelseitigen Ende der Antriebswelle in einer Lagerebene angeordneten, pleuelseitigen Antriebswellenlager als erstes Lager an einem koaxial zur Drehachse angeordneten ersten Lager-Aufnahmeabschnitt gelagert ist.As part of a particularly preferred development, the drive shaft in the compressor arrangement is mounted in the drive shaft bearing on the connecting rod end of the drive shaft in a bearing plane as the first bearing on a first bearing receiving section coaxially to the axis of rotation.

Die Weiterbildung geht von der Überlegung aus, dass ein Abstand in axialer Richtung zwischen der Lagerebene des ersten Lagers, bzw. A-Lagers und Pleuelebene zu einem Biegemoment führt, welches insbesondere in einer Verformung der Antriebswelle resultiert. Eine derartige Verformung kann bei einer drehenden Antriebswelle zu gegebenenfalls unvorteilhaften dynamischen Belastungszuständen und einer Geräusch- und Vibrationsentwicklung führen. Derartige Geräusch- und Vibrationsentwicklungen können durch gegebenenfalls über die Betriebszeit zunehmendes Lagerspiel noch weiter verstärkt werden. Verformungen der Antriebswelle sind insbesondere auf Pleuelkräfte zurückzuführen, welche bei einem Verdichten der Luft durch die Bewegung des Verdichterkolbens im Zylinder entstehen und über das Pleuellager und/oder das erste Lager bzw. A-Lager in die Antriebswelle geleitet werden. Das Biegemoment ist dabei proportional zu den Pleuelkräften und dem Abstand in axialer Richtung zwischen der Lagerebene und der Pleuelebene.The development is based on the consideration that a distance in the axial direction between the bearing plane of the first bearing or A-bearing and the connecting rod plane leads to a bending moment, which in particular results in a deformation the drive shaft results. In the case of a rotating drive shaft, such a deformation can lead to possibly disadvantageous dynamic load conditions and the development of noise and vibrations. Such noise and vibration developments can be further intensified by bearing play that may increase over the operating time. Deformations of the drive shaft are due in particular to connecting rod forces which arise when the air is compressed by the movement of the compressor piston in the cylinder and which are passed into the drive shaft via the connecting rod bearing and / or the first bearing or A-bearing. The bending moment is proportional to the connecting rod forces and the distance in the axial direction between the bearing plane and the connecting rod plane.

Die Weiterbildung hat erkannt, dass bei einer Verringerung des Abstandes in axialer Richtung zwischen der Lagerebene des ersten Lagers bzw. A-Lagers und der Pleuelebene des Pleuels das auf die Antriebswelle wirkende Biegemoment reduziert wird. Eine Verringerung kann insbesondere erreicht werden, wenn das erste Lager bzw. A-Lager in radialer Richtung innerhalb des Pleuellagers angeordnet ist. Insbesondere wird bei einer vollständigen Vermeidung des Abstandes in axialer Richtung zwischen der Lagerebene des ersten Lagers bzw. A-Lagers und der Pleuelebene des Pleuellagers ein durch Pleuelkräfte hervorgerufenes, auf die Antriebswelle wirkendes Biegemoment vollständig vermieden.The development has recognized that when the distance in the axial direction between the bearing plane of the first bearing or A-bearing and the connecting rod plane of the connecting rod is reduced, the bending moment acting on the drive shaft is reduced. A reduction can be achieved in particular if the first bearing or A-bearing is arranged in the radial direction within the connecting rod bearing. In particular, if the distance in the axial direction between the bearing plane of the first bearing or A-bearing and the connecting rod plane of the connecting rod bearing is completely avoided, a bending moment which is caused by connecting rod forces and acting on the drive shaft is completely avoided.

Insbesondere ist vorgesehen, dass die Antriebswelle in dem an einem pleuelfernen Ende der Antriebswelle angeordneten pleuelfernen Antriebswellenlager als zweites Lager an einem koaxial zur Drehachse am pleuelfernen Ende angeordneten zweiten Lager-Aufnahmeabschnitt gelagert ist.In particular, it is provided that the drive shaft is mounted in the drive shaft bearing located on an end remote from the connecting rod as a second bearing on a second bearing receiving section located coaxially to the axis of rotation at the end remote from the connecting rod.

Weiterhin ist in einer bevorzugten Weiterbildung vorgesehen, dass die Lager innerhalb des Gehäuses und/oder an diesem angeordnet sind. Das Gehäuse kann die Verdichteranordnung und/oder den Antrieb und/oder weitere Komponenten umfassen und diese einhausen, und besonders vorteilhaft modular, das heißt insbesondere jeweils für Verdichteranordnung und Antrieb einzeln, aber zusammensetzbar, ausgebildet sein.Furthermore, it is provided in a preferred development that the bearings are arranged within the housing and / or on it. The housing can comprise the compressor arrangement and / or the drive and / or further components and house them, and particularly advantageously in a modular manner means, in particular, for the compressor arrangement and drive to be designed individually but can be assembled.

Vorzugsweise ist bei der Verdichteranordnung

  • der erste Lager-Aufnahmeabschnitt zur Aufnahme des ersten Lagers als ein zylindrischer Hohlraum ausgebildet, und/oder
  • das erste Lager weiterhin auf einem gestellfest mit dem Gehäuse verbundenen und praktisch koaxial zur Drehachse angeordneten Achszapfen befestigt ist, wobei
  • das erste Lager in dem zylindrischen Hohlraum zwischen dem ersten Lager-Aufnahmeabschnitt und dem Achszapfen sitzt.
Preferably in the compressor arrangement
  • the first bearing receiving section for receiving the first bearing is designed as a cylindrical cavity, and / or
  • the first bearing is also attached to an axle journal which is fixedly connected to the frame and arranged practically coaxially to the axis of rotation, wherein
  • the first bearing is seated in the cylindrical cavity between the first bearing receiving section and the journal.

Weiter geht die Weiterbildung von der Überlegung aus, dass eine Umkehrung der Befestigungsanordnung des ersten Lagers bzw. A-Lagers, nämlich die orts- bzw. gestellfeste Befestigung des Innenrings und eine drehbare Lagerung des Außenrings, in besonders vorteilhafter Weise eine Ableitung der Pleuelkräfte in das Gehäuse ermöglicht. Dies ist insbesondere der Fall, weil die gestellfeste Befestigung des ersten Lagers bzw. A-Lagers mittels eines gestellfesten Achszapfens in geringem axialen Abstand zur Wand des Gehäuses möglich ist. Durch den geringen axialen Abstand ist eine verbesserte Aufnahme der Pleuelkräfte möglich, insbesondere ohne durch Pleuelkräfte hervorgerufene Biegemomente und besonders bevorzugt ohne Verformung der Antriebswelle oder des Achszapfens.Furthermore, the development is based on the idea that a reversal of the fastening arrangement of the first bearing or A-bearing, namely the stationary or frame-fixed fastening of the inner ring and a rotatable mounting of the outer ring, a transfer of the connecting rod forces into the Housing allows. This is particularly the case because it is possible to fasten the first bearing or A-bearing fixed to the frame by means of an axle journal fixed to the frame at a small axial distance from the wall of the housing. Due to the small axial distance, an improved absorption of the connecting rod forces is possible, in particular without bending moments caused by connecting rod forces and particularly preferably without deforming the drive shaft or the axle journal.

Insbesondere ist vorgesehen, dass das erste Lager fest auf dem Achszapfen aufsitzt und in dem ersten Lager-Aufnahmeabschnitt festsitzt und den Achszapfen und den ersten Lager-Aufnahmeabschnitt relativ zueinander drehbar verbindet. Konkret bedeutet dies, dass der Lagerinnenring des ersten Lagers ortsfest auf dem Achszapfen befestigt ist, beispielsweise durch ein geeignetes form-, kraft, oder stoffschlüssiges Befestigungsverfahren. Weiterhin ist der Lageraußenring des ersten Lagers fest mit dem Lager-Aufnahmeabschnitt der Antriebswelle verbunden. Auf diese Weise wird eine rotatorische Relativbewegung zwischen dem gestellfesten Achszapfen und der Antriebswelle um die Drehachse ermöglicht.In particular, it is provided that the first bearing is firmly seated on the journal and is firmly seated in the first bearing receiving section and connects the journal and the first bearing receiving section rotatably relative to one another. Specifically, this means that the bearing inner ring of the first bearing is fixed in place on the axle journal, for example by a suitable form-fitting, force-fitting or material-locking fastening method. Furthermore, the bearing outer ring of the first bearing is fixed to the bearing receiving section of the Drive shaft connected. In this way, a rotational relative movement between the axle journal fixed to the frame and the drive shaft around the axis of rotation is made possible.

Vorteilhaft ist vorgesehen, dass der Verdichter mehrere, insbesondere ein erstes Pleuel und ein zweites Pleuel aufweist. Konkret kann dies beinhalten, dass Gas, insbesondere Luft, in zwei oder mehreren Verdichtungskammern verdichtet wird. In diesem Fall wird ein zweistufiger Verdichter durch die Anordnung von zwei Zylindern realisiert, wobei die Zylinder jeweils über einen Verdichterkolben und ein Pleuel verfügen. Diese werden insbesondere von einer Antriebswelle angetrieben und sind bevorzugt derart angeordnet, dass sich das Gesamtsystem in einem praktisch ausgewuchteten Zustand befindet. Ein zweistufiger Verdichter führt insbesondere zu den Vorteilen höherer erreichbarer Wirkungsgrade und Verdichtungsdrücke.It is advantageously provided that the compressor has several, in particular a first connecting rod and a second connecting rod. Specifically, this can mean that gas, in particular air, is compressed in two or more compression chambers. In this case, a two-stage compressor is implemented by arranging two cylinders, the cylinders each having a compressor piston and a connecting rod. These are in particular driven by a drive shaft and are preferably arranged such that the overall system is in a practically balanced state. A two-stage compressor leads in particular to the advantages of higher achievable efficiencies and compression pressures.

Insbesondere ist vorgesehen, dass das erste Pleuel und das zweite Pleuel derartig angeordnet sind, dass das erste Pleuel in einem ersten Lagerabstand und das zweite Pleuel in einem zweiten Lagerabstand in axialer Richtung, d. h. in Richtung der Drehachse, zur Lagerebene angeordnet sind. Konkret bedeutet dies, dass der erste und der zweite Lagerabstand je nach konstruktivem Erfordernis derart gewählt werden können, dass insbesondere Verformungen der Antriebswelle und Belastungen auf Pleuel und Lager möglichst minimiert werden können. Insbesondere für den Fall, dass ein Pleuel größere Kräfte aufnimmt als das andere, können auf die Antriebswelle wirkende Biegemomente dadurch minimiert werden, dass der Lagerabstand zu dem die größeren Kräfte aufnehmenden Pleuel verringert wird. Weiterhin kann das Einstellen des Lagerabstandes in vorteilhafter Weise genutzt werden, um eine Wellenbiegung, insbesondere zur Kompensation einer Verformung des Achszapfens, zu erzeugen. Dies ist in der Zeichnung in Fig. 3 beispielhaft dargestellt und im Zusammenhang mit der Fig. 3 beispielhaft im Rahmen einer bevorzugten Ausführungsform weiter erläutert.In particular, it is provided that the first connecting rod and the second connecting rod are arranged in such a way that the first connecting rod is arranged at a first bearing distance and the second connecting rod is arranged at a second bearing distance in the axial direction, ie in the direction of the axis of rotation, to the bearing plane. Specifically, this means that the first and the second bearing spacing can be selected depending on the structural requirements in such a way that, in particular, deformations of the drive shaft and loads on connecting rods and bearings can be minimized as far as possible. Particularly in the event that one connecting rod absorbs greater forces than the other, bending moments acting on the drive shaft can be minimized by reducing the bearing spacing from the connecting rod absorbing the greater forces. Furthermore, the setting of the bearing spacing can be used in an advantageous manner to produce a shaft bending, in particular to compensate for a deformation of the axle journal. This is in the drawing in Fig. 3 shown by way of example and in connection with the Fig. 3 further explained by way of example in the context of a preferred embodiment.

