Camshaft centering in the split rotor of a hydraulic camshaft adjuster
10584617 ยท 2020-03-10
Assignee
Inventors
Cpc classification
F01L2001/34423
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01L2001/3445
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01L1/3442
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01L2301/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01L2820/01
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F01L1/344
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A camshaft adjuster (1) is provided for an internal combustion engine of the vane cell type, having a stator (2) and a rotor (3) which can be rotated relative to the stator (2) and consists of a plurality of rotor parts (4, 5, 6) which are connected to one another, wherein the rotor (3) can be connected fixedly to a camshaft (7) of the internal combustion engine so as to rotate with it, and a first rotor part (4) is configured in such a way that the camshaft (7) is supported with contact on the first rotor part (4) in an operating state, wherein the first rotor part (4) is produced by a sintering process, and at least one first supporting surface (9), supporting the camshaft (7), of the first rotor part (4) is set geometrically by a chipless machining operation, and to a method for producing a rotor (3) for a camshaft adjuster (1) of this type.
Claims
1. A camshaft adjuster for an internal combustion engine of the vane cell type, the camshaft adjuster comprising: a stator; and a rotor rotatable relative to the stator and made up of a first rotor part, a second rotor part and a third rotor part, the first, second and third rotor parts being nested together at least one of axially or radially such that the first, second and third rotor parts rotate together within the stator, the rotor being connectable in a rotatably fixed manner to a camshaft of the internal combustion engine, the first rotor part including at least one first supporting surface configured for contacting the camshaft, the at least one first supporting surface being geometrically adjusted such that a porosity of the at least one first supporting surface is lower than other surfaces of the first rotor part, a diamond wheel configured for increasing a friction force contacts the at least one first supporting surface or at least one second support surface of the second rotor part.
2. The camshaft adjuster as recited in claim 1 wherein the second rotor part supports the camshaft in an axial direction, the first rotor part being connected to the second rotor part in a rotatably fixed manner.
3. The camshaft adjuster as recited in claim 1 wherein the first, second and third rotor parts are nested axially.
4. The camshaft adjuster as recited in claim 3 wherein the first rotor part includes a first radially extending surface configured for facing axially toward the camshaft and a second radially extending surface axially abutting the second rotor part.
5. The camshaft adjuster as recited in claim 4 wherein the second rotor part includes a first radially extending surface axially abutting the second radially extending surface of the first rotor part, and the second rotor part further including a second radially extending surface axially abutting the third rotor part such that the second rotor part is sandwiched axially between the first rotor part and the third rotor part radially inside of the stator.
6. The camshaft adjuster as recited in claim 3 wherein the first, second and third rotor parts together form rotor vanes.
7. The camshaft adjuster as recited in claim 3 wherein the first and second rotor parts form radially extending channels therebetween.
8. The camshaft adjuster as recited in claim 7 wherein the second and third rotor parts form radially extending channels therebetween.
9. A camshaft adjuster for an internal combustion engine of the vane cell type, the camshaft adjuster comprising: a stator; and a rotor rotatable relative to the stator and made up of a first rotor part, a second rotor part and a third rotor part, the first, second and third rotor parts being nested together at least one of axially or radially such that the first, second and third rotor parts rotate together within the stator, the rotor being connectable in a rotatably fixed manner to a camshaft of the internal combustion engine, the first rotor part including at least one first supporting surface configured for contacting the camshaft, the at least one first supporting surface being geometrically adjusted such that a porosity of the at least one first supporting surface is lower than other surfaces of the first rotor part, wherein the first, second and third rotor parts are nested radially, wherein the first rotor part is provided radially outside of the second rotor part, wherein a radially outer portion of the third rotor part is radially outside of the first rotor part.
10. The camshaft adjuster as recited in claim 9 wherein a radially inner portion of the third rotor part is radially inside of the first rotor part.
11. The camshaft adjuster as recited in claim 10 wherein the second rotor part axially abuts the radially inner portion of the third rotor part.
12. The camshaft adjuster as recited in claim 10 wherein the third rotor part includes an intermediate portion connecting the radially inner portion and the radially outer portion, the first rotor part being inserted within the third rotor part and axially abutting the intermediate portion.
