Pump device for driving blow-by-gas

Abstract

A pump device may include a side channel compressor that may include a housing having a conveying chamber and a fluid inlet and outlet. The compressor may include an impeller having blades radially on an outside and which may be mounted rotatably in the housing, the blades lying in the conveying chamber, and a shaft mounted rotatably about an axis of rotation and on which the impeller may be fastened. The conveying chamber may have at least one side channel running in a region of the blades and connecting the fluid inlet and outlet to one another in a circumferential direction. An intermediate region may be formed in the circumferential direction between the fluid inlet and outlet and in which a distance of the blades in an axial direction to the nearest wall may be such that no more than a predetermined amount of fluid flows in the intermediate region.

Claims

1. A pump device for driving blow-by gas in a crankcase ventilation apparatus, comprising a side channel compressor including: a housing having a conveying chamber, a fluid inlet, and a fluid outlet, each extending in a circumferential direction and positioned at an axial location of the pump device; having blades radially on an outside and which is mounted rotatably in the housing, wherein the blades lie in the conveying chamber at the axial location; a shaft mounted rotatably about an axis of rotation and on which an impeller is fastened; wherein the conveying chamber has at least one side channel that runs in a region of the blades and connects the fluid inlet and the fluid outlet to one another in the circumferential direction; and wherein an intermediate region is formed at the axial location and in the circumferential direction between the fluid outlet and the fluid inlet and in which a distance of the blades in an axial direction to the nearest wall is such that no more than a predetermined amount of fluid flows in the intermediate region.

2. The pump device according to claim 1, further comprising at least one oil drain through which oil is drainable from the conveying chamber.

3. The pump device according to claim 2, wherein the at least one oil drain is arranged at a lowest point of the conveying chamber in a direction of gravity.

4. The pump device according to claim 2, wherein the oil drain guides oil separated in the side channel compressor into an oil return, which returns the oil to an oil cycle.

5. The pump device according to claim 1, further comprising at least one fin in the at least one side channel, the at least one fin separating at least two chambers open towards the impeller from one another.

6. The pump device according to claim 1, wherein the housing has an at least one insert into the conveying chamber, wherein the housing and at least one insert have different materials.

7. The pump device according to claim 1, wherein at least one of: the pump device has two opposite side channels; at least one fin is arranged in each side channel, the at least one fin extending at least in sections obliquely to a circumferential direction; and at least two chambers open to the impeller are arranged in each of the two side channels.

8. The pump device according to claim 1, further comprising a drive unit coupled to the shaft.

9. The pump device according to claim 8, wherein the drive unit includes a turbine wheel that is held in a torque-proof manner to and on the shaft.

10. A crankcase ventilation apparatus comprising: an inertia-based oil mist separator; and a pump device having a side channel compressor that includes: a housing having a conveying chamber, a fluid inlet, and a fluid outlet, each extending in a circumferential direction and positioned at an axial location of the pump device; an impeller having blades radially on an outside and which is mounted rotatably in the housing, wherein the blades lie in the conveying chamber at the axial location; a shaft mounted rotatably about an axis of rotation and on which the impeller is fastened; wherein the conveying chamber has at least one side channel that runs in a region of the blades and connects the fluid inlet and the fluid outlet to one another in a circumferential direction; and wherein an intermediate region is formed at the axial location and in the circumferential direction between the fluid outlet and the fluid inlet and in which a distance of the blades in an axial direction to the nearest wall is such that no more than a predetermined amount of fluid flows occur in the intermediate region.

11. The crankcase ventilation apparatus according to claim 10, wherein the inertia-based oil mist separator is arranged downstream of the pump device, wherein the inertia-based oil mist separator includes an oil drain that guides oil separated in the oil mist separator to an oil return.

12. The crankcase ventilation apparatus according to claim 10, wherein the inertia-based oil mist separator is an impactor.

13. The crankcase ventilation apparatus according to claim 11, wherein the oil drain guides the oil into a drive housing part of the crankcase ventilation apparatus, and wherein the oil return returns oil from the drive housing part into an oil cycle.