Im Rahmen einer besonders bevorzugten Weiterbildung ist vorgesehen, dass das erste Pleuel und das zweite Pleuel derartig angeordnet sind, dass sich die Lagerebene in axialer Richtung mittig zwischen einer ersten Pleuelebene (bereits hier zur Verdeutlichung: in der Zeichnung mit P1 bezeichnet) und einer zweiten Pleuelebene (bereits hier zur Verdeutlichung: in der Zeichnung mit P2 bezeichnet) befindet. Konkret bedeutet dies, dass die erste und die zweite Pleuelebene in einem betragsmäßig gleichen axialen Abstand, jedoch in entgegengesetzter Richtung zur Lagerebene angeordnet sind. Obwohl sich in dieser Weiterbildung keine der beiden Pleuelebenen in der Lagerebene befindet und somit auf die Antriebswelle wirkende Biegemomente auftreten, stellt die axial mittige Anordnung des ersten Lagers bzw. A-Lagers zwischen beiden Pleueln einen Kompromiss zur Minimierung der durch Pleuelkräfte entstehenden Biegemomente dar.In a particularly preferred development, it is provided that the first connecting rod and the second connecting rod are arranged in such a way that the bearing plane is centered in the axial direction between a first connecting rod plane (already here for clarification: denoted by P1 in the drawing) and a second connecting rod plane (already here for clarification: designated in the drawing with P2). Specifically, this means that the first and the second connecting rod planes are arranged at an axial distance of the same amount, but in the opposite direction to the bearing plane. Although neither of the two connecting rod planes is in the bearing plane in this further development and therefore bending moments acting on the drive shaft occur, the axially central arrangement of the first bearing or A-bearing between the two connecting rods represents a compromise to minimize the bending moments caused by connecting rod forces.

Insbesondere ist vorgesehen, dass der Kompressor ein erstes Pleuel aufweist, das in der Lagerebene des ersten Lagers angeordnet ist, der Lagerabstand zwischen Pleuelebene und Lagerebene praktisch gleich null ist. Konkret bedeutet dies, dass durch die Anordnung von erstem Pleuel und ersten Lager bzw. A-Lager ohne axialen Abstand mit einer Lageranordnung gemäß dem Konzept der Erfindung eine praktisch biegemomentfreie Aufnahme von Pleuelkräften erreicht wird.In particular, it is provided that the compressor has a first connecting rod which is arranged in the bearing plane of the first bearing, the bearing distance between the connecting rod plane and the bearing plane is practically zero. Specifically, this means that the arrangement of the first connecting rod and the first bearing or A-bearing without axial spacing with a bearing arrangement according to the concept of the invention achieves a practically bending moment-free absorption of connecting rod forces.

Diese Weiterbildung kommt insbesondere für einstufige Verdichter mit einem Pleuel und einem Zylinder in Frage. Jedoch kann im Rahmen dieser biegemomentfreien, einfachen Pleuelanordnung wie untenstehend weiter beschrieben auch ein zweistufiger Verdichter innerhalb eines Zylinders mit einem beidseitig druckbeaufschlagbaren Verdichterkolben realisiert werden.This development is particularly suitable for single-stage compressors with a connecting rod and a cylinder. However, within the scope of this bending moment-free, simple connecting rod arrangement, as further described below, a two-stage compressor can also be implemented within a cylinder with a compressor piston that can be pressurized on both sides.

Insbesondere ist vorgesehen, dass der Kompressor ein erstes Pleuel aufweist, das in einem axialen Lagerabstand zum ersten Lager angeordnet ist. Konkret bedeutet dies, dass die auf die Antriebswelle wirkenden Pleuelkräfte zu einem Biegemoment führen, welches, in Abhängigkeit der konstruktiven Auslegung der Antriebswelle, insbesondere zu einer Verformung führen kann. Diese Verformung, insbesondere eine Biegung der Antriebswelle, kann beispielsweise vorteilhaft genutzt werden, um eine Verformung des Achszapfens zu kompensieren. Dies ist in der Zeichnung in Fig. 3 beispielhaft dargestellt und im Zusammenhang mit der Fig. 3 beispielhaft im Rahmen einer bevorzugten Ausführungsform weiter erläutert.In particular, it is provided that the compressor has a first connecting rod which is arranged at an axial bearing spacing from the first bearing. Specifically, this means that the connecting rod forces acting on the drive shaft lead to a bending moment which, depending on the structural design of the drive shaft, can in particular lead to deformation. This deformation, in particular a bend in the drive shaft can be used advantageously, for example, to compensate for a deformation of the axle journal. This is in the drawing in Fig. 3 shown by way of example and in connection with the Fig. 3 further explained by way of example in the context of a preferred embodiment.

Im Rahmen einer besonders bevorzugten Weiterbildung ist vorgesehen, dass das erste Pleuel und der Verdichterkolben starr miteinander verbunden sind, insbesondere der Verdichter als Taumelkolbenkompressor ausgebildet ist. Dies bedeutet konkret, dass Pleuel und Verdichterkolben im Wesentlichen einstückig ausgebildet sind. Dies führt zu dem Vorteil, dass weniger bewegte Teile zur Kopplung von Antrieb und Verdichterkolben eingesetzt werden müssen und gegebenenfalls auch keine Führungselemente für den Kolben zur Aufnahme seitlicher, durch das Pleuel eingeleiteter Kräfte, benötigt werden. Etwaige, sich durch die Taumelkinematik ergebende Spalte zwischen Zylinder und Verdichterkolben werden in einer derartigen Ausführungsform durch geeignete Dichtungen, insbesondere Kolbenmanschettendichtungen, abgedichtet.In the context of a particularly preferred development, it is provided that the first connecting rod and the compressor piston are rigidly connected to one another, in particular the compressor is designed as a wobble piston compressor. Specifically, this means that the connecting rod and the compressor piston are essentially constructed in one piece. This leads to the advantage that fewer moving parts have to be used to couple the drive and compressor piston and, if necessary, no guide elements are required for the piston to absorb lateral forces introduced by the connecting rod. Any gaps between the cylinder and the compressor piston resulting from the wobble kinematics are sealed in such an embodiment by means of suitable seals, in particular piston sleeve seals.

Vorteilhaft ist vorgesehen, dass der Verdichter als einstufiger Verdichter ausgebildet ist. Konkret bedeutet dies, dass das Gas, insbesondere die Luft, in einer Verdichtungskammer verdichtet wird. Diese Verdichtungskammer wird von dem Innenraum des Zylinders und der dem Pleuel gegenüberliegenden Seite des Verdichterkolbens gebildet.It is advantageously provided that the compressor is designed as a single-stage compressor. Specifically, this means that the gas, in particular the air, is compressed in a compression chamber. This compression chamber is formed by the interior of the cylinder and the side of the compressor piston opposite the connecting rod.

Insbesondere ist vorgesehen, dass der Verdichter als mehrstufiger Verdichter, insbesondere zweistufiger Verdichter, ausgebildet ist. Konkret bedeutet dies, dass das Gas, insbesondere die Luft, in zwei oder mehreren Verdichtungskammern verdichtet wird. Ein derartiger mehrstufiger Verdichter durch die Anordnung mehrerer, insbesondere von zwei, Kolben realisiert werden, wobei die Kolben jeweils über einen Verdichterkolben und ein Pleuel verfügen. Diese werden insbesondere von einer Antriebswelle angetrieben und sind bevorzugt derart angeordnet, dass sich das Gesamtsystem in einem praktisch ausgewuchteten Zustand befindet.In particular, it is provided that the compressor is designed as a multi-stage compressor, in particular a two-stage compressor. Specifically, this means that the gas, in particular the air, is compressed in two or more compression chambers. Such a multi-stage compressor can be realized by the arrangement of several, in particular two, pistons, the pistons each having a compressor piston and a connecting rod. These are in particular driven by a drive shaft and are preferably arranged such that the overall system is in a practically balanced state.

Im Falle eines zweistufigen Verdichters kann das Gas beispielsweise in zwei Verdichtungskammern verdichtet werden, die jeweils durch einen Zylinder sowie einem beidseitig druckbeaufschlagbaren Verdichterkolben gebildet werden. Die dem Pleuel gegenüberliegende Seite des Verdichterkolbens bildet hierbei zusammen mit dem auf dieser Seite des Verdichterkolbens liegenden Innenraum des Zylinders die erste Verdichtungskammer. Die dem Pleuel zugewandte Seite bildet weiterhin zusammen mit dem auf jener Seite des Verdichterkolbens liegenden Innenraum des Zylinders die zweite Verdichtungskammer.In the case of a two-stage compressor, the gas can be compressed in two compression chambers, for example, which are each formed by a cylinder and a compression piston that can be pressurized on both sides. The side of the compressor piston opposite the connecting rod together with the interior of the cylinder located on this side of the compressor piston forms the first compression chamber. The side facing the connecting rod together with the interior of the cylinder located on that side of the compressor piston also forms the second compression chamber.

Vorteilhaft ist vorgesehen, dass das Pleuellager als ein Wälzlager, insbesondere ein Kugellager, Nadellager, Zylinderrollenlager, Tonnenlager oder dergleichen Wälzlager gebildet ist.It is advantageously provided that the connecting rod bearing is formed as a roller bearing, in particular a ball bearing, needle roller bearing, cylindrical roller bearing, barrel bearing or similar roller bearing.

Konkret bedeutet dies, dass eine Lagerform in Abhängigkeit der konstruktiven Anforderungen gewählt wird. Nadel- und Zylinderrollenlager und allgemein Wälzlager mit zylindrischen Wälzkörpern haben aufgrund des Linienkontaktes mit der Lauffläche eine generell hohe radiale Tragfähigkeit. Bei einem Nadellager kommt hinzu, dass es aufgrund der geringen Wälzkörperdurchmesser relativ kompakt ist, und somit in vorteilhafter Weise den Einbauraum des Antriebs weiter verkleinert. Kugellager weisen aufgrund der Schmiegung in den Wälzkontakten eine relativ hohe axiale und radiale Tragfähigkeit auf. Tonnenlager ermöglichen weiterhin, aufgrund der balligen Ausführung der Wälzkörper und einer hohlkugeligen Außenringlaufbahn, eine gewisse Pendelbewegung zwischen Innen- und Außenring. Somit wird eine Unempfindlichkeit gegen Schiefstellung und Fluchtfehler der Antriebswelle gegenüber dem Gehäuse erreicht.In concrete terms, this means that a bearing form is selected depending on the design requirements. Needle and cylindrical roller bearings and generally roller bearings with cylindrical rolling elements have a generally high radial load capacity due to the line contact with the running surface. In the case of a needle bearing, there is also the fact that it is relatively compact due to the small diameter of the rolling elements, and thus advantageously further reduces the installation space of the drive. Due to the osculation in the rolling contacts, ball bearings have a relatively high axial and radial load-bearing capacity. Due to the spherical design of the rolling elements and a spherical outer ring raceway, barrel bearings also allow a certain pendulum movement between the inner and outer ring. This makes it insensitive to misalignment and misalignment of the drive shaft with respect to the housing.

Vorteilhaft ist vorgesehen, dass das erste Lager und/oder das zweite Lager als ein Gleitlager gebildet ist. Konkret kann dies durch eine geschmierte oder schmierungsfreie Gleitlagerung erreicht werden. Dies führt in vorteilhafter Weise zu einer wartungsarmen, besonders bevorzugt wartungsfreien, Auslegung der drehbeweglichen Verbindung, da sie - abgesehen von der Relativbewegung zwischen Welle und Lager - keine bewegten Teile, insbesondere keine Wälzkörper, aufweist.It is advantageously provided that the first bearing and / or the second bearing is formed as a plain bearing. Specifically, this can be achieved with a lubricated or lubrication-free plain bearing. This leads in an advantageous manner to a low-maintenance, particularly preferably maintenance-free, design of the rotatable connection, since it - apart from the relative movement between shaft and bearing - has no moving parts, in particular no rolling elements.