13. A camshaft adjuster for an internal combustion engine of the vane cell type, the camshaft adjuster comprising: a stator; and a rotor rotatable relative to the stator and made up of a first rotor part, a second rotor part and a third rotor part, the first, second and third rotor parts being nested together at least one of axially or radially such that the first, second and third rotor parts rotate together within the stator, the rotor being connectable in a rotatably fixed manner to a camshaft of the internal combustion engine, the first rotor part including at least one first supporting surface configured for contacting the camshaft, the at least one first supporting surface being geometrically adjusted such that a porosity of the at least one first supporting surface is lower than other surfaces of the first rotor part, wherein the first, second and third rotor parts are nested radially, wherein the rotor includes vanes, the vanes being formed solely by the third rotor part.
14. The camshaft adjuster as recited in claim 13 wherein the at least one first supporting surface is an inner circumferential surface of the first rotor part configured for contacting the camshaft in a radial direction.
15. The camshaft adjuster as recited in claim 13 wherein the first, second and third rotor parts are nested radially, wherein the first rotor part is provided radially outside of the second rotor part, wherein a radially outer portion of the third rotor part is radially outside of the first rotor part.
Description
BRIEF DESCRIPTION OF THE INVENTION
(1) The present invention is now explained below with reference to several specific embodiments in the figures.
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(15) The figures are merely schematic, and are used only for an understanding of the present invention. Identical elements are provided with the same reference numerals.
DETAILED DESCRIPTION
(16) The various specific embodiments, as illustrated in conjunction with
(17) Fastening means 8 is designed as a central valve/central valve screw which is designed not only for fastening rotor 3 at an end area of camshaft 7, but also for introducing and discharging a supply of pressure fluid, which effectuates displacement of camshaft adjuster 1, into/out of camshaft adjuster 1. Stator 2 in turn is coupled in a rotatably fixed manner to a crankshaft of the internal combustion engine, preferably with the aid of a traction drive, namely, a chain drive, or alternatively, with the aid of a belt drive. The valve opening times of the internal combustion engine may thus be adjusted as a function of the rotational position between stator 2 and rotor 3. In addition, at least one first rotor part 4 of rotor 3 is designed in such a way that in the operating state it supports camshaft 7 in the radial direction.
(18) First rotor part 4 is manufactured with the aid of a sintering process, in addition at least one first supporting surface 9 of first rotor part 4 which supports camshaft 7 (in the radial or in the axial direction) being geometrically adjusted/calibrated with the aid of a non-cutting machining operation.
(19) As is further clearly apparent in
(20) According to the vane cell design, rotor 3 forms multiple vanes 10 for providing vane cells. These vanes 10 protrude outwardly in the radial direction from an outer circumferential surface of rotor 3, and protrude into stator 2. Each vane 10 protrudes into a separate chamber/working chamber formed in stator 2, each of the chambers being formed at stator 2 with the aid of projections which extend in the direction of rotor 3. In turn, vanes 10 thus divide the chambers of stator 2 into two working subchambers, which may be filled with a pressure fluid and acted on by pressure in alternation in order to adjust the rotary position of rotor 3 relative to stator 2.
(21) In the first specific embodiment, as illustrated particularly well in
(22) The calibration step (or a geometric adjustment) is understood to mean a local re-compaction of sintered pore surfaces, with the aim of compensating for distortions in the sintering process and increasing the dimensional accuracy as well as the surface density, surface hardness, surface quality of the relevant functional surfaces (supporting surface) or functional elements, and the strength of the component. The sintered part (first rotor part 4) is re-compacted in a calibration tool similar to a pressing tool. For wall thicknesses of approximately 3 mm, the degree of pressing is usually several tenths of a millimeter (approximately 0.1-0.3 mm); i.e., the local overpressing of the sintered surfaces in the calibration step may be up to 12% maximum of the wall thickness. Depending on the density and material of the rotor parts, improvements in the dimensional accuracy by approximately two tolerance classes may be achieved (for example, from ISO/IT 8-9 to ISO/IT 6-7 for Sint-D11 according to DI30910-4). Depending on the pore density and pore size in the starting material, the compaction process (deformation in the pressing tool or rolling), and the degree of deformation, the re-compaction in the calibration step may be increased by up to 100% maximum of the possible spatial filling. The calibrated surfaces are thus virtually pore-free, and the material density in the surface region is essentially comparable to the density of the solid base material (for steel, for example, approximately 7.8 g/cm.sup.3).
