Method and tool for producing an exact-fit cylindrical bore by removal of material from an existing bore with a finishing allowance
09919389 · 2018-03-20
Assignee
Inventors
Cpc classification
Y10T409/501804
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
B23B27/00
PERFORMING OPERATIONS; TRANSPORTING
Y10T29/5168
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
Y10T409/503116
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
Y10T408/89
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
B21D28/34
PERFORMING OPERATIONS; TRANSPORTING
Y10T409/502788
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
B23D13/00
PERFORMING OPERATIONS; TRANSPORTING
Y10T29/5115
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
B23D11/00
PERFORMING OPERATIONS; TRANSPORTING
Y10T409/502952
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
B23D43/02
PERFORMING OPERATIONS; TRANSPORTING
B23C7/04
PERFORMING OPERATIONS; TRANSPORTING
B23B35/00
PERFORMING OPERATIONS; TRANSPORTING
B23P13/02
PERFORMING OPERATIONS; TRANSPORTING
Y10T408/356
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
B23D79/00
PERFORMING OPERATIONS; TRANSPORTING
Y10T409/500984
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
Y10T408/78
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
Y10T29/49995
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
B23B2215/24
PERFORMING OPERATIONS; TRANSPORTING
Y10T409/303808
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
Y10T409/50082
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
B23B27/10
PERFORMING OPERATIONS; TRANSPORTING
Y10T408/45
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
Y10T409/509348
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
B23D79/04
PERFORMING OPERATIONS; TRANSPORTING
B23D5/02
PERFORMING OPERATIONS; TRANSPORTING
International classification
B23P13/02
PERFORMING OPERATIONS; TRANSPORTING
B23C3/12
PERFORMING OPERATIONS; TRANSPORTING
B23D11/00
PERFORMING OPERATIONS; TRANSPORTING
B23D13/00
PERFORMING OPERATIONS; TRANSPORTING
B23D79/04
PERFORMING OPERATIONS; TRANSPORTING
B23D79/02
PERFORMING OPERATIONS; TRANSPORTING
B23D5/02
PERFORMING OPERATIONS; TRANSPORTING
B23B51/06
PERFORMING OPERATIONS; TRANSPORTING
B21D28/34
PERFORMING OPERATIONS; TRANSPORTING
B23B35/00
PERFORMING OPERATIONS; TRANSPORTING
B23C3/00
PERFORMING OPERATIONS; TRANSPORTING
B23C7/04
PERFORMING OPERATIONS; TRANSPORTING
B23D79/00
PERFORMING OPERATIONS; TRANSPORTING
B23B27/00
PERFORMING OPERATIONS; TRANSPORTING
Abstract
The provided method and material-removing tool serve for producing an exact-fit cylindrical bore with a high degree of surface quality and a length that may be a multiple of the diameter from an existing bore with a finishing allowance. In order to reduce the time taken for the finishing by means of a reamer to be performed, it is proposed to use a tool in the form of an impact die, which is formed at the front end with a circular or substantially circular cutting edge, the diameter of which corresponds to the nominal diameter of the bore to be produced, and which tapers from directly behind the cutting edge or behind a front region of a certain length.
Claims
1. A method for material-removing machining of a cylindrical bore having a length that is a multiple of a diameter of the bore, the method comprising: providing the cylindrical bore, which cylindrical bore is a pre-processed bore which includes a finishing allowance, peeling off the finishing allowance to a nominal diameter of a finish-machined bore with an impact die that has at its front end a circular or substantially circular cutting edge and that performs an axial stroke in the direction of the length of the cylindrical bore, wherein the cylindrical bore is a blind bore, and wherein the impact die is provided with a milling or drilling head attached axially forwardly of the circular or substantially circular cutting edge, the method further comprising rotating the impact die to prepare a bottom of the blind bore via the milling or drilling head.
2. The method of claim 1, further comprising superimposing a rotary motion of the impact die on the axial stroke of the impact die, wherein the ratio of the feed speed of the impact die during the axial stroke to a rotation speed of the impact die during the rotary motion is either constant or varies.
3. The method of claim 2, wherein the rotary motion of the impact die superimposed on the axial stroke of the impact die has a rotation speed of at least 1 rpm.