Insbesondere ist vorgesehen, dass das erste Lager und/oder das zweite Lager kraftschlüssig, insbesondere durch einen Toleranzring, befestigt ist. Konkret kann der Toleranzring durch einen Metall-Federring, oder ein aus Gummi oder Kunststoff bestehenden Ring mit geeignetem Querschnitt, oder ein weiteres geeignetes, komprimierbares Verbindungselement gebildet sein. Weiterhin kann das das erste Lager bzw. A-Lager und/oder das zweite Lager bzw. B-Lager alternativ und/oder zusätzlich auch auf andere Weise, beispielsweise formschlüssig durch einen in axialer Richtung angeordneten Sicherungsring oder kraft-/ bzw. reibschlüssig durch thermisches Einschrumpfen, fixiert werden. Die Befestigung mittels eines Befestigungselements wie z. B. eines Toleranzrings kann sich sowohl auf die Innenseite des Innenrings als auch auf die Außenseite des Außenrings des jeweiligen Lagers beziehen. Folglich wäre beispielsweise für das erste Lager sowohl ein zwischen dem Hohlraum und dem Außenring des ersten Lagers angeordneter Toleranzring möglich, als auch zwischen ein zwischen dem Achszapfen und dem Innenring angeordneter Toleranzring.In particular, it is provided that the first bearing and / or the second bearing is non-positively fastened, in particular by a tolerance ring. Specifically, the tolerance ring can be formed by a metal spring ring, or a ring made of rubber or plastic with a suitable cross section, or a further suitable, compressible connecting element. Furthermore, the first bearing or A-bearing and / or the second bearing or B-bearing can alternatively and / or additionally also in other ways, for example positively by a locking ring arranged in the axial direction or non-positively or frictionally by thermal Shrink, be fixed. The attachment by means of a fastening element such. B. a tolerance ring can refer to both the inside of the inner ring and the outside of the outer ring of the respective bearing. Consequently, for the first bearing, for example, both a tolerance ring arranged between the cavity and the outer ring of the first bearing and between a tolerance ring arranged between the axle journal and the inner ring would be possible.

Die Erfindung führt zur Lösung der Aufgabe auch auf eine Druckluftversorgungsanlage zum Betreiben einer Pneumatikanlage. Diese Druckluftversorgungsanlage weist auf: eine vorgenannte Verdichteranordnung, einen Lufttrockner und eine Ventilanordnung. Weiterhin führt die Erfindung zur Lösung der Aufgabe auch auf ein Fahrzeug, mit einer Druckluftversorgungsanlage und einer Pneumatikanlage, wobei die Druckluftversorgungsanlage eine Verdichteranordnung gemäß dem Konzept der Erfindung aufweist. Eine Verdichteranordnung gemäß dem Konzept der Erfindung ist insbesondere bei PKW vorteilhaft, da im Bereich der PKW hohe Akustikanforderungen herrschen und ein geräusch- und vibrationsarmer Betrieb der Verdichteranordnung hohe Bedeutung besitzt bzw. vorteilhaft ist.In order to achieve the object, the invention also leads to a compressed air supply system for operating a pneumatic system. This compressed air supply system has: an aforementioned compressor arrangement, an air dryer and a valve arrangement. Furthermore, the invention also leads to the solution of the object on a vehicle with a compressed air supply system and a pneumatic system, the compressed air supply system having a compressor arrangement according to the concept of the invention. A compressor arrangement according to the concept of the invention is particularly advantageous in the case of cars, since high acoustic requirements prevail in the field of cars and low-noise and low-vibration operation of the compressor arrangement is of great importance or is advantageous.

Ausführungsformen der Erfindung werden nun nachfolgend anhand der Zeichnung beschrieben. Diese soll die Ausführungsformen nicht notwendigerweise maßstäblich darstellen, vielmehr ist die Zeichnung, wo zur Erläuterung dienlich, in schematisierter und/oder leicht verzerrter Form ausgeführt. Im Hinblick auf Ergänzungen der aus der Zeichnung unmittelbar erkennbaren Lehren wird auf den einschlägigen Stand der Technik verwiesen. Dabei ist zu berücksichtigen, dass vielfältige Modifikationen und Änderungen betreffend die Form und das Detail einer Ausführungsform vorgenommen werden können, ohne von der allgemeinen Idee der Erfindung abzuweichen. Die in der Beschreibung, in der Zeichnung sowie in den Ansprüchen offenbarten Merkmale der Erfindung können sowohl einzeln als auch in beliebiger Kombination für die Weiterbildung der Erfindung wesentlich sein. Zudem fallen in den Rahmen der Erfindung alle Kombinationen aus zumindest zwei der in der Beschreibung, der Zeichnung und/oder den Ansprüchen offenbarten Merkmale. Die allgemeine Idee der Erfindung ist nicht beschränkt auf die exakte Form oder das Detail der im Folgenden gezeigten und beschriebenen bevorzugten Ausführungsformen oder beschränkt auf einen Gegenstand, der eingeschränkt wäre im Vergleich zu dem in den Ansprüchen beanspruchten Gegenstand. Bei angegebenen Bemessungsbereichen sollen auch innerhalb der genannten Grenzen liegende Werte als Grenzwerte offenbart und beliebig einsetzbar und beanspruchbar sein. Der Einfachheit halber sind nachfolgend für identische oder ähnliche Teile oder Teile mit identischer oder ähnlicher Funktion gleiche Bezugszeichen verwendet.Embodiments of the invention will now be described below with reference to the drawing. This is not necessarily intended to represent the embodiments to scale; rather, the drawing, where useful for explanation, is shown in a schematic and / or slightly distorted form. With regard to additions to the teachings that can be seen directly from the drawing, reference is made to the relevant prior art. It must be taken into account here that various modifications and changes relating to the shape and detail of an embodiment can be made without deviating from the general idea of the invention. The features of the invention disclosed in the description, in the drawing and in the claims can be essential for the development of the invention both individually and in any combination. In addition, all combinations of at least two of the features disclosed in the description, the drawing and / or the claims fall within the scope of the invention. The general idea of the invention is not restricted to the exact form or the detail of the preferred embodiments shown and described below or restricted to an object that would be restricted in comparison to the object claimed in the claims. In the case of the specified measurement ranges, values lying within the stated limits should also be disclosed as limit values and be able to be used and claimed as required. For the sake of simplicity, the same reference symbols are used below for identical or similar parts or parts with identical or similar functions.

Weitere Vorteile, Merkmale und Einzelheiten der Erfindung ergeben sich aus der nachfolgenden Beschreibung der bevorzugten Ausführungsformen sowie anhand der Zeichnung; diese zeigt in:

Fig. 1
eine Verdichteranordnung gemäß einer besonders bevorzugten Ausführungsform,
Fig. 2A - 2C
unterschiedliche Anordnungen von Antriebswellenlager und Pleuellager gemäß dem Konzept der Erfindung,
Fig. 3A - 3D
unterschiedliche Anordnungen von erstem Lager bzw. A-Lager und Pleuellager in verschiedenen Weiterbildungen, vor allem gemäß der bevorzugten Ausführungsform der Fig.1 aber insgesamt dem Konzept der Fig.2 folgend,
Fig. 4
eine schematische Darstellung der Durchbiegung von Antriebswelle und Achszapfen,
Fig. 5
eine stark vereinfachte, schematische Übersicht einer Druckluftversorgungsanlage,
Fig. 6
eine schematische Darstellung eines Fahrzeugs mit einer Druckluftversorgungsanlage.
Further advantages, features and details of the invention emerge from the following description of the preferred embodiments and with reference to the drawing; this shows in:
Fig. 1
a compressor arrangement according to a particularly preferred embodiment,
Figures 2A-2C
different arrangements of drive shaft bearings and connecting rod bearings according to the concept of the invention,
Figures 3A-3D
different arrangements of the first bearing or A-bearing and connecting rod bearing in different developments, especially according to the preferred embodiment of FIG Fig.1 but overall the concept of Fig. 2 following,
Fig. 4
a schematic representation of the deflection of the drive shaft and axle journal,
Fig. 5
a greatly simplified, schematic overview of a compressed air supply system,
Fig. 6
a schematic representation of a vehicle with a compressed air supply system.

Fig. 1 zeigt eine Verdichteranordnung mit einem Verdichter 100 gemäß einer besonders bevorzugten Ausführungsform der Erfindung. In einem ersten Zylinder 170 wird zwecks Verdichtung von Luft ein erstes Pleuel 140 mit einem ersten Verdichterkolben 150 oszillierend und praktisch entlang der Symmetrieachse des ersten Zylinders 170 auf- und abwärts bewegt. Vorliegend ist der erste Verdichterkolben 150 nahe dem oberen Totpunkt, d. h. am oberen Ende des Hubweges H, dargestellt. Aufgrund der Tatsache, dass es sich bei der hier gezeigten Ausführungsform um einen Taumelkolbenkompressor handelt, das heißt das erste Pleuel 140 und der erste Verdichterkolben 150 starr verbunden sind, ist die oszillierende Bewegung zwar überwiegend, aber nicht vollständig translatorisch. Daher führen das erste Pleuel 140 und der erste Verdichterkolben 150 bei der Auf- und Abwärtsbewegung eine der Kinematik entsprechende, taumelnde Bewegung durch. Fig. 1 shows a compressor arrangement with a compressor 100 according to a particularly preferred embodiment of the invention. In a first cylinder 170, for the purpose of compressing air, a first connecting rod 140 with a first compressor piston 150 is moved up and down in an oscillating manner and practically along the axis of symmetry of the first cylinder 170. In the present case, the first compressor piston 150 is shown near top dead center, ie at the top end of the stroke path H. Due to the fact that the embodiment shown here is a wobble piston compressor, that is, the first connecting rod 140 and the first compressor piston 150 are rigidly connected, the oscillating movement is predominantly, but not completely, translational. The first connecting rod 140 and the first compressor piston 150 therefore perform a tumbling movement corresponding to the kinematics during the upward and downward movement.

Analog zum ersten Zylinder 170 wird in einem zweiten Zylinder 171 zwecks Verdichtung von Luft ein zweites Pleuel 141 mit einem zweiten Verdichterkolben 151 oszillierend und praktisch entlang der Symmetrieachse des zweiten Zylinders 171 auf- und abwärts bewegt.Analogous to the first cylinder 170, a second connecting rod 141 with a second compressor piston 151 is moved up and down in a second cylinder 171 in an oscillating manner and practically along the symmetry axis of the second cylinder 171 for the purpose of compressing air.

Auch wäre jedoch eine Ausführungsform gemäß dem Konzept der Erfindung denkbar, bei dem - wie bei Kolbenverdichtern weithin üblich - der erste Verdichterkolben 150 mit dem ersten Pleuel 140 bzw. der zweite Verdichterkolben 151 mit dem zweiten Pleuel 141 jeweils gelenkig, insbesondere jeweils mittels einer Lagerung, verbunden sind.However, an embodiment according to the concept of the invention would also be conceivable in which - as is widely used in piston compressors - the first compressor piston 150 with the first connecting rod 140 and the second compressor piston 151 with the second connecting rod 141 are each articulated, in particular by means of a bearing, are connected.

Auch sind neben dem gezeigten zweistufigen Kompressor einstufige Kompressoren gemäß dem Konzept der Erfindung möglich. Auch kann in einer weiteren Weiterbildung ein mehrstufiger Kompressor durch einen Einkolben-Kompressor gebildet sein, welcher, durch entsprechend abgestufte Kolben und Zylinder oder durch einen mehrseitig druckbeaufschlagbaren Kolben, mehrere Verdichtungskammern bildet.In addition to the two-stage compressor shown, single-stage compressors according to the concept of the invention are also possible. In a further development, a multi-stage compressor can also be formed by a single-piston compressor which, by means of appropriately graduated pistons and cylinders or by a piston that can be pressurized on more than one side, forms a plurality of compression chambers.

In der vorliegenden Weiterbildung ist die Antriebswelle 220 mittels eines ersten, pleuelseitigen Antriebswellenlagers bzw. A-Lagers 360 und eines zweiten, pleuelfernen Antriebswellenlagers bzw. B-Lagers 362 in einem Gehäuse 440 gelagert. Dabei kann sowohl das A-Lager 360 als auch das B-Lager 362 mittels eines hier nicht näher dargestellten Toleranzrings 164 befestigt sein. Diese Befestigung, die insbesondere einem festen Lagersitz dient, kann sich sowohl auf die Innenseite des jeweiligen Lagers 360, 362, als auch auf die Außenseite des jeweiligen Lagers 360, 362 beziehen.In the present development, the drive shaft 220 is supported in a housing 440 by means of a first, connecting-rod-side drive shaft bearing or A-bearing 360 and a second, connecting-rod-remote drive shaft bearing or B-bearing 362. Both the A-bearing 360 and the B-bearing 362 can be fastened by means of a tolerance ring 164, not shown here. This fastening, which in particular serves as a fixed bearing seat, can relate both to the inside of the respective bearing 360, 362 and to the outside of the respective bearing 360, 362.

