Method for producing a cam phaser and cam phaser
11473454 ยท 2022-10-18
Assignee
Inventors
Cpc classification
F01L2250/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01L1/3442
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01L2303/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
Abstract
A method for producing a cam phaser for a cam shaft of an internal combustion engine, the cam phaser including a rotor, a stator and at least one cover, the method including arranging the at least one cover at the stator; and welding the at least one cover with the stator, wherein a first weld, a second weld and a third weld are formed at least on a large radius or on a small radius during the welding, and wherein the small radius is smaller than the large radius. The invention furthermore relates to a cam phaser for a cam shaft of an internal combustion engine, the cam phaser including a rotor; a stator and at least one cover.
Claims
1. A method for producing a cam phaser for a cam shaft of an internal combustion engine, the cam phaser including a rotor, a stator and at least one cover, the method comprising: arranging the at least one cover at the stator; and welding the at least one cover with the stator, wherein a first weld, a second weld and a third weld are formed on a large radius and on a small radius during the welding, wherein the small radius is smaller than the large radius, wherein the second weld is formed on the large radius and the third weld is formed on the small radius, wherein the third weld on the small radius is arranged and attached at a radially inward extending vane of the stator, wherein a borehole is arranged in the radially inward extending vane of the stator, and wherein the third weld is formed on the small radius closer to a rotation axis of the rotor than the borehole.
2. The method according to claim 1, wherein the first weld includes radial weld portions which extend in an essentially radial direction relative to a rotation axis of the rotor.
3. The method according to claim 2, wherein the radial weld portions connect the third weld on the small radius with the second weld on the large radius.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) Further advantages of the invention can be derived from the description and the drawing figures. The invention is subsequently described based on an embodiment with reference to drawing figures, wherein:
(2)
(3)
(4)
(5)
DETAILED DESCRIPTION OF THE INVENTION
(6)
(7) The cam phaser 100 includes a rotor 110 wherein
(8) A cover 130 is arranged at the stator 120. The cover 130 is configured disc shaped or circular segment shaped. The cover 130 is configured to cover pressure chambers between the stator 120 and the rotor 110. Thus, a high pressure impacts the cover 130. This pressure can have the effect that surface portions of the cover 130 bulge outward. In order to prevent this the cover 130 is welded with the stator 120 in a special manner. In particular the cover 130 is welded on a small radius 133 and on a large radius 134 with the stator 120 wherein the term radius relates to the cover 130. Thus, a circumferential weld 140 is not only formed at an outer radius of the cover 130 but also further inside.
(9) The circumferential weld 140 thus includes welds 142 at the small radius 133 and welds 141 at the large radius 134. The large radius 134 corresponds to the outer radius of the cover 130.
(10) The weld 140 furthermore includes radial weld portions 143 between the welds 141 and the welds 142 wherein the radial weld portions respectively connect a weld 141 on the large radius 134 and a weld 142 on the small radius 133. The radial weld portions 133 thus bridge the radial offset between the welds 141 and the welds 142. Thus, the radial weld portions 143 do not have to be configured exactly in the radial direction. It is sufficient that the radial weld portions facilitate the radius change of the circumferential weld 140.
(11) Thus, the circumferential weld 140 is configured continuous in
(12) The stator 120 includes plural vanes 121. The vanes 121 extend from an annular body 125 of the stator 120 radially inward. Therefore the vanes 121 are particularly suitable to form the welds 142 on the small radius 133 on the vanes 121. Accordingly the welds 142 in
(13)
(14) The circumferential weld 140 that includes the welds 141, 142 and 143 is configured essentially clover shaped in a radial axial direction of the rotor R. In particular the weld 140 is configured as a four leaf clover. Thus, each individual clover is formed by one of the welds at the large radius 134 and by two adjacent weld portions 143. The individual clover leafs are then connected by one of the welds 142 on the small radius 133.
(15)
(16) The cover 130 in
(17) An inward oriented edge of the recess 131 is arranged on the small radius 133 so that the welds 142 are arranged on the small radius. Also on the opposite edge, thus on the outward oriented edge welds are arranged. Furthermore welds are also formed at radial weld portions 143 between the two edges. Overall also the inner circumference of the recess 131 is connected by a continuous weld with the stator 120. Thus the continuous weld has the shape of the recess 131 in the cross section, this means in the rotation axis direction of the rotor 110. The welds 141 formed on the large radius 134 and the welds 142 formed on the small radius 133 are separate from each other in this embodiment.
(18) The welds 141 on the large radius 134 are configured in
(19) It is provided in a non-illustrated embodiment that the weld 140 is configured as a continuous weld exclusively on the large radius 134. The recesses 131 are not welded together with the stator 120 in this embodiment. The sealing is only provided by applying the cover 130 onto an advantageously ground contact surface of the stator 120.
(20) Advantageously it is also conceivable to provide a weld 142 exclusively on the small radius 133 or to weld exclusively about the recesses 131.
(21)
(22)
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(24) A circumferential groove 123 is configured at the stator 120. The circumferential groove 123 is formed on the same radius as the circumferential groove 132. Consequently also the radius of the circumferential groove 123 is smaller than the large radius 134. The bore holes 122 are connected through radial grooves 124 with the circumferential groove 123. Thus, gasses can be vented particularly easily. Melted material from the cover 130 can run into the radial groove 124 during welding so that the connection is particularly good.
(25) All features described and illustrated in a context with individual embodiments of the invention can be provided according to the invention in different combinations while still bringing their advantages to bear. The spirit and scope of the invention is defined by the appended claims and is not limited to the features described in the description or illustrated in the drawing figure.