14. A pump device for driving blow-by gas in a crankcase ventilation apparatus, comprising: a side channel compressor that includes: a housing having a conveying chamber, a fluid inlet, and a fluid outlet, each extending in a circumferential direction and positioned at an axial location of the pump device; an impeller having blades radially on an outside and which is mounted rotatably in the housing, wherein the blades lie in the conveying chamber; a shaft mounted rotatably about an axis of rotation and on which the impeller is fastened; wherein the conveying chamber has at least one side channel that runs in a region of the blades and connects the fluid inlet and the fluid outlet to one another in the circumferential direction; and wherein an intermediate region is formed at the axial location and in the circumferential direction between the fluid outlet and the fluid inlet and in which a distance of the blades in an axial direction to the nearest wall is such that no more than a predetermined amount of fluid flows occur in the intermediate region; and at least one oil drain arranged at a lowest point of the conveying chamber in a direction of gravity, the oil drain guiding oil separated in the side channel compressor from the conveying chamber into an oil return that returns the oil to an oil cycle.

15. The pump device according to claim 14, wherein at least one of: the pump device has two opposite side channels; at least one fin is arranged in each side channel, the at least one fin extending at least in sections obliquely to a circumferential direction; and at least two chambers open to the impeller are arranged in each of the two side channels.

16. The pump device according to claim 1, wherein the at least one side channel includes a radially inner surface and a radially outer surface, and the impeller is positioned between the radially inner surface and the radially outer surface, and wherein the fluid inlet and the fluid outlet are positioned radially external to at least the radially inner surface.

17. The pump device according to claim 16, wherein the fluid inlet and the fluid outlet are positioned approximately within a common plane with one another, wherein the fluid inlet is positioned such that fluid enters the fluid inlet along the common plane, and wherein the fluid outlet is positioned such that fluid exits the fluid outlet along the common plane.

18. The crankcase ventilation apparatus according to claim 10, wherein the at least one side channel includes a radially inner surface and a radially outer surface, and the impeller is positioned between the radially inner surface and the radially outer surface, and wherein the fluid inlet and the fluid outlet are positioned radially external to at least the radially inner surface.

19. The crankcase ventilation apparatus according to claim 18, wherein the fluid inlet and the fluid outlet are positioned approximately within a common plane with one another, wherein the fluid inlet is positioned such that fluid enters the fluid inlet along the common plane, and wherein the fluid outlet is positioned such that fluid exits the fluid outlet along the common plane.

20. The pump device according to claim 14, wherein the at least one side channel includes a radially inner surface and a radially outer surface, and the impeller is positioned between the radially inner surface and the radially outer surface, wherein the fluid inlet and the fluid outlet are positioned radially external to at least the radially inner surface, wherein the fluid inlet and the fluid outlet are positioned approximately within a common plane with one another, wherein the fluid inlet is positioned such that fluid enters the fluid inlet along the common plane, and wherein the fluid outlet is positioned such that fluid exits the fluid outlet along the common plane.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) In the figures, in each case schematically

(2) FIG. 1 shows a schematic diagram of a crankcase ventilation apparatus,

(3) FIG. 2 shows a sectional view through the crankcase ventilation apparatus,

(4) FIG. 3 shows an exploded view of the crankcase ventilation apparatus,

(5) FIG. 4 shows a schematic diagram to illustrate the function of a side channel compressor,

(6) FIG. 5 shows a sectional view through the side channel compressor along the plane of intersection AA from FIG. 4,

(7) FIG. 6 shows a sectional view through the side channel compressor along the plane of intersection BB from FIG. 4,

(8) FIG. 7 shows a perspective view of a housing upper part of the side channel compressor,

(9) FIG. 8 shows a perspective view of a housing lower part of the side channel compressor with an impeller arranged therein,

(10) FIG. 9 shows an enlarged view of the region C from FIG. 6,

(11) FIG. 10 shows an enlarged view of the region D from FIG. 6,

(12) FIG. 11 shows a schematic diagram of a view of a housing part of the side channel compressor,

(13) FIG. 12 shows a diagram of an insert part,

(14) FIG. 13 shows a schematic view of another insert part,

(15) FIG. 14a-g shows a schematic view of the course of fins in the side channels,

(16) FIG. 15 shows a sectional view through a side channel compressor along the plane of intersection AA from FIG. 4 to illustrate the fins,

(17) FIG. 16 shows a sectional view through a side channel compressor according to another variant, along the plane of intersection AA from FIG. 4 and

(18) FIG. 17 shows a sectional view through a side channel compressor according to another variant, along the plane of intersection AA from FIG. 4.