Weiterhin sind vorliegend die beiden Zylinder 170, 171 hinsichtlich der Drehachse A praktisch gegenüberliegend angeordnet. Somit sind diese in vorteilhafter Weise derartig angeordnet, dass sich die linearen Trägheitskräfte des Systems bewegter Massen, insbesondere der Pleuel, Verdichterkolben und Manschetten, während der Bewegung aufheben.Furthermore, in the present case the two cylinders 170, 171 are arranged practically opposite one another with regard to the axis of rotation A. Thus, these are advantageously arranged in such a way that the linear inertial forces of the system of moving masses, in particular the connecting rods, compressor pistons and sleeves, cancel each other out during the movement.

Im Falle eines einstufigen, insbesondere einkolbigen Kompressors, kann diese aufhebende Funktion eines gegenüberliegenden Kolbens durch ein Ausgleichsgewicht erreicht werden. Bei einer Zylinder- bzw. Kolbenanzahl größer zwei müssen analog zum Erreichen eines Massenausgleichs die Zylinder derartig um die Drehachse A angeordnet werden, dass sich die Trägheitskräfte insgesamt ausgleichen.In the case of a single-stage, in particular single-piston, compressor, this canceling function of an opposing piston can be achieved by a counterweight. If the number of cylinders or pistons is greater than two, the cylinders must be similar to achieve a mass balance be arranged around the axis of rotation A, that the inertial forces balance each other out.

Die Pleuel 140, 141 weisen weiterhin jeweils auf ihren dem Verdichterkolben 150, 151 gegenüberliegenden Seiten ein Pleuelauge auf, welches zur Aufnahme eines Pleuellagers 160, 161 dient. Das Pleuellager 160, 161 dient weiterhin zur drehbeweglichen Verbindung des Pleuels 140, 141 mit einem PleuelAufnahmeabschnitt 320 einer Antriebswelle 220.The connecting rods 140, 141 each have a connecting rod eye on their sides opposite the compressor piston 150, 151, which is used to hold a connecting rod bearing 160, 161. The connecting rod bearing 160, 161 also serves to connect the connecting rod 140, 141 in a rotatable manner to a connecting rod receiving section 320 of a drive shaft 220.

Vorliegend ist der Pleuelaufnahmeabschnitt 320 einstückig mit der Antriebswelle 220 verbunden; gleichwohl ist es aber genauso möglich, dass Pleuelaufnahmeabschnitt 320 und Antriebswelle 220 zweistückig ausgeführt sind und über eine entsprechende form-, kraft- oder stoffschlüssige Verbindung zusammengefügt sind.In the present case, the connecting rod receiving section 320 is integrally connected to the drive shaft 220; Nevertheless, it is just as possible for the connecting rod receiving section 320 and the drive shaft 220 to be designed in two pieces and to be joined together via a corresponding positive, non-positive or material connection.

Die Antriebswelle 220 weist weiterhin an einem pleuelseitigen Ende PS neben dem außenliegenden Pleuel-Aufnahmeabschnitt 320, einen innenliegenden ersten Lager-Aufnahmeabschnitt 380 auf. Der außenliegende Pleuel-Aufnahmeabschnitt 320 weist eine zylindrische Außenform auf, welche den Innenring der Pleuellager 160, 161 aufnimmt. Der innenliegende erste Lager-Aufnahmeabschnitt 330 weist eine zylindrische Innenform auf, und dient zur Aufnahme des ersten Lagers bzw. A-Lagers 360. Sowohl Pleuellager 160, 161 als auch erstes Lager bzw. A-Lager 380 und zweites Lager bzw. B-Lager 382 können an der Antriebswelle 220 auf verschiedene Weise befestigt werden. Insbesondere kann diese Befestigung formschlüssig geschehen, beispielsweise durch geeignete Befestigungselemente, kraftschlüssig durch Aufschrumpfen oder durch eine Kombination der vorher genannten oder weiteren Wirkprinzipien.The drive shaft 220 furthermore has, at an end PS on the connecting rod side, next to the outer connecting rod receiving section 320, an inner first bearing receiving section 380. The outer connecting rod receiving section 320 has a cylindrical outer shape which receives the inner ring of the connecting rod bearings 160, 161. The inner first bearing receiving section 330 has a cylindrical inner shape and is used to receive the first bearing or A-bearing 360. Both connecting rod bearings 160, 161 and the first bearing or A-bearing 380 and the second bearing or B-bearing 382 can be attached to the drive shaft 220 in a number of ways. In particular, this fastening can take place in a form-fitting manner, for example by means of suitable fastening elements, in a force-fitting manner by shrinking on, or by a combination of the aforementioned or other operating principles.

Das A-Lager 360 ist weiterhin über einen gestellfesten Achszapfen 450 mit dem Gehäuse 440 verbunden. Dies bedeutet, dass der Innenring des A-Lagers 360 ortsfest auf dem Achszapfen 450 befestigt ist, während der Außenring des A-Lagers 360 drehbar um die Drehachse A gelagert ist. Durch die Aufnahme des Außenrings des A-Lagers 360 im ersten Lager-Aufnahmeabschnitt 380 wird somit, zusammen mit der Lagerung durch das B-Lager 362 an einem pleuelfernen Ende PF der Antriebswelle 220, die Drehbewegung der Antriebswelle 220 ermöglicht. Der Achszapfen 450 ermöglicht hierbei besonders vorteilhaft ein möglichst direktes Einleiten von Pleuelkräften in die Wand des Gehäuses 440, ohne dass signifikante Biegemomente auftreten bzw. es zu signifikanten Verformungen durch auftretende Biegemomente kommt.The A-bearing 360 is also connected to the housing 440 via a journal 450 fixed to the frame. This means that the inner ring of the A-bearing 360 is fixed in place on the journal 450, while the outer ring of the A-bearing 360 is mounted rotatably about the axis of rotation A. By including the The outer ring of the A bearing 360 in the first bearing receiving section 380, together with the mounting by the B bearing 362 at an end PF of the drive shaft 220 remote from the connecting rod, enables the rotational movement of the drive shaft 220. The axle journal 450 particularly advantageously enables connecting rod forces to be introduced into the wall of the housing 440 as directly as possible, without significant bending moments or significant deformations occurring as a result of bending moments.

Tatsächlich auftretende Verformungen des Achszapfens 450 können durch eine entsprechende Dimensionierung des Achszapfens 450 insbesondere durch eine Vergrößerung des Achszapfen-Durchmessers AD und/oder eine Verkleinerung des Achszapfen-Hebels AH auf ein vernachlässigbares Niveau reduziert werden.Deformations of the journal 450 that actually occur can be reduced to a negligible level by appropriate dimensioning of the journal 450, in particular by increasing the journal diameter AD and / or reducing the journal lever AH.

Vorliegend sind das erste Pleuellager 160 in einer ersten Pleuelebene P1 und das zweite Pleuellager 161 in einer zweiten Pleuelebene P2 derartig zum A-Lager 360 angeordnet, dass sich die Lagerebene LE des A-Lagers 360 in axialer Richtung mittig zwischen den Pleuelebenen P1 und P2 befindet. Auf diese Weise wird gemäß dem Konzept der Erfindung vorteilhaft erreicht, dass unter Berücksichtigung sämtlicher im Betrieb in beiden Pleueln 140, 141 auftretenden Pleuelkräfte ein möglichst biegemomentarmer, insbesondere biegemomentfreier Zustand der Antriebswelle 220 erreicht wird.In the present case, the first connecting rod bearing 160 is arranged in a first connecting rod plane P1 and the second connecting rod bearing 161 in a second connecting rod plane P2 in relation to the A-bearing 360 in such a way that the bearing plane LE of the A-bearing 360 is axially centered between the connecting rod planes P1 and P2 . In this way, according to the concept of the invention, it is advantageously achieved that, taking into account all the connecting rod forces occurring in both connecting rods 140, 141 during operation, a state of drive shaft 220 that is as low in bending moment as possible, in particular free of bending moment, is achieved.

Tatsächlich treten aufgrund des Abstandes beider Pleuelebenen P1 und P2 weiterhin Biegemomente auf; jedoch stellt die mittige Positionierung des A-Lagers 360 in axialer Richtung mittig zwischen den Pleuelebenen P1 und P2 ein Optimum hinsichtlich der Minimierung von durch Pleuelkräfte hervorgerufenen Biegemomenten dar. Diese mittige Position ergibt sich aus der Annahme betragsmäßig nahezu gleicher Pleuelkräfte in beiden Pleueln 140, 141. Im Falle einer Abweichung der auftretenden Pleuelkräfte in einem der beiden Pleuel 140, 141 wäre zur Minimierung der Biegemomente das A-Lager 360 und somit die Lagerebene LE entsprechend axial in Richtung desjenigen Pleuellagers 160 oder 161 zu verschieben, an dem die größeren Pleuelkräfte aufgenommen werden.In fact, because of the distance between the two connecting rod planes P1 and P2, bending moments continue to occur; However, the central positioning of the A-bearing 360 in the axial direction between the connecting rod planes P1 and P2 represents an optimum in terms of minimizing the bending moments caused by connecting rod forces. This central position results from the assumption of almost identical connecting rod forces in both connecting rods 140, 141 In the event of a deviation in the connecting rod forces occurring in one of the two connecting rods 140, 141, the A-bearing 360 and thus the bearing plane LE would be correspondingly axially in the direction of that connecting rod bearing 160 in order to minimize the bending moments or 161 to move where the larger connecting rod forces are absorbed.

Zur Erzeugung einer oszillierenden Hubbewegung von Pleuel 140, 141 und Verdichterkolben 150, 151 ist der Pleuel-Aufnahmeabschnitt 320 exzentrisch zur Drehachse A der Antriebswelle 220 angeordnet. Das heißt, dass die auf der Drehachse A liegende Symmetrieachse des ersten Lager-Aufnahmeabschnitts 380 parallel, aber versetzt zu der auf der Exzenterachse Ex der Pleuellager 160, 161 liegenden Zylinderachse des zylindrischen Pleuel-Aufnahmeabschnittes 320 angeordnet ist.To generate an oscillating stroke movement of the connecting rod 140, 141 and the compressor piston 150, 151, the connecting rod receiving section 320 is arranged eccentrically to the axis of rotation A of the drive shaft 220. This means that the axis of symmetry of the first bearing receiving section 380 lying on the axis of rotation A is arranged parallel but offset to the cylinder axis of the cylindrical connecting rod receiving section 320 lying on the eccentric axis Ex of the connecting rod bearings 160, 161.

Die Antriebswelle 220 dient zur Übertragung der von einem Antrieb 200 erzeugten Drehbewegung auf die Pleuel 140, 141. Vorliegend wird die Antriebswelle 220 über einen Elektromotor 290 angetrieben.The drive shaft 220 serves to transmit the rotary movement generated by a drive 200 to the connecting rods 140, 141. In the present case, the drive shaft 220 is driven by an electric motor 290.

Gemäß dem Konzept der Erfindung ist das A-Lager 360 in axialer Richtung mittig zwischen den Pleuelebenen P1 und P2 angeordnet. Auf diese Weise werden auf die Antriebswelle 220 wirkende Biegemomente wesentlich reduziert, bzw. vermieden, da praktisch sämtliche Pleuelkräfte im Wesentlichen innerhalb der Lagerebene LE angreifen und somit praktisch kein oder nur ein geringer Hebelarm für ein auf die Antriebswelle 220 wirkendes Biegemoment entstehen kann.According to the concept of the invention, the A-bearing 360 is arranged in the axial direction centrally between the connecting rod planes P1 and P2. In this way, bending moments acting on the drive shaft 220 are significantly reduced or avoided, since practically all connecting rod forces act essentially within the bearing plane LE and thus practically no or only a small lever arm can arise for a bending moment acting on the drive shaft 220.

