Method for producing a shaft
09884361 ยท 2018-02-06
Assignee
Inventors
Cpc classification
F16C33/64
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y10T29/49828
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
F16C3/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C3/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B21D7/00
PERFORMING OPERATIONS; TRANSPORTING
B21K1/12
PERFORMING OPERATIONS; TRANSPORTING
B21D35/002
PERFORMING OPERATIONS; TRANSPORTING
F16C19/466
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C2361/53
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y10T29/49698
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
F16F2226/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C33/581
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B21J1/06
PERFORMING OPERATIONS; TRANSPORTING
F16F15/264
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C3/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B21B1/16
PERFORMING OPERATIONS; TRANSPORTING
International classification
F02B75/06
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16F15/26
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B21D7/00
PERFORMING OPERATIONS; TRANSPORTING
B21D35/00
PERFORMING OPERATIONS; TRANSPORTING
F16C3/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B21B1/16
PERFORMING OPERATIONS; TRANSPORTING
F16C3/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C33/58
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C33/64
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B21J5/02
PERFORMING OPERATIONS; TRANSPORTING
B21K1/12
PERFORMING OPERATIONS; TRANSPORTING
Abstract
A method for producing a shaft, in particular a balance shaft, crankshaft and the like, having at least one substantially annular bearing seat and at least one unbalance portion. The method includes the steps: provision of a shaft blank; formation of the at least one unbalance portion and of at least two opposite bearing seat side members by a forming process; and deformation of the at least two opposite bearing seat side members by a shell tool such that the bearing seat side members are bent together, whereby the at least one substantially annular bearing seat is formed.
Claims
1. A method for producing a shaft having at least one substantially annular bearing seat and at least one unbalance portion, the method comprising: providing a shaft blank; forming the at least one unbalance portion and forming at least two opposite bearing seat side members via a forming process; and deforming the at least two opposite bearing seat side members via a shell tool such that the bearing seat side members are bent together such that the at least one substantially annular bearing seat is formed.
2. The method according to claim 1, wherein, prior to the step of forming the at least one unbalance portion and the at least two opposite bearing seat side members, a predeformation in the region of the at least one bearing seat and of the at least one unbalance portion is realized by cross-rolling and/or roll forging.
3. The method according to claim 1, wherein the forming process for forming the at least one unbalance portion and the at least two opposite bearing seat side members is a drop forging process.
4. The method according to claim 1, wherein the shaft blank is provided as a round billet, which has different diameters.
5. The method according to claim 1, wherein the shaft blank, before and/or during the deformation and/or drop forging, is heated inductively.
6. The method according to claim 1, wherein, after a drop forging and/or after the deformation of the at least two opposite bearing seat side members, excess material is trimmed.
7. The method according to claim 6, wherein the end faces of the bearing seat side members that have been brought into contact with each other are welded together.
8. The method according to claim 1, wherein the deformation of the at least two opposite bearing seat side members is realized in a hot, warm or cold deforming step.
9. The method according to claim 1, wherein the bearing seat side members are bent together in such a way that end faces of the bearing seat side members are brought into contact with each other and a closed bearing seat is formed.
10. The method according to claim 1, wherein the bearing seat side members are bent together in such a way that an open bearing seat is formed, wherein the bearing seat is open over an angular range between 5 and 45, between 10 and 30, or between 15 and 20.
11. The method according to claim 1, wherein after formation of the bearing seat, the bearing seat, at least in sections, is hardened, and is final machined via an inductive hardening process and/or via further other processes including grinding and finishing.
12. The method according to claim 1, wherein the bearing seat has a wall thickness between 2 and 15 mm, between 4 and 10 mm, or between 5 and 8 mm.
13. The method according to claim 1, wherein the bearing seat has a different wall thicknesses over its periphery.
14. The method according to claim 1, wherein a diameter of the bearing seat measures between 15 and 150 mm, between 20 and 100 mm, or between 25 and 40 mm.
15. A shaft produced according to a method according to claim 1.
16. A shaft produced according to claim 1, wherein the shaft is a balance shaft or crankshaft having at least one substantially annular bearing seat and at least one unbalance portion.
17. The shaft according to claim 16, wherein the bearing seat is a closed bearing seat and the bearing seat side members are welded together.
18. The shaft according to claim 16, wherein the bearing seat is an open bearing seat, and wherein the bearing seat is open over an angular range between 45 and 5, between 30 and 10, or between 20 and 15.
19. The shaft according to claim 16, wherein the shaft is configured as an integral component.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) The present invention will become more fully understood from the detailed description given hereinbelow and the accompanying drawings which are given by way of illustration only, and thus, are not limitive of the present invention, and wherein:
(2)
(3)
(4)
(5)
DETAILED DESCRIPTION
(6)
(7) The shaft 10 according to the invention can be used as a balance shaft in an internal combustion engine for the partial or full compensation of the free inertia forces and/or of the moments of inertia. A radial mounting of the shaft 10 can be realized via low-friction needle or roller bearings (not shown). These are disposed on a circumferential contact surface 16 of the annular bearing seat 15 or on corresponding surfaces on contact surfaces located at mutually opposite ends 30, 31 of the shaft 10. Instead of balance shafts, any other known types of shafts which have bearing seats and unbalances (i.e. a mass distributed in a non-rotationally-symmetrical manner in at least one section of the shaft; irrespective of whether the centre of gravity of the shaft lies on the rotational axis thereof, or not), such as, for instance, crankshafts, camshafts and the like, are also conceivable.
