METHOD FOR MACHINING THE TOOTH FLANKS OF FACE COUPLING WORKPIECES IN THE SEMI-COMPLETING METHOD
20180056417 ยท 2018-03-01
Inventors
Cpc classification
B23F19/005
PERFORMING OPERATIONS; TRANSPORTING
International classification
B23F15/06
PERFORMING OPERATIONS; TRANSPORTING
Abstract
A continuous semi-completing method for machining the tooth flanks of a face coupling workpiece using a gear cutting tool having multiple blades. Exemplary methods include a) setting of a first machine setting, wherein an inner cutting edge of an mth blade of the gear cutting tool machines a convex flank of a first tooth gap, and an inner cutting edge of a further blade machines a convex flank of a following tooth gap, until all convex flanks of all tooth gaps are finish machined, and b) setting of a second machine setting wherein an outer cutting edge of an nth blade of the gear cutting tool machines a concave flank of a tooth gap, and an outer cutting edge of a further blade machines a concave flank of a following tooth gap, until all concave flanks of all tooth gaps are finish machined.
Claims
1. A method for machining tooth flanks of a face coupling workpiece in a continuous semi-completing process, the method comprising: performing the following steps a) and b), which are carried out in a sequence of step a) and then step b), or a sequence of step b) and then step a), using a gear cutting tool having a plurality of blades, wherein each of the plurality of blades includes an inner cutting edge and an outer cutting edge, and steps a) and b) comprise: a) setting a first machine setting, rotationally driving the face coupling workpiece about a workpiece rotational axis, and coupledly rotationally driving the gear cutting tool about a tool rotational axis, wherein the first machine setting is defined and said coupled driving of the face coupling workpiece with said driving of the gear cutting tool is performed to provide an indexing movement of the face coupling workpiece relative to the gear cutting tool, machine a convex flank of a first tooth gap of the face coupling workpiece with a respective inner cutting edge of an mth blade of the gear cutting tool, and machine a convex flank of a following tooth gap of the face coupling workpiece with an inner cutting edge of a further blade of the gear cutting tool that follows after the mth blade, until all convex flanks of all tooth gaps of the face coupling workpiece are finish machined; b) setting a second machine setting, rotationally driving the face coupling workpiece about the workpiece rotational axis and coupledly rotationally driving the gear cutting tool about the tool rotational axis, wherein the second machine setting is defined and said coupled driving of the face coupling workpiece with said driving of the gear cutting tool is performed to provide an indexing movement of the face coupling workpiece relative to the gear cutting tool, machine a concave flank of a first tooth gap of the face coupling workpiece with a respective outer cutting edge of an nth blade of the gear cutting tool, and machine a concave flank of a following tooth gap of the face coupling workpiece with an outer cutting edge of a further blade of the gear cutting tool that follows after the nth blade, until all concave flanks of all tooth gaps of the face coupling workpiece are finish machined.
2. The method according to claim 1, wherein the face coupling workpiece was untoothed prior to performing the method, and the method further comprises: when step a) and then step b) is performed, roughing the concave flanks of the face coupling workpiece with the outer cutting edges of the plurality of blades during said machining of the convex flanks using the inner cutting edges of the plurality of blades, or when step b) then step a) is performed, roughing the convex flanks of the face coupling workpiece with the inner cutting edges of the plurality of blades during said machining of the concave flanks using the outer cutting edges of the plurality of blades.
3. The method according to claim 1, further comprising: when step a) and then step b) is performed, during step a), broaching the rotationally-driven gear cutting tool into the material of the face coupling workpiece after the first machine setting has been set, at the end of step a), removing the gear cutting tool from the face coupling workpiece, and during step b), broaching the rotationally-driven gear cutting tool into the material of the face coupling workpiece after the second machine setting has been set.
4. The method according to claim 1, further comprising: when step b) then step a) is performed, during step b), broaching the rotationally-driven gear cutting tool into the material of the face coupling workpiece after the second machine setting has been set, at the end of step b), removing the gear cutting tool from the face coupling workpiece, and during step a), broaching the rotationally-driven gear cutting tool into the material of the face coupling workpiece after the first machine setting has been set.