Bezugnehmend auf Fig. 2A bis Fig. 2C ist vorliegend schematisch eine Situation mit einem einzigen Pleuellager 260' und einem einzigen Antriebswellenlager 260 gezeigt. Diese Situation steht symbolisch auch für eine in Fig. 1 oder Fig. 3 dargestellte Ausführungsform. Insofern steht das Pleuellager 260' der Fig. 2 symbolisch für eine Pleuellager-Anordnung 160, 161 der Fig. 1 oder Fig. 3 und das Antriebswellenlager 260 der Fig. 2 symbolisch für eine Antriebswellenlager-Anordnung 360 der Fig. 1 oder Fig. 3.Referring to Figures 2A to 2C a situation with a single connecting rod bearing 260 ′ and a single drive shaft bearing 260 is shown schematically in the present case. This situation also symbolizes an in Fig. 1 or Fig. 3 illustrated embodiment. In this respect, the connecting rod bearing 260 'stands Fig. 2 symbolic of a connecting rod bearing arrangement 160, 161 of the Fig. 1 or Fig. 3 and the drive shaft bearing 260 of FIG Fig. 2 symbolic of a drive shaft bearing assembly 360 of Fig. 1 or Fig. 3 .

In Fig. 2A ist eine Weiterbildung dargestellt, in der sich das Pleuellager 260' und Antriebswellenlager 260 teilweise überdecken. Dies bedeutet, dass das Antriebswellenlager 260 in axialer Richtung derartig entlang der Drehachse A in Richtung des Pleuellagers 260' verschoben ist, dass es sich teilweise innerhalb des Pleuellager-Innenraums 190 befindet. Diese Verschiebung --vorliegend in Richtung des Antriebs 200 gemäß der Fig. 1 (in der Fig. 2A, Fig. 2B nach rechts)-- wird beschrieben durch einen axialen Abstand SA zwischen der axialen Mittenebene EP des Pleuellagers 260' und der axialen Mittenebene EA des Antriebswellenlagers 260. Diese Verschiebung kann in einer alternativen Abwandlung auch in Richtung weg vom Antrieb 200 gemäß der Fig. 1 umgesetzt werden (in der Fig. 2A, Fig. 2B wäre das dann nach links).In Figure 2A a further development is shown in which the connecting rod bearing 260 'and drive shaft bearing 260 partially overlap. This means that the driveshaft bearing 260 is shifted in the axial direction along the axis of rotation A in the direction of the connecting rod bearing 260 ′ such that it is partially located within the connecting rod bearing interior 190. This shift - present in the direction of the drive 200 according to FIG Fig. 1 (in the Figures 2A, 2B to the right) - is described by an axial distance SA between the axial center plane EP of the connecting rod bearing 260 'and the axial center plane EA of the drive shaft bearing 260. This shift can in an alternative modification also in the direction away from the drive 200 according to FIG Fig. 1 implemented (in the Figures 2A, 2B that would then be to the left).

Je größer der axiale Abstand SA gewählt wird, desto größer sind die auf die Antriebswelle 220 wirkenden und durch Pleuelkräfte hervorgerufenen Biegemomente, welche gemäß dem Konzept der Erfindung vermindert bzw. vermieden werden sollen.The larger the axial distance SA is chosen, the larger the bending moments acting on the drive shaft 220 and caused by connecting rod forces, which according to the concept of the invention are to be reduced or avoided.

Als Überdeckung UD wird hier derjenige axiale Abstand bezeichnet, mit dem das Antriebswellenlager 260 in den Pleuellager-Innenraum 190 hineinragt. Die Überdeckung UD ergibt sich in der in Fig. 2A ersichtlichen Ausführungsform, aus der Breite BP des Pleuellagers 260', der Breite BA des Antriebswellenlagers 260 und dem axialen Abstand SA.The axial distance with which the drive shaft bearing 260 protrudes into the connecting rod bearing interior 190 is referred to here as the overlap UD. The UD overlap results from the in Figure 2A apparent embodiment, from the width BP of the connecting rod bearing 260 ', the width BA of the drive shaft bearing 260 and the axial distance SA.

In der in Fig. 2A dargestellten Weiterbildung ist die Überdeckung UD vergleichsweise gering, insbesondere ragt das Antriebswellenlager 260 weniger mit einem Abstand UD in den Pleuellager-Innenraum 190 hinein, der geringer ist als die Hälfte seiner axialen Breite BA. Dieser Fall einer "einfachen" Überdeckung UD lässt sich durch folgenden Zusammenhang ausdrücken: UD < 0,5*BA.In the in Figure 2A The further development shown, the overlap UD is comparatively small, in particular the drive shaft bearing 260 protrudes less into the connecting rod bearing interior 190 at a distance UD that is less than half its axial width BA. This case of a "simple" overlap UD can be expressed by the following relationship: UD <0.5 * BA.

Das Konzept der Erfindung kann -jedenfalls grundsätzlich, wenn auch nicht bevorzugt-- in einer anderen hier nicht gezeigten Ausführungsform realisiert werden wenn keine Überdeckung stattfindet. Es zeigt sich, dass dies jedenfalls in der hier nicht gezeigten Ausführungsform hinnehmbar wäre solange der axiale Abstand SA ausreichend gering ist, um einen Hebelarm für auf die Antriebswelle 220 wirkende und durch Pleuelkräfte hervorgerufene Biegemomente zu vermeiden. Als Richtwert für einen maximalen axialen Abstand SA wird der Wert SA = BP + BA angesehen.The concept of the invention can - in any case in principle, even if not preferred - be implemented in another embodiment, not shown here, if there is no overlap. It turns out that this would be acceptable in any case in the embodiment not shown here as long as the axial distance SA is sufficiently small to allow a lever arm for the drive shaft 220 acting bending moments caused by connecting rod forces. The value SA = BP + BA is regarded as a guide value for a maximum axial distance SA.

In Fig. 2B ist eine weitere mögliche Anordnung von Pleuellager 260' und Antriebswellenlager 260 dargestellt. Hierbei ist wesentlich, dass die in der in Fig. 2B ersichtlich variierte Überdeckung UD' der Ausführungsform der Fig. 2B größer ist als die Überdeckung UD der in Fig. 2A dargestellten Weiterbildung. Das Antriebswellenlager 260 ragt infolge einer insofern vergrößerten Überdeckung UD' in den Pleuellager-Innenraum 190 hinein, wobei die vergrößerte Überdeckung UD' größer ist als die Hälfte der axialen Breite BA des Antriebswellenlagers 260. Dieser Fall der vergrößerten und insofern "überwiegenden" Überdeckung UD' lässt sich durch folgenden Zusammenhang ausdrücken: 0,5*BA < UD' < BA.In Figure 2B a further possible arrangement of connecting rod bearing 260 'and drive shaft bearing 260 is shown. Here it is essential that the in Figure 2B apparent varied coverage UD 'of the embodiment of Figure 2B is greater than the UD coverage of the in Figure 2A illustrated training. The drive shaft bearing 260 protrudes into the connecting rod bearing interior 190 as a result of an enlarged overlap UD ', the enlarged overlap UD' being greater than half the axial width BA of the drive shaft bearing 260. This case of the enlarged and, in this respect, "predominant" overlap UD ' can be expressed using the following relationship: 0.5 * BA <UD '<BA.

Für die hier dargestellte Weiterbildung gilt ebenfalls, dass der axialer Abstand SA im Vergleich zu der in Fig. 2A dargestellten Weiterbildung, verkleinert ist. Dies hat vorteilhaft zur Folge, dass der Hebelarm für auf die Antriebswelle 220 und durch Pleuelkräfte verursachte Biegemomente, gemäß dem Konzept der Erfindung ebenfalls verkleinert ist.For the development shown here it also applies that the axial distance SA compared to that in Figure 2A illustrated training, is reduced in size. This advantageously has the consequence that the lever arm for bending moments caused on the drive shaft 220 and by connecting rod forces is also reduced in accordance with the concept of the invention.

Fig. 2C zeigt schließlich eine dritte mögliche Lageranordnung, bei der besonders vorteilhaft die axiale Mittenebene EP des Pleuellagers 260' und die axiale Mittenebene EA des Antriebswellenlagers 260 in einer Lagerebene E zusammenfallen. Dies bedeutet, dass der axialer Abstand SA gleich null ist und somit praktisch kein Hebelarm für aus dem Pleuel 140 in die Antriebswelle 220 geleitete Kräfte besteht. Auf diese Weise wird besonders vorteilhaft gemäß dem Konzept der Erfindung eine Entstehung von Biegemomenten vermieden. Die Tatsache, dass das Antriebswellenlager 260 in axialer Richtung derart angeordnet ist, dass es sich vollständig im Pleuellager-Innenraum 190 befindet, führt zu einer nochmals ersichtlich vergrößerten, nämlich "vollständigen" Überdeckung UD", das heißt: UD" = BA. Figure 2C Finally, shows a third possible bearing arrangement in which the axial center plane EP of the connecting rod bearing 260 'and the axial center plane EA of the drive shaft bearing 260 coincide in a bearing plane E particularly advantageously. This means that the axial distance SA is equal to zero and thus there is practically no lever arm for forces conducted from the connecting rod 140 into the drive shaft 220. In this way, according to the concept of the invention, the creation of bending moments is avoided in a particularly advantageous manner. The fact that the drive shaft bearing 260 is arranged in the axial direction in such a way that it is located completely in the connecting rod bearing interior 190 leads to a clearly enlarged, namely "complete" overlap UD ", that is to say: UD" = BA.

Fig. 3A - Fig. 3D zeigen unterschiedliche Anordnungen von A-Lager und Pleuellager bzw. Pleuellagern gemäß dem Konzept der Erfindung. Figures 3A-3D show different arrangements of A-bearings and connecting rod bearings or connecting rod bearings according to the concept of the invention.

In Fig. 3A ist eine Lageranordnung gemäß einer Weiterbildung dargestellt, in der sich A-Lager 360 und Pleuellager 160 in axialer Richtung praktisch genau überdecken. Dies bedeutet, dass Lagerebene LE und Pleuelebene P in einer Ebene zusammenfallen. Folglich ist der Lagerabstand LA zwischen A-Lager 360 und Pleuellager 160 gleich null. Hieraus resultiert, dass von einem hier nicht näher dargestellten Pleuel 140 über das Pleuellager 160 auf den Pleuelaufnahmeabschnitt 320 der Antriebswelle 220 eingeleitete Pleuelkraft FP direkt, insbesondere biegemomentfrei, auf das A-Lager 360 und somit über den Achszapfen 450 in die Wand des Gehäuses 440 übertragen wird.In Figure 3A shows a bearing arrangement according to a development in which A-bearing 360 and connecting rod bearing 160 practically exactly overlap in the axial direction. This means that the bearing level LE and the connecting rod level P coincide in one level. Consequently, the bearing distance LA between A-bearing 360 and connecting rod bearing 160 is equal to zero. As a result, the connecting rod force FP introduced from a connecting rod 140, not shown here, via the connecting rod bearing 160 to the connecting rod receiving section 320 of the drive shaft 220 is transmitted directly, in particular without bending moment, to the A-bearing 360 and thus via the journal 450 into the wall of the housing 440 becomes.

In Fig. 3B ist eine Lageranordnung gemäß einer weiteren Weiterbildung der Erfindung dargestellt. In dieser ist das Pleuellager 160 auf dem Pleuel-Aufnahmeabschnitt 320 und das A-Lager 360 in dem A-Lager Aufnahmeabschnitt 380 derartig angeordnet, dass ein Versatz in axialer Richtung zwischen Pleuellager 160 und A-Lager 360 besteht. Folglich liegen Pleuelebene P des Pleuellagers 160 und Lagerebene LE des A-Lagers 360 in axialer Richtung in einem Lagerabstand LA parallel zueinander entfernt. Hieraus resultiert insbesondere, dass ein durch die Pleuelkräfte hervorgerufenes Biegemoment, welches sich aus der Pleuelkraft FP und einem Hebelarm mit der Länge LA bildet, auf den Pleuelaufnahmeabschnitt 320 der Antriebswelle 220 wirkt. Eine derartige Lageranordnung kann in vorteilhafter Weise dazu genutzt werden, eine durch ein Biegemoment hervorgerufene Verformung des Achszapfens 450 durch eine mittels des Lagerabstandes LA gezielt hervorgerufene Verformung der Antriebswelle 220 zu kompensieren. Dass dabei auf den Achszapfen 450 wirkende Biegemoment ergibt sich aus der auf das A-Lager 360 wirkenden Lagerkraft sowie dem Achszapfen-Hebel AH. Dieser Zusammenhang ist im Folgenden in Fig. 4 näher erläutert.In Figure 3B shows a bearing arrangement according to a further development of the invention. In this, the connecting rod bearing 160 is arranged on the connecting rod receiving section 320 and the A bearing 360 in the A bearing receiving section 380 in such a way that there is an offset in the axial direction between the connecting rod bearing 160 and the A bearing 360. Consequently, the connecting rod plane P of the connecting rod bearing 160 and the bearing plane LE of the A-bearing 360 lie parallel to one another in the axial direction at a bearing spacing LA. This results in particular that a bending moment caused by the connecting rod forces, which is formed from the connecting rod force FP and a lever arm with the length LA, acts on the connecting rod receiving section 320 of the drive shaft 220. Such a bearing arrangement can advantageously be used to compensate for a deformation of the axle journal 450 caused by a bending moment by a deformation of the drive shaft 220 specifically caused by the bearing spacing LA. The bending moment acting on the journal 450 results from the bearing force acting on the A-bearing 360 and the journal lever AH. This connection is shown below in Fig. 4 explained in more detail.