DETAILED DESCRIPTION

(19) The crankcase ventilation apparatus 10 shown in FIG. 1 is used to ventilate a crankcase 12 of an internal combustion engine 14. In this case blow-by gas 32 is removed from the crankcase 12 and freed from an oil mist and supplied to the intake tract 16 of the internal combustion engine 14. The crankcase ventilation apparatus has a pump device 18 which comprises a side channel compressor 20 which is driven by a drive unit 22 and an oil mist separating device 24 which comprises an inertia-based oil mist separator 26, for example, an impactor 28. Further, the crankcase ventilation apparatus 10 has a pressure-regulating valve 30 which prevents the pressure in the crankcase 12 from dropping too much or even taking in oil.

(20) The crankcase ventilation apparatus 10 is arranged in such a manner that blow-by gas 32 from the crankcase 12 is initially guided to the pressure-regulating valve 30 and then flows through the pump device 18 and is driven by the pump device 18, then the compressed blow-by gas 32 is guided through the oil mist separator 26 in which the blow-by gas 32 is freed from oil mist. From the oil mist separator 26 the purified blow-by gas 32 is supplied to the intake tract 16 of the internal combustion engine 14.

(21) In particular, the purified blow-by gas 32 downstream of a filter device 15 of the intake tract 16 is supplied to the intake tract 16. Since the oil mist is largely removed from the blow-by gas 32, the elements arranged downstream of the filter device 15, for example, a compressor 17 of a charging device 19, are protected. For example, FIG. 1 shows an internal combustion engine 14 with a charging device 19 with a compressor 17 and a turbine 21 driven by an exhaust gas stream, i.e. with an exhaust gas turbocharger. However, the crankcase ventilation apparatus 10 according to the invention can also be used in differently charged or non-charged internal combustion engines 14.

(22) As shown, for example, in FIGS. 2 and 3, the crankcase ventilation apparatus 10 has a housing 34 which is configured to be multipart, for example four-part. The housing 34 has a cover 36 in which the oil mist separator 26 is arranged. Furthermore, the housing 34 comprises an upper part 38 of the side channel compressor 20, a lower part 40 of the side channel compressor 20 and a drive housing part 42 in which the drive unit 22 is arranged. Preferably the individual housing parts are arranged on one another from top to bottom in this order in the direction of gravity. Seals 25 are provided between the individual housing parts which seal an interior of the housing 34 with respect to the surroundings.

(23) Alternatively or additionally to this, it can be provided that the cover is formed in one part with the upper part 38 of the side channel compressor 20 so that required seals and screw connections can be saved as a result.

(24) As shown in FIGS. 3 to 6 for example, the side channel compressor 20 has a housing 44 which is formed by the upper part 38 and the lower part 40. The housing 44 encloses a conveying chamber 46 and has a fluid inlet 48 and a fluid outlet 50 which each have a fluidic connection to the conveying space 46. Furthermore an impeller 52 is arranged in the housing 44 of the side channel compressor 20, which has a shaft connection 54 and radially outer blades 56. An annular section 96 of the impeller 52 connects the shaft connection 54 to the blades 56. The impeller 52 is arranged in such a manner that the blades 56 lie in the conveying chamber 46. Furthermore, the impeller is held on the shaft 58 in a torque-proof manner, which shaft is in turn mounted rotatably about an axis of rotation 60. Consequently the impeller 52 is also rotatable about the axis of rotation 60.

(25) The conveying chamber 46 has at least one side channel 62, for example an upper side channel 64 and a lower side channel 66. The side channels 62 extend in the region of the blades 56 of the impeller 52. In particular, the side channels 62 extend next to the blades 52. When viewed in the circumferential direction, the side channels 62 extend between the fluid inlet 48 and the fluid outlet 50.

(26) The fluid inlet 48 and the fluid outlet 50 are arranged here in such a manner that they are spaced apart from one another at an angle of less than 90, particularly preferably less than 60. The angular information relates to the axis of rotation 60. Consequently there is short connection possibility in the circumferential direction and a long connection possibility.

(27) The side channels 62 connect the fluid inlet 48 and the fluid outlet 50 via the long path. None of the side channels 62 extends in an intermediate region 68 which lies on the short path between the fluid inlet 48 and the fluid outlet 50. In particular, in the intermediate region 68 the distance of the blades in the axial direction to the nearest wall is very small so that none or only small fluid flows occur in this region.