5. The method according to claim 1, further comprising, when step a) and then step b) is performed, after step a) and before step b), retracting the gear cutting tool from the face coupling workpiece, and transferring from the first machine setting into the second machine setting.
6. The method according to claim 1, further comprising, when step b) and then step a) is performed, after step b) and before step a), retracting the gear cutting tool from the face coupling workpiece, and transferring from the second machine setting into the first machine setting.
7. The method according to claim 1, wherein the inner cutting edge and the outer cutting edge of a respective blade are located on a common cutting head of the tool.
8. The method according to claim 1, wherein the plurality of blades are assembled into groups, and each group includes only one blade.
9. The method according to claim 1, wherein the second machine setting differs from the first machine setting by one or more of: a location of a rotation center of the tool in relation to a location of the face coupling workpiece; a setting of a radial of a machine in which the method is executed; a setting of a sway angle of a machine in which the method is executed, or a setting of a tilt angle of a machine in which the method is executed.
10. The method according to claim 1, wherein the tool is a cutter head gear cutting tool or a solid tool, each of the plurality of blades includes a cutting head including the inner cutting edge and the outer cutting edge, and the inner cutting edge and outer cutting edge are arranged on the cutting head to define a positive tip width.
11. The method according to claim 1, further including, in the first machine setting and in the second machine setting, inclining the tool in relation to the face coupling workpiece, and guiding the tool along an inclined path through the first tooth gap during machining thereof, wherein said inclined path, in an axial section through the face coupling workpiece, is generally parallel to a profile of a tooth base of the first tooth gap.
12. The method according to claim 11, wherein said tooth base of said tooth gap is inclined at a machine base angle in relation to an index plane of the face coupling workpiece.
13. The method according to claim 1, further comprising controlling a crowning of teeth of the face coupling workpiece by setting an inclination of the tool in relation to the face coupling workpiece.
14. The method according to claim 1, further comprising compensating for spiral angle errors of the face coupling workpiece by changing one or more of the first or second machine setting.
Description
DRAWINGS
[0045] An exemplary embodiment of the invention is described in greater detail hereafter with reference to the drawings.
[0046]
[0047]
[0048]
[0049]
[0050]
[0051]
[0052]
[0053]
DETAILED DESCRIPTION OF EMBODIMENTS
[0054] Terms are used in conjunction with the present description which are also used in relevant publications and patents. However, it is to be noted that the use of these terms is only to serve for better comprehension. The inventive concepts are not to be limited by the specific selection of the terms. At least some embodiments of the invention may be readily transferred to other term systems and/or technical fields. The terms are to be applied accordingly in other technical fields.
[0055] Gear cutting tools 100 having defined cutting edges are used in the scope of the various embodiments of the present invention. Primarily details of embodiments in which cutter head gear cutting tools are used are described in conjunction with the following description. However, the description can also be expanded to solid tools.
[0056] The reference sign 10 is used here both for the face coupling workpiece and also for the finish machined face coupling elements.
[0057]
[0058] Since the method of at least some embodiments of the invention is a continuous semi-completing method, the face coupling workpiece 10 and the gear cutting tool 100 are rotationally driven in a coupled manner. In
[0059] Variables which are identified here with a v each relate to the concave flanks 13.2 of the face coupling workpiece 10. Variables which are identified here with an x each relate to the convex flanks 13.1 of the face coupling workpiece 10. Additionally, variables which are identified here with an i relate to inner cutting edges or inner grinding surfaces and variables which are identified here with an a relate to outer cutting edges or outer grinding surfaces.