In Fig. 3C ist eine Lageranordnung gemäß einer weiteren Weiterbildung der Erfindung beispielhaft dargestellt. In dieser Weiterbildung handelt es sich um einen Verdichter mit hier nicht dargestellten zwei Zylindern 170, 171 und entsprechend zwei hier ebenfalls nicht dargestellten Pleuel 140,141. Die entsprechenden Pleuellager 160,161 sind vorliegend axial nebeneinander auf dem Pleuelaufnahmeabschnitt 320 angeordnet. Das A-Lager 360 ist dazu derartig innerhalb des A-Lager Aufnahmeabschnittes 180 sowie auf dem Achszapfen 450 angeordnet, dass die Lagerebene LE in axialer Richtung mittig zwischen den Pleuelebenen P1, P2 liegt. Wie bereits im Zusammenhang mit Fig. 1 beschrieben, stellt die mittige Anordnung des A-Lagers 360 in axialer Richtung zwischen den Pleuellagern 160, 161 einen Kompromiss zur Minimierung der durch Pleuelkräfte FP1, FP2 hervorgerufenen Biegemomenten dar, da aufgrund der Anordnung der Pleuelebenen P1 und P2 außerhalb der Lagerebene LG keine vollständig biegemomentfreie Lagerung der Antriebswelle 220 möglich ist. Vorliegend ist das erste Pleuellager 160 um einen ersten Lagerabstand LA1 in negativer axialer Richtung, d.h. in Richtung der Wand des Gehäuses 440, an welcher der Achszapfen 450 befestigt ist, verschoben angeordnet. Weiterhin ist das zweite Pleuellager 161 um einen zweiten Lagerabstand LA2, der vorliegend betragsmäßig gleich dem ersten Lagerabstand LA1 ist, in positiver axialer Richtung, d. h. in Richtung des freistehenden Stirnendes des Achszapfens 450, angeordnet.In Figure 3C a bearing arrangement according to a further development of the invention is shown by way of example. This training is about a compressor with two cylinders 170, 171, not shown here, and correspondingly two connecting rods 140, 141, also not shown here. In the present case, the corresponding connecting rod bearings 160, 161 are arranged axially next to one another on the connecting rod receiving section 320. For this purpose, the A-bearing 360 is arranged within the A-bearing receiving section 180 and on the axle journal 450 such that the bearing plane LE lies centrally in the axial direction between the connecting rod planes P1, P2. As in connection with Fig. 1 described, the central arrangement of the A-bearing 360 in the axial direction between the connecting rod bearings 160, 161 represents a compromise for minimizing the bending moments caused by connecting rod forces FP1, FP2, since due to the arrangement of the connecting rod planes P1 and P2 outside the bearing plane LG it is not completely free of bending moments Storage of the drive shaft 220 is possible. In the present case, the first connecting rod bearing 160 is arranged displaced by a first bearing spacing LA1 in the negative axial direction, that is to say in the direction of the wall of the housing 440 on which the journal 450 is attached. Furthermore, the second connecting rod bearing 161 is arranged in the positive axial direction, ie in the direction of the free end of the journal 450, by a second bearing spacing LA2, which in this case is equal to the first bearing spacing LA1 in terms of amount.

In Fig. 3D ist eine Lageranordnung gemäß einer noch weiteren Weiterbildung der Erfindung dargestellt. Hierbei ist, im Unterschied zu der in Fig. 2C dargestellten Weiterbildung, das A-Lager 360 in Bezug zu den Pleuellager 160, 161 derartig angeordnet, dass die Lagerabstände LA1 und LA2 jeweils unterschiedlich groß sind. Hieraus kann, im Falle betragsmäßig etwa gleich belasteter Pleuel 140, 141, dass eine aus beiden Pleuel 140, 141 und somit beiden Pleuellagern 160, 161 in die Antriebswelle 220 geleitete, resultierende Gesamtpleuelkraft im Wesentlichen nicht innerhalb der Lagerebene E angreift. Die hierdurch entstehende, gezielt hervorgerufene Verformung kann, analog zu der in Fig. 3B beschriebenen Lageranordnung, zur Kompensation der Verformung des Achszapfens 450 genutzt werden.In Figure 3D shows a bearing arrangement according to yet another development of the invention. In contrast to the in Figure 2C Further development shown, the A-bearing 360 is arranged in relation to the connecting rod bearings 160, 161 in such a way that the bearing distances LA1 and LA2 are each of different sizes. In the case of connecting rods 140, 141 that are approximately equally loaded in terms of amount, this means that one of the resulting total connecting rod forces conducted into drive shaft 220 from both connecting rods 140, 141 and thus both connecting rod bearings 160, 161 does not essentially act within bearing plane E. The resulting, deliberately induced deformation can, analogous to that in Figure 3B Bearing arrangement described, can be used to compensate for the deformation of the journal 450.

Alternativ kann weiterhin, für den Fall, dass ein Pleuel stärker belastet wird als das andere Pleuel, eine in Fig. 3D gezeigte Lageranordnung zu Berücksichtigung und Kompensation dieses Umstandes gezielt eingesetzt werden. Vorliegend wird beispielsweise angenommen, dass die auf das zweite Pleuellager 161 wirkende Pleuelkraft FP2 größer ist als auf das erste Pleuellager 160 wirkende Pleuelkraft FP1. Folglich wird die axiale Position des A-Lagers 360 in Richtung des stärker belasteten Pleuellagers, in diesem Falle das Pleuellager 161, verschoben, so dass der zweite Lagerabstand LA2 kleiner als der erste Lagerabstand LA1 ist. Hierdurch wird erreicht, dass die größere, auf das Pleuellager 161 wirkende Pleuelkraft FP2 die Antriebswelle 220 in einer Pleuelebene P2 angreift, die insbesondere so nah an der Lagerebene LE liegt dass die resultierenden Biegemomente keine kritische Verformung der Antriebswelle 220 hervorruft. Unter kritischer Verformung wird in diesem Kontext eine Verformung genannt, die direkt oder indirekt zu einem oder mehreren der eingangs erwähnten Nachteile, insbesondere hinsichtlich Geräusch- und Vibrationsentwicklung sowie Verschleißverhalten, führt.Alternatively, in the event that one connecting rod is more heavily loaded than the other connecting rod, an in Figure 3D Bearing arrangement shown can be used specifically to take into account and compensate for this fact. It is assumed here, for example, that the connecting rod force FP2 acting on the second connecting rod bearing 161 is greater than the connecting rod force FP1 acting on the first connecting rod bearing 160. Consequently, the axial position of the A-bearing 360 is shifted in the direction of the more heavily loaded connecting rod bearing, in this case the connecting rod bearing 161, so that the second bearing spacing LA2 is smaller than the first bearing spacing LA1. This ensures that the larger connecting rod force FP2 acting on the connecting rod bearing 161 engages the drive shaft 220 in a connecting rod plane P2 which, in particular, is so close to the bearing plane LE that the resulting bending moments do not cause any critical deformation of the drive shaft 220. In this context, critical deformation refers to a deformation that leads directly or indirectly to one or more of the disadvantages mentioned at the beginning, in particular with regard to noise and vibration development as well as wear behavior.

Fig. 4 zeigt in einer schematischen Darstellung eine Durchbiegung von einer Antriebswelle 220 und einem Achszapfen 450. In dieser stark vereinfachten Darstellung sind die Verformungen übertrieben dargestellt. Eine Pleuelkraft FP, die auf das Pleuellager 160 angreift, wird auf die Antriebswelle 220 und somit auf das A Lager 360 übertragen. Über das A-Lager 360 wird diese Kraft schließlich in den Achszapfen 450 geleitet, wo sie aufgrund des Abstandes zwischen Gehäuse 440 und A-Lager 360 zu einem Biegemoment führt, welches wiederum eine Verformung des Achszapfens 450, nämlich eine Zapfenauslenkung ZA, zur Folge hat. Gleichzeitig wird durch die Anordnung von A-Lager 360 und Pleuellager 160, insbesondere durch die Anordnung von A-Lager 360 und Pleuellager 160 in einem axialen Lagerabstand LA, erreicht, dass auf die Antriebswelle 220 ein Biegemoment wirkt. Dieses Biegemoment ist dem auf den Achszapfen wirkenden Biegemoment entgegengerichtet. Hierdurch wird in vorteilhafter Weise erreicht, dass die Antriebswelle 220 derart verformt wird, dass auf das B-Lager 362 möglichst geringe Kräfte, insbesondere Querkräfte und Kippmomente, wirken. Durch das Verformen der Antriebswelle 220 wird somit die Zapfenauslenkung ZA teilweise oder vollständig kompensiert. Fig. 4 shows in a schematic representation a deflection of a drive shaft 220 and an axle journal 450. In this greatly simplified representation, the deformations are shown exaggerated. A connecting rod force FP that acts on the connecting rod bearing 160 is transmitted to the drive shaft 220 and thus to the A bearing 360. This force is finally conducted via the A-bearing 360 into the journal 450, where it leads to a bending moment due to the distance between the housing 440 and the A-bearing 360, which in turn results in a deformation of the journal 450, namely a pin deflection ZA . At the same time, the arrangement of A-bearing 360 and connecting rod bearing 160, in particular the arrangement of A-bearing 360 and connecting rod bearing 160 at an axial bearing spacing LA, ensures that a bending moment acts on drive shaft 220. This bending moment is opposite to the bending moment acting on the stub axle. This advantageously ensures that the drive shaft 220 is deformed in such a way that the forces acting on the B-bearing 362 are as small as possible, in particular transverse forces and Overturning moments act. The deformation of the drive shaft 220 thus partially or completely compensates for the pin deflection ZA.

Fig. 5 zeigt eine stark vereinfachte, schematische Übersicht einer Druckluftversorgungsanlage 500 mit einer Verdichteranordnung 1000 gemäß dem Konzept der Erfindung zur Versorgung einer Pneumatikanlage 600. Die Druckluftversorgungsanlage 500 weist eine Luftansaugung 0 zum Ansaugen von Frischluft auf, die weiterhin mit einem Einlass des Verdichters 100 fluidführend, insbesondere gasführend, verbunden ist. Der Verdichter 100 wird als Teil der Verdichteranordnung 1000 von einem Antrieb 200 über eine Antriebswelle 220 angetrieben. Die verdichtete Frischluft wird weiterhin über eine Druckluftquelle 1 bereitgestellt, an welche sich eine Abzweigung 510 anschließt. An diese Abzweigung 510 ist zum einen, über ein Entlüftungsventil 520, eine Entlüftung 3 angeschlossen. Zum anderen ist an die Abzweigung 510 ein Lufttrockner 520 angeschlossen, der weiterhin zu einem Druckluftanschluss 2 führt. An diesen sind weiterhin über eine Galerie 570 ein Druckluftspeicher 560 und die Pneumatikanlage 600 angeschlossen. Die Pneumatikanlage 600 kann beispielsweise eine Luftfederanlage, oder eine weitere pneumatische Anlage, insbesondere eine Fahrzeugs, sein. Weiterhin sind einzelne Ventile, Drosseln und dergleichen Stellmittel sowie einzelne Komponenten, insbesondere der Pneumatikanlage, in dieser Darstellung aus Gründen der Übersicht und Vereinfachung nicht dargestellt. Fig. 5 shows a greatly simplified, schematic overview of a compressed air supply system 500 with a compressor arrangement 1000 according to the concept of the invention for supplying a pneumatic system 600. The compressed air supply system 500 has an air intake 0 for sucking in fresh air, which continues to carry fluid, in particular gas, with an inlet of the compressor 100 , connected is. As part of the compressor arrangement 1000, the compressor 100 is driven by a drive 200 via a drive shaft 220. The compressed fresh air is also made available via a compressed air source 1, to which a branch 510 is connected. On the one hand, a vent 3 is connected to this junction 510 via a vent valve 520. On the other hand, an air dryer 520 is connected to the junction 510, which also leads to a compressed air connection 2. A compressed air reservoir 560 and the pneumatic system 600 are also connected to this via a gallery 570. The pneumatic system 600 can, for example, be an air suspension system or another pneumatic system, in particular a vehicle. Furthermore, individual valves, throttles and similar adjusting means as well as individual components, in particular the pneumatic system, are not shown in this illustration for reasons of clarity and simplicity.