(28) During operation the impeller 52 is rotated about an axis of rotation 60 so that the blades transport the medium to be pumped, for example, blow-by gas 32 from the fluid inlet 48 via the long path to the fluid outlet 50. Through the rotation of the impeller 52, the blow-by gas 32 is compressed radially outwards as a result of the centrifugal force. Since the blades of the impeller 52 are open towards the outside, the blow-by gas 32 can also flow from intermediate spaces between the blades 56 into the side channels 62. In the side channels 62 the blow-by gas 32 is decelerated in the circumferential direction and can thus flow radially outwards without losing pressure. The blow-by gas 32 flows radially inwards again into regions between the blades 56 of the impeller 52 and is again entrained in the circumferential direction so that it can be compressed again. As a result of this cycle, a pressure difference can build up between the fluid outlet 50 and the fluid inlet 48.

(29) The compression of the blow-by gas 32 in the side channel compressor 20 takes place without sealing surfaces needing to slide on one another, so that the friction of a side channel compressor 20 is extremely low so that both the efficiency is particularly high and the lifetime is particularly long and a particle loading of the blow-by gas 32 by the side channel compressor 20 is particularly low. A side channel compressor 20 is therefore particularly well suited for driving the blow-by gas in the crankcase ventilation apparatus.

(30) For mass production it is desirable if most of the crankcase ventilation apparatus 10, in particular the housing 34, is made or plastic or fibre-reinforced plastic. However, with plastic or fibre-reinforced plastic the required tolerances, in particular in the intermediate region 68 in which the distance between the impeller 52 and the wall of the housing 44 is small cannot be sufficiently maintained. Furthermore the required stability cannot be maintained with the aid of plastics or fibre-reinforced plastics.

(31) For this reason, at least one insert part 70 can be provided such as is shown for example in FIGS. 7 to 10. The insert part 70 can be fabricated from a different material to the housing 44 of the side channel compressor 20 and the housing 34 of the crankcase ventilation apparatus 10. Consequently a higher-quality material can be selected which has a higher stability and allows smaller manufacturing tolerances. At the same time, the amount of high-quality material required is reduced since the entire housing 44 of the side channel compressor 20 need not be fabricated from the high-quality material.

(32) For example, the insert part 70 is made of metal so that a hybrid design of plastic and metal is obtained for the crankcase ventilation apparatus 10. The insert part 70 can for example be made by stamping and/or bending and/or deep drawing and/or turning processes.

(33) The at least one insert part 70 therefore forms a wall 72 of the conveying space 46, in particular in the intermediate region 68. Accordingly, the insert part 70 is configured to be annular, where the rotational symmetry is interrupted by the intermediate region 68.

(34) Preferably the side channel compressor 20 has two insert parts 70, namely a first insert part 73 and a second insert part 74. The first insert part 73 for example is inserted in the upper part 38 of the housing 44 of the side channel compressor 20. It forms in particular an upper wall of the conveying chamber 46 in the intermediate region 68.

(35) The second insert part 74 is inserted for example in the lower part 40 of the housing 44 of the side channel compressor 20. In the radially outer region it forms the lower side channel 66 and the intermediate region 68. In a radially inner region the second insert part 74 forms a radial bearing surface 76 on which a bearing device 78 is arranged.

(36) The bearing device 78 preferably mounts the shaft 58 of the impeller 52. As a result, the alignment of the impeller 52 is precise due to the high precision of the second insert part 74 so that the tolerance during the positioning of the impeller 52 with respect to the wall in the intermediate region 68 can be further reduced.

(37) In order to further improve the efficiency of the side channel compressor 20, at least one fin 80, preferably at least two fins 80 are provided, which are arranged in the side channels 62 and extend at least in sections obliquely to the circumferential direction. As a result, the fins 80 decelerate the movement of the blow-by gas 32 to be pumped in the circumferential direction so that the rotation of the blow-by gas 32 in the side channels 62 is additionally supported and as a result the pressure increase through the side channel 62 is improved. The fins 80 improve the efficiency in certain load ranges.