[0060] It is to be noted here that
[0061] The rotation center for machining the convex tooth flanks 13.1 is identified as M.sub.i and for machining the concave tooth flanks 13.2 is identified as M.sub.a (see
[0062] Because of the fact that in the gear cutting tool 100 of at least some embodiments of the invention, one outer cutting edge 21.a and one inner cutting edge 21.i were combined on cutting head 22, different tool radii r.sub.a>r.sub.i result. In addition, the spiral angle difference , which results between the index plane TE2 of the tool and the index plane TE1 of the workpiece (see
[0063] During the cutting of the concave flanks 13.2, because of a different machine setting in the index plane TE2 of the tool, an epicycloid flight path 13.2* of the outer cutting edge 21.a results. The epicycloid flank lines are shown by dot-dash lines in
[0064] It is to be noted here that the illustration of
[0065] The relative location of the gear cutting tool 100 in relation to the face coupling workpiece 10 is defined by the respective instantaneous setting of the machine (hereinafter called machine setting), in which the face coupling workpiece 10 is machined by milling. This setting during the machining of the convex flanks 13.1 is called the first machine setting here. The setting during the machining of the concave flanks 13.2 is called the second machine setting here.
[0066] The names first machine setting and second machine setting are not to specify a sequence here, but rather these names are merely used to be able to differentiate the two machine settings.
[0067] In the coordinate system of the tool 100, the cutting heads 22, or the blades 20, move along circular circles of rotation, the radius of which is determined by the distance of the blades 20 from the tool rotational axis R1. Details can be inferred from
[0068] Since the tool 100 is inclined during the machining of the concave and convex flanks in relation to the face coupling workpiece 10 (by inclining away or inclining toward, defined by the angle of inclination ), the cutting heads 22 move along elliptical flight paths during the rotational driving .sub.2 of the gear cutting tool 100, if one observes the movement thereof from the position of the face coupling workpiece 10. Because of the indexing movement (caused by the coupled rotation) of the face coupling workpiece 10 with the gear cutting tool 100, flanks result on the face coupling workpiece 10 which have the shape of an epicycloid, as already noted. In the method of at least some embodiments of the invention, the two rotational movements .sub.1 and .sub.2 are coupled so that only one cutting head 22 moves through a tooth gap 12 at a time. The next cutting head 22 of the gear cutting tool 100 moves through the next tooth gap 12 of the face coupling workpiece 10. In order that the chip angle of the rake surface 27 of the cutting heads 22 approximately corresponds to 0 during the cutting of the material of the face coupling workpiece 10, the cutting heads 22 are arranged with an offset on the gear cutting tool 100. This offset is shown in
[0069] The rotation center M of the face coupling workpiece 10 corresponds to the passage point of the tool rotational axis R1 through the plane of the drawing of
[0070] According to at least some embodiments of the invention, in the first machine setting, for example, all convex tooth flanks 13.1 of the tooth gaps 12 of the (not previously toothed) face coupling workpiece 10 are finish machined. This finish machining of the convex tooth flanks 13.1 is performed using the inner cutting edges 21.i of the tool 100. While the inner cutting edge 21.i of one cutting head 22 finish machines a convex tooth flank 13.1, the outer cutting edge 21.a of the same cutting head 22 carries out a pre-machining (also called roughing) of the concave tooth flank 13.2 of the same tooth gap 12. In the second machine setting, for example, all concave tooth flanks 13.2 of the tooth gaps 12 of the (not previously toothed) face coupling workpiece 10 are then finish machined.
[0071] It is to be noted that the dimensions of the cutting head 22 (especially the location of the inner cutting edge 21.i and the outer cutting edge 21.a, and also the tip width s.sub.a0, as schematically shown in
[0072] The first machine setting may include, according to at least some embodiments of the invention, for example, the following criteria or features: (1) in the first machine setting, all inner cutting edges 21.i are moved in relation to the face coupling workpiece 10 along a first elliptical flight path and all outer cutting edges 21.a are moved in relation to the face coupling workpiece 10 along a second elliptical flight path. In
[0073] According to at least some embodiments of the invention, a second machine setting is set in the machine to finish machine the concave tooth flanks 13.2.
[0074] The second machine setting differs from the first machine setting and it may include, according to at least some embodiments of the invention, for example, the following criteria or features: (1) in the second machine setting, all outer cutting edges 21.a are moved in relation to the face coupling workpiece 10 along a third elliptical flight path. In
[0075] As already indicated, the cutting heads 22, or the blades 20, of the gear cutting tool 100 may be guided in at least some embodiments along an inclined path B (see
[0076] If one wishes to achieve a constant tooth head play, it is advantageous to operate with the same profile of the inclined path B during the finish gear cutting of the concave flanks and during the finish gear cutting of the convex flanks. For optimization purposes, however, the inclined path B can have a slightly different profile during the finish gear cutting of the concave flanks than during the finish gear cutting of the convex flanks.