Fig. 6 zeigt eine schematische Darstellung eines Fahrzeugs 800 -vorliegend in Form eines PKW-- mit einer Druckluftversorgungsanlage 500 und einer Pneumatikanlage 600. Bei Fahrzeugen im PKW-Bereich ist ein geräusch- und vibrationsarmer Betrieb von großer Bedeutung, da hier, im Unterschied zu Anwendungen im LKW-Bereich, die Akustikanforderungen höher bzw. sensibler sind. Das hier deswegen, ohne Einschränkung der Anwendbarkeit auch für LKW'S oder andere Nutzfahrzeuge, beispielhaft dargestellte PKW-Fahrzeug 800 verfügt über vier Räder 801, 802, 803 und 804, von denen hier aufgrund der Schnittdarstellung die zwei jeweils vorderen Räder gezeigt sind. Analog zur Anzahl der Räder verfügt die Pneumatikanlage 600 über vier Luftfedern 601, 602, 603 und 604, von denen hier analog zu den Rädern aufgrund der Schnittdarstellung die zwei jeweils vorderen Luftfedern gezeigt sind. Die Luftfedern 601, 602, 603 und 604, die jeweils den Rädern 801, 802, 803 und 804 zugeordnet sind, werden als Teil der Pneumatikanlage 600 von der Druckluftversorgungsanlage 500 mit Druckluft versorgt. Die Druckluftversorgungsanlage 500 ist über die Galerie 570 mit den Komponenten der Pneumatikanlage 600, in diesem Falle den hier dargestellten Luftfedern 601, 602, 603 und 604, fluidführend verbunden. Fig. 6 shows a schematic representation of a vehicle 800 - in the present case in the form of a car - with a compressed air supply system 500 and a pneumatic system 600. In vehicles in the passenger car sector, low-noise and low-vibration operation is of great importance because here, in contrast to applications in trucks -Area, the acoustic requirements are higher or more sensitive. The car vehicle 800 shown here by way of example, without restricting its applicability for trucks or other commercial vehicles, has four wheels 801, 802, 803 and 804, of which the two front wheels are shown here due to the sectional view. Analogous to the number of wheels, the pneumatic system 600 has four air springs 601, 602, 603 and 604, of which the two front air springs are shown here analogously to the wheels due to the sectional view. The air springs 601, 602, 603 and 604, which are respectively assigned to the wheels 801, 802, 803 and 804, are supplied with compressed air from the compressed air supply system 500 as part of the pneumatic system 600. The compressed air supply system 500 is connected in a fluid-conducting manner via the gallery 570 to the components of the pneumatic system 600, in this case the air springs 601, 602, 603 and 604 shown here.

Die Druckluftversorgungsanlage 500 ist in dieser Darstellung stark vereinfacht zeigt, so dass lediglich der Druckluftspeicher 560 und der Verdichter 100 gemäß dem Konzept der Erfindung sichtbar ist. Der Verdichter 100 gemäß dem Konzept der Erfindung könnt allerdings in einer hier nicht gezeigten Abwandlung zusätzlich oder alternativ unabhängig von der Druckluftversorgungsanlage eingesetzt werden. Das Konzept bietet vorzugsweise die Basis für eine in verbesserter Weise funktionierende, insbesondere vibrations- und geräuscharme Verdichteranordnung. Weiterhin führen eine Reduzierung von Kräften und/oder Momenten sowie insbesondere eine Reduzierung der mit den Kräften und/oder Momenten verbundenen dynamischen Belastungen und Vibrationen, zu einer schonenderen Betriebsweise, welche sich auf Effizienz und Langlebigkeit der Verdichteranordnung positiv auswirken.The compressed air supply system 500 is shown greatly simplified in this illustration, so that only the compressed air reservoir 560 and the compressor 100 according to the concept of the invention are visible. The compressor 100 according to the concept of the invention can, however, in a modification not shown here, additionally or alternatively be used independently of the compressed air supply system. The concept preferably offers the basis for a compressor arrangement that functions in an improved manner, in particular a low-vibration and low-noise compressor arrangement. Furthermore, a reduction in forces and / or moments and, in particular, a reduction in the dynamic loads and vibrations associated with the forces and / or moments lead to a gentler mode of operation, which has a positive effect on the efficiency and longevity of the compressor arrangement.

Bezugszeichenliste (Bestandteil der Beschreibung)List of reference symbols (part of the description)

00
LuftansaugungAir intake
11
DruckluftquelleCompressed air source
22
DruckluftanschlussCompressed air connection
33
EntlüftungVenting
100100
Verdichtercompressor
140140
Erstes PleuelFirst connecting rod
141141
Zweites PleuelSecond connecting rod
150150
Erster VerdichterkolbenFirst compressor piston
151151
Zweiter VerdichterkolbenSecond compressor piston
160160
Erstes PleuellagerFirst connecting rod bearing
161161
Zweites PleuellagerSecond connecting rod bearing
170170
Erster ZylinderFirst cylinder
171171
Zweiter ZylinderSecond cylinder
164164
ToleranzringTolerance ring
200200
Antriebdrive
220220
Antriebswelledrive shaft
290290
ElektromotorElectric motor
320320
Pleuel-AufnahmeabschnittConnecting rod receiving section
360360
Erstes Lager, Pleuelseitiges Antriebswellenlager (A-Lager)First bearing, connecting rod end drive shaft bearing (A bearing)
362362
Zweites Lager, Pleuelfernes Antriebswellenlager (B-Lager)Second bearing, drive shaft bearing remote from the connecting rod (B bearing)
370370
Hohlraumcavity
380380
Erster Lager-Aufnahmeabschnitt (A-Lager-)First bearing receiving section (A-bearing)
382382
Zweiter Lager-Aufnahmeabschnitt (B-Lager-)Second bearing receiving section (B-bearing)
440440
Gehäusecasing
450450
AchszapfenJournal
500500
DruckluftversorgungsanlageCompressed air supply system
510510
AbzweigungJunction
520520
EntlüftungsventilVent valve
540540
LufttrocknerAir dryer
560560
DruckluftspeicherCompressed air storage
600600
PneumatikanlagePneumatic system
601, 602, 603, 604601, 602, 603, 604
LuftfederAir spring
800800
Fahrzeugvehicle
801,802,803,804801,802,803,804
Radwheel
10001000
VerdichteranordnungCompressor arrangement
AA.
Drehachse der AntriebswelleAxis of rotation of the drive shaft
ADAD
Achszapfen-DurchmesserAxle journal diameter
AHAH
Achszapfen-HebelJournal lever
ExEx
ExzenterachseEccentric axis
FPFP
PleuelkraftConnecting rod force
FP1FP1
Erste PleuelkraftFirst connecting rod force
FP2FP2
Zweite PleuelkraftSecond connecting rod force
HH
Hubweg des VerdichterkolbensStroke of the compressor piston
LALA
LagerabstandBearing spacing
LA1LA1
Erster LagerabstandFirst bearing clearance
LA2LA2
Zweiter LagerabstandSecond bearing spacing
MM.
Mittenebene, axiale Mittenebene des A-LagersCenter plane, axial center plane of the A bearing
P1P1
Erste PleuelebeneFirst connecting rod level
P2P2
Zweite PleuelebeneSecond connecting rod level
PFPF
pleuelfernes Ende der Antriebswelleend of the drive shaft remote from the connecting rod
PSPS
pleuelseitiges Ende der Antriebswelleend of the drive shaft on the connecting rod side
WAWA
Wellenauslenkung, Auslenkung der AntriebswelleShaft deflection, deflection of the drive shaft
ZAZA
Zapfenauslenkung, Auslenkung des AchszapfensPin deflection, deflection of the journal
BABA
Antriebswellenlager-BreiteDrive shaft bearing width
BPBP
Pleuellager-BreiteBig end bearing width
DAADAA
Antriebswellenlager-AußendurchmesserDrive shaft bearing outer diameter
DIASLIDE
Antriebswellenlager-InnendurchmesserDrive shaft bearing inside diameter
DAPDAP
Pleuellager-AußendurchmesserBig end bearing outer diameter
DIPDIP
Pleuellager-InnendurchmesserConnecting rod bearing inside diameter
EE.
LagerebeneStorage level
EAEA
Axiale Mittenebene des AntriebswellenlagersAxial center plane of the drive shaft bearing
EPEP
Axiale Mittenebene des PleuellagersAxial center plane of the connecting rod bearing
UDUD
einfache Überdeckungsimple overlap
UD'UD '
überwiegende Überdeckungpredominant overlap
UD"UD "
vollständige Überdeckungcomplete coverage

Claims (17)

  1. Compressor assembly (1000) for a compressed-air feed of a compressed-air supply system, for operating a pneumatic system (600), having:
    - a compressor (100) having at least one cylinder (170, 171) and at least one connecting rod (140, 141) in a connecting-rod plane (P, P1, P2), wherein the at least one connecting rod further has a compressor piston (150, 151) and at least one connecting-rod bearing (160, 161),
    - a drive (200) having an axis of rotation (A) and a drive shaft (220), and also a housing (440), wherein the drive shaft (220) is mounted in at least one drive shaft bearing (360) and has a connecting-rod-side end (PS) and a connecting-rod-remote end (PF), and
    - the drive shaft (220) has a connecting-rod-receiving portion (320) which is arranged eccentrically to the axis of rotation (A) of the drive (200) at the connecting-rod-side end (PS),
    characterized in that
    - the at least one drive shaft bearing (360) and the at least one connecting-rod bearing (160, 161) are arranged in such a way that the at least one drive shaft bearing (360) is situated at least partially within the at least one connecting-rod bearing (160, 161) in the radial direction.
  2. Compressor assembly (1000) according to Claim 1, characterized in that
    - the drive shaft (220) is mounted in a connecting-rod-side drive shaft bearing, which is arranged at the connecting-rod-side end (PS) of the drive shaft (220) in a bearing plane (LE), as first bearing (360, A bearing) on a first bearing-receiving portion (380) arranged coaxially to the axis of rotation (A).
  3. Compressor assembly (1000) according to Claim 1 or 2, characterized in that
    - the drive shaft (220) is mounted in a connecting-rod-remote drive shaft bearing, which is arranged at the connecting-rod-remote end (PF) of the drive shaft (220), as second bearing (362, B bearing) on a second bearing-receiving portion (382) arranged coaxially to the axis of rotation (A) at the connecting-rod-remote end (PF).
  4. Compressor assembly (1000) according to one of the preceding claims, characterized in that the bearings (360, 362) are arranged within and/or on the housing (440) .
  5. Compressor assembly (1000) according to one of the preceding claims, characterized in that
    - the first bearing-receiving portion (380) for receiving the first bearing (360) is designed as a cylindrical cavity (370), and/or
    - the first bearing (360) is further fastened on a journal (450) which is connected to the housing (440) in a frame-fixed manner and which is arranged practically coaxially to the axis of rotation (A), wherein
    - the first bearing (360) is seated in the cylindrical cavity (370) between the first bearing-receiving portion (380) and the journal (450).
  6. Compressor assembly (1000) according to one of the preceding claims, characterized in that the first bearing (360) is seated fixedly on the journal (450) and firmly seated in the first bearing-receiving portion (380) and connects the journal (450) and the first bearing-receiving portion (380) such that they can be rotated relative to one another.
  7. Compressor assembly (1000) according to one of the preceding claims, characterized in that the compressor (100) has a plurality of connecting rods, in particular a first and a second connecting rod (140, 141).
  8. Compressor assembly (1000) according to one of the preceding Claim 6 or 7, characterized in that the first connecting rod (140) and the second connecting rod (141) are arranged in such a way that the first connecting rod (140) is arranged at a first bearing distance (LA1) and the second connecting rod (141) is arranged at a second bearing distance (LA2) in the axial direction, i.e. in the direction of the axis of rotation (A), from the bearing plane (LE).
  9. Compressor assembly (1000) according to Claim 6 or 7, characterized in that the first and the second connecting rod (140, 141) are arranged in such a way that the bearing plane (LE) is situated in the axial direction centrally between a first connecting-rod plane (P1) and a second connecting-rod plane (P2).
  10. Compressor assembly (1000) according to one of the preceding claims, characterized in that the compressor has a first connecting rod (140) which is arranged in the bearing plane (LE) of the first bearing (360).
  11. Compressor assembly (1000) according to one of the preceding claims, characterized in that the compressor has a first connecting rod (140) which is arranged at an axial bearing distance (LA) from the first bearing (360).
  12. Compressor assembly (1000) according to one of the preceding claims, characterized in that the first connecting rod (140) and the compressor piston (150) are rigidly connected to one another, in particular with the compressor (100) being designed as a wobble piston compressor.
  13. Compressor assembly (1000) according to one of the preceding claims, characterized in that the compressor (100) is designed as a single-stage compressor or as a multistage compressor, in particular two-stage compressor.
  14. Compressor assembly (1000) according to one of the preceding claims, characterized in that the connecting-rod bearing (160) is formed as a rolling bearing, in particular a ball bearing, needle bearing, cylinder roller bearing, barrel bearing or similar rolling bearing, and/or the first bearing (360) and/or the second bearing (362) are/is formed as a sliding bearing.
  15. Compressor assembly (1000) according to one of the preceding claims, characterized in that the first bearing (360) and/or the second bearing (362) are/is fastened in a force-fitting manner, in particular by means of a tolerance ring (164).
  16. Compressed-air supply system (500) for operating a pneumatic system (600), having:
    - a compressor assembly (1000) according to one of Claims 1 to 15,
    - an air dryer (520), and
    - a valve arrangement (540).
  17. Vehicle (800), in particular a passenger car, having a compressor assembly according to one of Claims 1 to 15 and/or a compressed-air supply system (500) according to Claim 16 and a pneumatic system (600).
EP18716604.6A 2017-04-28 2018-04-09 Compressor device for the delivery of compressed air to a compressed air supply system Active EP3615798B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102017004086.9A DE102017004086A1 (en) 2017-04-28 2017-04-28 Compressor arrangement for a compressed air supply of a compressed air supply system
PCT/EP2018/058950 WO2018197186A1 (en) 2017-04-28 2018-04-09 Compressor assembly for a compressed-air feed of a compressed-air supply system