(38) Different profiles and arrangements of the fins 80 are feasible. In a variant shown as an example in FIG. 14a, the side channels have eight fins 80 which run substantially perpendicularly to the fins 80. Alternatively the fins can also run tilted thereto, as shown for example in FIG. 14b.

(39) It is furthermore possible that the fins 80 do not run straight but in a bent manner. For example, the fin can run in an S-shape as shown for example in FIG. 14c. Furthermore, the fins 80 can have a bend. Alternatively or additionally it can also be provided for this purpose that the fins 80 have gaps as shown for example in FIGS. 14e and 14f.

(40) The dependence of the efficiency on the working point can be improved by the differently shaped fins 80. That is, that the efficiency is less strongly dependent on the respective working point and therefore a high efficiency can be achieved over a wider range.

(41) It can further be provided that in the upper side channel 64 more or less fins 81 are provided that fins 83 are arranged in the lower side channel 66.

(42) Finally it can also be provided that fins 81 in the upper side channel 64 and fins 83 in the lower side channel 66 are arranged offset by an angle in the circumferential direction. Furthermore it can also be provided that the fins 81 in the upper side channel 64 are differently shaped or larger or smaller than the fins 83 in the lower side channel 66, as shown for example in FIG. 15.

(43) Due to the fins 80, chambers 82 are formed in the side channels 62 which are open towards the impeller 52. Flow vortices of the blow-by gas 32 can be formed particularly effectively in the chambers 82.

(44) The fins 80 can, for example, be formed by the at least one insert part 70. The insert part 70 can be stamped accordingly so that a tab can be bent upwards in the insert part so that a fin 80 is formed. Furthermore the fins 80 can also be formed by parts of the housing 44, in particular by the upper part 38 or lower part 40. For example, the injection mould can be adapted accordingly.

(45) Furthermore plastic surfaces can be injection-moulded onto the insert parts 70, 73, 74 on which the fins 80 are formed of plastic.

(46) On the basis of its operating mode, a side channel compressor 20 functions as an oil mist separator 26 according to the inertia principle. For this reason oil from the blow-by gas 32 collects in the conveying chamber 46 of the side channel compressor 20. For this reason at least one oil drain 84 is provided through which oil can drain from the conveying chamber 46 out from the side channel compressor 20 and in particular is fed into an oil return 85 which returns the separated oil to an oil cycle. For example, the oil drain 84 guides the oil into the drive housing part 42 from which the oil from the oil return 85 is returned to the oil cycle.

(47) Preferably the lower side channel 66 has the oil drain 84 since as a result of gravity the oil separated in the side channel compressor 20 will run into the lower side channel 66. Particularly preferably the lower side channel 66 has its own oil drain 84 for each chamber 82 so that the separated oil can drain from each of the chambers 82. In particular, the oil drains 84 are arranged in the lowest positions of the respective chambers in the direction of gravity so that none or at least only a very small amount of oil can remain in the side channel compressor 20.

(48) As a result of this configuration of the side channel compressor 20, the side channel compressor 20 can be used as a first stage in the oil mist separation so that the crankcase ventilation apparatus 10 offers a two-stage oil mist separation. In particular, as a result of the at least one oil drain 84, it is possible for the first time that the pump device 18 and therefore the side channel compressor 20 is arranged between the crankcase 12 and the oil mist separator 26. Thus, in this way an elevated pressure compared with the ambient pressure can be generated by the pump device 18 which can be used in the inertia-based oil mist separator 26 in order to separate oil from the blow-by gas 32. Compared with the generation of negative pressure, the generation of positive pressure is advantageous since in this way higher pressure differences can be provided at the oil mist separator 26.

(49) Furthermore, the bearing device 78, as shown for example in FIG. 5 or 10, is arranged between the impeller 52 and the drive unit 22 so that a particularly compact design of the crankcase ventilation apparatus 10 is obtained. The bearing device 78 has an oil supply 86 which in particular is supplied for example from an oil drain 84 or the oil return of the oil mist separator 26. Furthermore, the bearing device 78 has an oil drain 88 so that an oil circulation can be achieved in the bearing device 78.

(50) The bearing device 78 is in particular designed as an axial and radial bearing so that a single bearing device 78 is sufficient. Alternatively as shown for example in FIG. 6, the bearing device can also comprise an axial bearing and a separate radial bearing which however are both arranged between the impeller 52 and the drive unit 22.