[0077] The face coupling 10 of at least some embodiments of the invention may include the following features. In all embodiments, it has an index cone angle , which is 90. In
[0078] The face coupling 10 of at least some embodiments of the invention may include the following features: a) it has teeth 11 having variable tooth head height, as can be seen in
[0079] The further details of the face coupling 10 of
[0080] According to at least some embodiments of the invention, an end milling cutter head is used as the cutter head gear cutting tool 100 in all embodiments. The end milling cutter head is equipped with multiple stick blades 20, which protrude on the end face from the gear cutting tool 100. A stick blade 20 preferably has a shape as shown as an example in
[0081] In the head region (identified here as the cutting head 22) of the stick blade 20, a first open surface 25, a second open surface 26, a (common) rake surface 27, a head open surface 28, an inner cutting edge 21.i, an outer cutting edge 21.a, and a head cutting edge 29 are located, for example.
[0082] The rake surface 27 intersects with the first open surface 25 in a virtual intersection line, which approximately corresponds to the profile of the inner cutting edge 21.i, or which exactly corresponds to the profile of the inner cutting edge 21.i. The rake surface 27 intersects with the second open surface 26 in a virtual intersection line which approximately corresponds to the profile of the outer cutting edge 21.a, or which exactly corresponds to the profile of the outer cutting edge 21.a.
[0083] However, the rake surface 27 does not have to be a flat surface, as shown in
[0084] The cutting heads 22, or the blades 20, respectively, are arranged in all embodiments with an offset in relation to the rotation center M, such that the rake surfaces 27 have a rake angle of zero in relation to the epicycloid. According to
[0085] Since one inner cutting edge 21.i and one outer cutting edge 21.a are each located on a common cutting head 22 (or blade 20, respectively), the rake angle=0 is to be ensured by the mentioned offset.
[0086] The present invention, as already noted, is a continuous semi-completing method. The opposing flanks 13.1, 13.2 of the face coupling workpiece 10 to be machined are machined using the same tool 100, but using different machine settings. Before, during, or after the adjustment of the machine setting from the first to the second or from the second to the first machine setting, in all embodiments, for example, a retraction movement and an infeed movement (broaching movement) can be executed.
[0087] Preferably, the adjustment of the machine setting is performed in all embodiments only after the tool 100 has been moved out of the tooth gaps 12.
[0088] The method of at least some embodiments of the invention can be executed, for example, on a bevel gear cutting machine, wherein the face coupling workpiece 10 is fastened on the workpiece spindle and the tool 100 is fastened on the spindle of the bevel gear cutting machine. There are numerous different gear cutting machines (for example, 5-axis and 6-axis gear cutting machines), in which the method of the invention can be carried out.
[0089] A suitable gear cutting machine is designed so that it specifies the mentioned coupled relative movements precisely using the tool 100 and the face coupling workpiece 10 in the engagement of the tool 100 with the face coupling workpiece 10.
[0090] Typical variables which can define a specific machine setting in this environment are the location of the rotation center M in relation to the location of the face coupling workpiece 10 (defined, inter alia, by the axis offset), the radial, the swivel angle, the machine base angle , the angle of inclination (tilt angle), the rotational position of the tool rotational axis R1, the roller swaying angle, and the depth position of the tool 100 in relation to the face coupling workpiece 10.
[0091] At least one of the mentioned typical variables is changed upon the transition from the first to the second machine setting.
[0092] The description above can also be applied to solid tools having fixed blades and not only to bar cutter heads.
[0093] As may be recognized by those of ordinary skill in the pertinent art based on the teachings herein, numerous changes and modifications may be made to the above described and other embodiments of the present invention without departing from the spirit of the invention as defined in the claims. Accordingly, this detailed description of embodiments is to be taken in an illustrative, as opposed to a limiting sense.