Publications (2)

Publication Number Publication Date
EP3615798A1 EP3615798A1 (en) 2020-03-04
EP3615798B1 true EP3615798B1 (en) 2021-01-06

Family

ID=61913176

Family Applications (1)

Application Number Title Priority Date Filing Date
EP18716604.6A Active EP3615798B1 (en) 2017-04-28 2018-04-09 Compressor device for the delivery of compressed air to a compressed air supply system

Country Status (5)

Country Link
US (1) US11078895B2 (en)
EP (1) EP3615798B1 (en)
CN (1) CN110392784B (en)
DE (1) DE102017004086A1 (en)
WO (1) WO2018197186A1 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20230100781A1 (en) * 2021-09-29 2023-03-30 Graco Minnesota Inc. Pump drive system
CN118499216A (en) * 2024-07-17 2024-08-16 比亚迪股份有限公司 Compression device, compressor and vehicle

Family Cites Families (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH87818A (en) 1920-04-13 1921-05-16 Huma Werk A G Pistons for compressors with high and low pressure cylinders in tandem.
DE2424562A1 (en) 1974-05-21 1975-12-04 Rolf Dipl Phys Mueller Direct balancing of masses for piston engines - common centre of gravity located in centre of crank shaft
US5556264A (en) * 1995-07-28 1996-09-17 Gp Companies, Inc. Low profile positive displacement pump system
JPH1144216A (en) * 1997-07-29 1999-02-16 Honda Motor Co Ltd Double acting piston type compressor
DE20319969U1 (en) * 2003-12-23 2004-03-11 Siemens Ag Rotation carrier with elastic connection device for installing electrical machines in pipes
JP4347684B2 (en) * 2003-12-26 2009-10-21 株式会社日立製作所 Horizontally opposed compressor
DE102004020104A1 (en) 2004-04-24 2005-11-17 Arnold Müller GmbH & Co KG Double piston for a compressor
DE102005009445B4 (en) 2005-03-02 2015-12-24 Wabco Gmbh compressor unit
JP4553977B1 (en) * 2009-10-26 2010-09-29 有限会社ケイ・アールアンドデイ Rotary cylinder device
CN101782056A (en) * 2010-01-12 2010-07-21 台州三和机械有限公司 Double-cylinder sliding block type air compressor
JP5458438B2 (en) * 2010-03-16 2014-04-02 株式会社医器研 Rotary cylinder device
WO2012017820A1 (en) * 2010-08-02 2012-02-09 日邦産業株式会社 Fluid rotary machine
JP2012067660A (en) * 2010-09-22 2012-04-05 Toyota Industries Corp Multistage compressor
DE102010062160A1 (en) 2010-11-30 2012-05-31 Continental Teves Ag & Co. Ohg Motor-pump unit
DE102013100015A1 (en) 2013-01-02 2014-07-03 Air-Com Gmbh Oddzial W Polsce Piston compression device, particularly for use in automotive industry, has toothed wheel that is made of plastic portion, where spindle for supporting toothed wheel is arranged in center of toothed wheel
DE102013003513A1 (en) 2013-03-04 2014-09-04 Wabco Gmbh Compressor arrangement for operating a compressed air supply system, compressed air supply system and compressed air supply system and vehicle with such a compressed air supply system
JP6366959B2 (en) * 2014-02-28 2018-08-01 株式会社エアーサーフ販売 Fluid rotating machine
CN204458243U (en) * 2015-02-15 2015-07-08 上海酷风汽车部件有限公司 A kind of three cylinder passenger car air-conditioner compressors
DE102016001576A1 (en) * 2016-02-11 2017-08-17 Wabco Gmbh Reciprocating piston engine, in particular two- or multi-stage piston compressor, compressed air supply system, compressed air supply system and vehicle, in particular passenger car with a compressed air supply system
US10215166B2 (en) * 2016-12-29 2019-02-26 Stuart H. Bassine Medical air compressor

Non-Patent Citations (1)

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

Also Published As

Publication number Publication date
US20200386217A1 (en) 2020-12-10
CN110392784B (en) 2020-09-11
CN110392784A (en) 2019-10-29
DE102017004086A1 (en) 2018-10-31
EP3615798A1 (en) 2020-03-04
WO2018197186A1 (en) 2018-11-01
US11078895B2 (en) 2021-08-03

Similar Documents

Publication Publication Date Title
EP3615799B1 (en) Compressor assembly for a compressed-air feed of a compressed-air supply system
DE4229069C2 (en) Swashplate refrigerant compressor for a cooling system
EP3701147B1 (en) Compressor assembly for operating a compressed air supply system, compressed air supply system, and vehicle
EP3615798B1 (en) Compressor device for the delivery of compressed air to a compressed air supply system
EP2989326B1 (en) Pump unit
EP3535495B1 (en) Reciprocating piston machine, in particular one-, two-, or three-stage piston compressor for a compressed air supply system of a vehicle
EP1315906B1 (en) Piston compressor comprising a crankshaft whose mass is dynamically compensated, in particular for rail vehicles (detachable compensatory mass)
WO2018197182A1 (en) Compressor, compressed air supply facility for operating a pneumatic system, and method for operating a compressed air supply facility
DE4201257C2 (en) Adjustable vane pump with pressure piece
EP1831553B1 (en) Dry-running swash-plate compressor with an antifriction bearing-mounted swash-plate
WO2002018788A1 (en) Piston compressor having a dynamic mass compensation in the region of the crank mechanism
EP3663579B1 (en) Piston compressor
DE112013000763T5 (en) pump device
EP2206918B1 (en) Oscillating displacement vacuum pump
DE102022116197A1 (en) Orbital piston compressor with circumferentially offset cylinder assemblies and shaft-integrated bearing seats
EP3060776B1 (en) Motor vehicle and method for assembling a motor vehicle
DE102009057387B4 (en) Rotary piston internal combustion engine
EP3535494A1 (en) Reciprocating-piston machine, compressed-air supply system, vehicle having a compressed-air supply system, methods for assembling and for operating a reciprocating-piston machine
DE3530432A1 (en) Rotating piston compressor
DE102010035820A1 (en) Hydrostatic positive displacement engine has piston that is subjected to input tilting movement along transverse direction of raceway
DE102011116435A1 (en) Modular system for storing shaft i.e. driven shaft, of piston-internal combustion engine of passenger car, has base element comprising bearing point, and bearing elements connected with base element under formation of bearing point

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: 20191128

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

DAV Request for validation of the european patent (deleted)
DAX Request for extension of the european patent (deleted)
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

INTG Intention to grant announced

Effective date: 20200915

GRAJ Information related to disapproval of communication of intention to grant by the applicant or resumption of examination proceedings by the epo deleted

Free format text: ORIGINAL CODE: EPIDOSDIGR1

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

Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE

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

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

INTC Intention to grant announced (deleted)
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

INTG Intention to grant announced

Effective date: 20201117

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: AT

Ref legal event code: REF

Ref document number: 1352651

Country of ref document: AT

Kind code of ref document: T

Effective date: 20210115

Ref country code: CH

Ref legal event code: EP

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 502018003587

Country of ref document: DE

REG Reference to a national code

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: R081

Ref document number: 502018003587

Country of ref document: DE

Owner name: ZF CV SYSTEMS EUROPE BV, BE

Free format text: FORMER OWNER: WABCO GMBH, 30453 HANNOVER, DE

Ref country code: DE

Ref legal event code: R081

Ref document number: 502018003587

Country of ref document: DE

Owner name: ZF CV SYSTEMS HANNOVER GMBH, DE

Free format text: FORMER OWNER: WABCO GMBH, 30453 HANNOVER, DE

RAP4 Party data changed (patent owner data changed or rights of a patent transferred)

Owner name: ZF CV SYSTEMS HANNOVER GMBH

REG Reference to a national code

Ref country code: NL

Ref legal event code: MP

Effective date: 20210106

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG9D

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

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: 20210106

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: 20210407

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: 20210106

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: 20210406

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: 20210506

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: 20210406

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: 20210106

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: 20210106

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: 20210106

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: 20210106

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: 20210106

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: 20210506

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 502018003587

Country of ref document: DE

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: 20210106

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: 20210106

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: 20210106

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

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

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: 20210106

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: 20210106

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: 20210106

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: 20210106

26N No opposition filed

Effective date: 20211007

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

Ref country code: LU

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

Effective date: 20210409

REG Reference to a national code

Ref country code: BE

Ref legal event code: MM

Effective date: 20210430

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

Ref country code: CH

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

Effective date: 20210430

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: 20210106

Ref country code: LI

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

Effective date: 20210430

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: 20210106

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: 20210106

REG Reference to a national code

Ref country code: DE

Ref legal event code: R081

Ref document number: 502018003587

Country of ref document: DE

Owner name: ZF CV SYSTEMS EUROPE BV, BE

Free format text: FORMER OWNER: ZF CV SYSTEMS HANNOVER GMBH, 30453 HANNOVER, DE

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

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: 20210106

Ref country code: IE

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

Effective date: 20210409

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: 20210506

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: 20210430

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

Ref country code: NL

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

Effective date: 20210206

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: 20210106

P01 Opt-out of the competence of the unified patent court (upc) registered

Effective date: 20230528

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

Ref country code: HU

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

Effective date: 20180409

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

Ref country code: FR

Payment date: 20230417

Year of fee payment: 6

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

Ref country code: GB

Payment date: 20230420

Year of fee payment: 6

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: 20210106

REG Reference to a national code

Ref country code: AT

Ref legal event code: MM01

Ref document number: 1352651

Country of ref document: AT

Kind code of ref document: T

Effective date: 20230409

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: 20210106

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

Ref country code: DE

Payment date: 20240306

Year of fee payment: 7

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: 20230409

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: 20230409

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

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: 20210106