(51) The bearing device 78 mounts the shaft 58 on which the impeller 52 and for example the drive unit 22 are held in a torque-proof manner so that the oil mist separating device 24 manages with a single bearing device 78.

(52) In particular, the bearing device 78 can comprise a ball bearing, a plain bearing, a roller bearing or a needle bearing.

(53) As shown for example in FIG. 5, a sealing device 90 is provided which seals the conveying chamber of the side channel compressor 20 from an inner region of the side channel compressor 20 so that no unnecessary gas flow occurs in the inner region 92. The sealing device 90 is preferably formed as a labyrinth seal so that this only produces a small amount of friction.

(54) In a further variant, as shown for example in FIG. 16 or 17, the side channel compressor 20 has a recess 94 in a wall 93 of the housing 44. In particular, the recess 94 is arranged in the inner region 92. The recess 94 in this case lies opposite an annular section 96 of the impeller 52 which extends between the shaft connection 54 and the blades 56. Due to the recess 94, an axial distance 95 between the impeller 52 and the wall 93 of the housing 44 is increased so that the frictional forces produced as a result of shear flows can be reduced and therefore frictional losses can be reduced.

(55) The recess 94 can be formed by the wall 93 running obliquely to the annular section 96 of the impeller 52, as shown for example in FIG. 17. As a result, oil which collects at the wall 93 can be guided to the bearing device 78 with the result that the bearing device can be lubricated.

(56) Furthermore, the recess 94 can be formed by the wall 93 running in a bent manner and thus forming a depression or by running in a stepped manner, as shown for example in FIG. 16.

(57) The inertia-based oil mist separator 26 of the oil mist separating device 24 is configured as an impactor 28 and can also separate other liquids. At the impactor 28, the gas flow to be purified, for example the blow-by gas 32, is guided through at least one nozzle which is located opposite a baffle plate so that the gas flow is deflected directly after the nozzle. Due to the nozzle the gas flow acquires a high velocity so that the liquid droplets, hereinafter called oil droplets, cannot follow the deflection by the baffle plate and impinge on the baffle plate and remain suspended there and are thus separated from the gas flow.

(58) Furthermore the impactor 28 comprises a poppet valve which is closed in a spring-loaded manner wherein the poppet valve opens when a pressure difference between valve inlet and valve outlet is exceeded. In this case, the poppet valve forms an annular flow gap which also functions as a nozzle and accelerates the gas flow flowing through the impactor 28, for example the blow-by gas 32. The annular flow gap is surrounded by a cylindrical baffle plate which deflects the gas flow flowing through the annular flow gap and thus enables a separation of oil droplets from the gas flow there. Since the poppet valve opens with increasing pressure difference, the flow cross-section of the impactor is increased and thus the flow cross-section of the oil mist separating device 24 is enlarged. The flow cross-section is composed of the cross-section of all the nozzles and the flow area of the annular flow gap.

(59) The oil mist separating device 24 has an oil drain 97 which fluidically connects the cover 36 to the drive housing part 42. The oil separated by the oil mist separator 26, here impactor 28, is supplied to the oil drain 97. Through the oil drain 97, the oil can drain into the drive housing part 42 and from there return via the oil return 85 to the oil cycle.

(60) The drive unit 22 for example comprises a turbine wheel 98 which is held on the shaft 58 in a torque-proof manner. Thus, the turbine wheel 98 can drive the impeller 52 of the side channel compressor 20. Furthermore the turbine wheel 98 is also mounted by the bearing device 78 by means of which the shaft 58 is mounted so that a compact design is achieved.

(61) For example, the turbine wheel 98 is driven by oil which is guided via a nozzle 100 onto the turbine wheel 98. A hydraulic system is usually already provided in internal combustion engines 14 so that the drive unit 22 can be implemented cost-effectively. In particular, the turbine wheel can be formed as a Pelton turbine wheel.

(62) Since oil which drives the turbine wheel 98 collects in the drive housing part 42, the oil can be returned via the oil return 85 to the oil cycle. As a result, the oil guided by the oil mist separating device 24 into the drive housing part 42 and the oil guided from the side channel compressor 20 into the drive housing part 42 together with the oil used to drive the turbine wheel 98 can be returned through the oil return 85 to the oil cycle.

(63) As a result, oil lines can be saved so that a cost-effective and compact design is obtained.