(8) In the shown illustrative embodiment, similarly one of the bearing ends 31 is configured as a bearing seat according to the invention. Additionally or alternatively, the other bearing end 30 or further middle bearing seats could similarly also be configured according to the invention. Nor is the number, position and dimensions of the bearing seats and unbalance portions limited by the invention. For the sake of simplicity, for the description of the invention reference is below confined to the middle bearing seat 15, though the same can also apply to all other bearing seats.
(9) As can be clearly seen in
(10) Depending on the application, the wall thickness of the annular bearing seat 15 is between 2 and 15 mm, preferably between 4 and 10 mm, and particularly preferably between 5 and 8 mm. The wall thickness of the bearing seat 15, viewed over the periphery, can also be configured with different magnitude. The diameter of the bearing seat 15 (i.e. the outer diameter of the annular bearing seat 15 up to the contact surface 16) measures between 15 and 150 mm, preferably between 20 and 100 mm, and particularly preferably between 25 and 40 mm.
(11) As can further be seen in
(12) Depending on the field of application, there is the possibility, furthermore, of arranging a fixing device on the bearing seat 15 (in particular on the contact surface 16) in order to possibly increase the dimensional stability or functionality (for instance, possibly with open bearing seat 15) of the bearing seat 15. Fixing device of this type can be, for example, bearing rings disposed on the contact surface 16, which bearing rings, for instance, can be shrunk onto or drawn onto the contact surface 16.
(13) The shaft 10 shown in
(14) An embodiment of a method according to the invention for producing the shaft 10 shown in
(15) In a first method step, a shaft blank (not shown) is provided as a round billet. The shaft blank can have different diameters.
(16) After this, at least the unbalance portions 20, 21 and, in the region of the bearing seat 15, at least two opposite bearing seat side members 17, 18 are formed via a forming process. As can be seen in
(17) Prior to the formation of the unbalance portions 20, 21 and of the two opposite bearing seat side members 17, 18, a predeformation can be performed in these regions, in particular in order to reduce the forces generated in the drop forging process, wherein, for the predeformation of these regions, a cross-rolling and/or roll forging process is preferably used. As a result of this process, the shaft blank is kneaded, so to speak, in such a way as to displace material into the regions of the later bearing seats 15 or bearing seat side members 17, 18 and unbalances 10, 21.
(18) After the step of forming the two opposite bearing seat side members 17, 18, the bearing seat side members 17, 18 are bent together in such a way via a shell tool 40, 41 shown by way of example in
(19) Alternatively or additionally to the above-stated welding of the bearing seat side members 17, 18, there is the possibility of providing on the bearing seat side members 17, 18 (possibly on their respective end faces 17, 18) a latching (not shown), which, when the bearing seat side members 17, 18 are bent together, can be brought into mutual engagement and possibly interlocked. For instance, the latching of this type can be provided as tongue and a groove, which can be brought into non-positive and/or positive engagement with each other by the bending together of the bearing seat side members 17, 18.
(20) During the deformation and/or during the drop forging, the shaft blank can be heated inductively. In addition, after the drop forging and/or after the deformation of the at least two opposite bearing seat side members 17, 18, a trimming step, with which excess material can be trimmed, is realized. After formation of the bearing seat 15, at least the bearing seat 15 or sections of the bearing seat 15 can be hardened, wherein, an inductive hardening process is used. Other final machining steps or processes, such as grinding and finishing, are also conceivable.
(21) With the method according to the invention, a shaft 10, which has an annular, hollow bearing seat 15, can thus be produced. In comparison to the previously known bearing seats, the annular bearing seat 15 here has considerably less material or weight, so that, on the one hand, the total weight of the shaft 10 and, on the other hand, in particular the weight of the bearing seat 15, and thus also the weight of the unbalance regions 20, 21, can be considerably reduced. Furthermore, in the exemplary embodiment of the shaft 10, having a closed bearing seat 15, a separate bearing ring can be dispensed with, since the bearing seat 15 already provides a closed contact surface 16.
(22) The present invention is not limited to the preceding illustrative embodiment, but embraces all embodiments covered by the scope of protection of the following claims.
(23) For instance, the invention is not limited to the number of bearing seats, nor, in particular, to the number of these bearing seats which are formed according to the invention. Moreover, it is conceivable that different embodiments of bearing seats (for instance open/closed ring), combined on a single shaft, can be present. Nor is the invention limited to certain dimensions of the shaft, unbalances, bearing seats and wall thicknesses of these same.
(24) The invention being thus described, it will be obvious that the same may be varied in many ways. Such variations are not to be regarded as a departure from the spirit and scope of the invention, and all such modifications as would be obvious to one skilled in the art are to be included within the scope of the following claims.