(23) Due to the calibration, compaction of the surface in the area of first supporting surface 9 is thus achieved, as the result of which the porosity in the surface layer at first supporting surface 9 is greatly reduced (to virtually 0% porosity). It is thus possible to initially manufacture first rotor part 4 with the aid of a sintering process (production of the green compact). A subsequent compaction of approximately 98% at a density of 6.8 to 7.1 g/cm.sup.3/approximately 7 g/cm.sup.3 via the calibration step allows first rotor part 4 to be geometrically adjusted to the desired dimensions. First rotor part 4 is thus geometrically adjusted/calibrated at its inner circumferential surface (in particular the diameter of the inner circumferential surface is thus geometrically adjusted).
(24) A second rotor part 5 having an essentially ring-shaped design rests against first rotor part 4. Second rotor part 5 adjoins first rotor part 4 in the axial direction and is connected thereto in a rotatably fixed manner. Second rotor part 5 forms a second supporting surface 11 for the axial support of camshaft 7, whereas first supporting surface 9 supports camshaft 7 in the radial direction. This second supporting surface 11, the same as first supporting surface 9, is also geometrically adjusted with the aid of a calibration step. The geometric adjustment of second rotor part 5 takes place in the same way as in the above-described calibration step on first rotor part 4. Second rotor part 5 is also manufactured by sintering/is sintered. The calibration step is once again a direct part of the sintering process, but alternatively may be carried out as a punching process. Thus, a calibration of second supporting surface 11 of second rotor part 5, designed as an axial front side/front surface, at the same time results in a calibration of the width of second rotor part 5. At the same time, the planarity of second supporting surface 11 extending along the circumference is also adjusted by the calibration process.
(25) A third rotor part 6 is in turn connected to second rotor part 5 in a rotatably fixed manner on a side facing away from first rotor part 4. Third rotor part 6 rests against second rotor part 5 in the axial direction, thus allowing the axial nesting of rotor 3. As is clearly apparent in
(26) As is also clearly apparent in conjunction with
(27) In conjunction with
(28) This diamond wheel 13 has a hard diamond layer on its axial front surfaces which presses into the front side of camshaft 7 and into second supporting surface 11 for increasing the support force/contact force between camshaft 7 and second supporting surface 11, into the material of the two components. As is also particularly clearly apparent in
(29) Recess 14 is once again preferably geometrically adjusted/formed with the aid of a calibration step. The geometric adjustment of first rotor part 4 in the area of recess 14 takes place once again via the calibration step, as described in conjunction with the adjustment of first rotor part 4 in the first specific embodiment. The calibration step is once again a step in a sintering process or a punching process, as the result of which the surface of first rotor part 4 is compacted in the area of recess 14, namely, by the width/thickness of diamond wheel 13.
(30) The design of diamond wheel 13 is particularly clearly apparent in
(31) In conjunction with
(32) Second rotor part 5 is radially accommodated/inserted within first rotor part 4, and once again is designed the same way as second supporting surface 11 (second supporting surface 11 according to the specific embodiment according to
(33) In other words, camshaft adjuster 1 according to the present invention provides a rotor 3 that is made up of multiple parts (first through third rotor parts 4, 5, 6), rotor parts 4, 5, 6 being combined with one another and connected in layers. The camshaft centering (centering of camshaft 7) is provided, without cutting, in one of the rotor parts (namely, first rotor part 4) as a cylindrical through opening having the desired dimensions in a calibration process/calibration step. Rotor 3 may have a design according to the sandwich principle, made up of two to three layered parts that are joined together axially and radially by a form-fit, force-fit, or integral bond connection. At least one rotor part 4, 5, 6 has a cylindrical through recess, which for the centering on camshaft 7 is designed with appropriate properties such as diameter, width, hardness, surface roughness, etc., and manufactured without cutting by shaping and sintering with the aid of a calibration processes. The width of first rotor part 4 corresponds to the centering depth of camshaft 7 in the rotor assembly. The necessary undercuts for the camshaft edge (front side of camshaft 7) or for the fixing of diamond wheel 13 are produced, without cutting, as indentations/recesses 14 on the flange side of rotor part 4 by shaping. Alternatively, rotor 3 may also have a design according to the onion skin principle, in which the camshaft centering in the inner portion is produced, without cutting, by shaping, sintering, or calibrating. Diamond wheel 13 may be inserted between the rotor parts 4, 5 during joining in the rotor assembly, and fixed in rotor 3 with play, or also without play.
LIST OF REFERENCE NUMERALS
(34) 1 camshaft adjuster 2 stator 3 rotor 4 first rotor part 5 second rotor part 6 third rotor part 7 camshaft 8 fastening means 9 first supporting surface 10 vane 11 second supporting surface 12 fluid-conducting channel 13 diamond wheel 14 recess 15 rotation axis