4. The method of claim 2, wherein a rotation speed of the rotary motion is at least 2,000 rpm.
5. The method of claim 4, wherein the rotation speed is at least 30,000 rpm.
6. The method of claim 1, wherein a cutting speed during the axial stroke is 5 m/min to 150 m/min.
7. The method of claim 1, wherein a cutting speed during the axial stroke is 30 to 90 m/min.
8. The method of claim 1, wherein a cutting speed during the axial stroke for bore diameters of up to 20 mm is 50 to 80 m/min.
9. The method of claim 8, wherein during the axial stroke and a return stroke, friction between the bore wall and the impact die is limited by a taper of the impact die at its front end.
10. The method of claim 1, characterized in that during the axial stroke, the front end of the impact die is guided on a bore wall behind the cutting edge.
11. The method of claim 2, wherein the rotary motion of the impact die superimposed on the axial stroke of the impact die produces rifling with a twist in a bore wall.
12. The method of claim 11, wherein the rifling has a slope of between 1 and 75.
13. The method of claim 11, wherein the rifling has a slope of between 10 and 15.
14. The method of claim 1, wherein the diameter of the milling or drill head is less than the diameter of the cutting edge.
Description
BRIEF DESCRIPTION OF THE DRAWING
(1) Other details, advantages and features of the invention will become apparent not only from the claims, from the features recited thereinseverally and/or in combination, but also from the following description of preferred exemplary embodiments illustrated in the drawing.
(2) The drawing shows in:
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DETAILED DESCRIPTION OF PREFERRED EMBODIMENTS
(33) The tool shown in
(34) The impact die according to
(35) Different from the aforedescribed embodiment, the taper of the impact die may start already directly at the cutting edge 14. The conicity of the taper of the taper could, however, be chosen to be significantly smaller, for example, only about one to two m along longitudinal sections of 20 mm. In this case, the taper has only a minimal effect directly behind the cutting edge, so that it can be assumed that the front section 16 of
(36) In contrast to
(37) The circumferential surface of the impact die 10 should be devoid of a cutting edge outside of the front face cutting edge, as shown in
(38) The embodiment of
(39) The layer thickness of a diamond layer produced of PCD or CBN or a CVD process should be between 0.1 and 3 mm, without limiting the scope of the invention. The thickness of the layer depends on the material in which the bore is to be introduced, i.e. its elasticity, so that upon withdrawal of the impact die 10 the elastic nestling of the material acts mainly on the cutting material. Furthermore, the distance between the joint or soldering zone 15 and the hard metal support 15, which is integrally connected with the impact die 10, should be at a distance 3-8 mm from the front face of the hard metal layer 15 in order to prevent unintended forces during withdrawal caused by the elastic return of the material into which the bore is introduced. In particular, the distance should be at least 3.2 mm or more. The connection zone or soldering zone 15 extends in the region of the shank of the impact die 10 which has a smaller diameter compared to the cutting edge.
(40) If it is found in a specific situation that the most forward portion of the impact die also wears in the region where the diameter still essentially the same size as the diameter of the cutting edge 14, because the taper is practically noticeable only behind the cutting edge 14, the entire front region of the impact die should advantageously be made of the extremely hard cutting material.
(41) The tool illustrated in
(42) Instead of the depressions 26 shown in
(43) In the embodiment of
(44) The polygonal shape of the cutting edge is best seen in
(45) As previously described, to produce a bore with a precise fit, the impact die 10 having the cutting edge 14 performs substantially exclusively an axial stroke, on which optionally a rotary motion forming a twist in the inner wall of the bore is superimposed such that grooves or rifling are produced in the inner wall bore, wherein the slope angle should be between 1 and 75, preferably between 10 and 15.
(46) A rotary motion, in particular at high rotation speed, should be carried out in addition to the stroke motion. The rotary motion can run synchronously or asynchronously with the impact movement. Synchronous indicates here that the rotary motion is superimposed on the impact movement such that the ratio of the stroke speed and rotation speed is constant. In an asynchronous motion, the relation between impact speed and rotation speed varies, which can facilitate advance and return. Static friction is avoided or reduced to a degree so that only dynamic friction occurs. As a result, the impact die 10 can be rotated during impact with a rotation speed of, for example, 2000 rpm or more or less, in particular a rotation speed of 30,000 rpm or more. The stroke should be in a range of 5 m/min or more, and in particular up to 150 m/min. However, the teaching according to the invention is not limited by these numerical values.
(47) It may be appropriate or necessary in individual cases to form a bore to be finish-machined with the impact die as a blind bore. For such applications, a tool according to
(48) The milling or drill head 30 and 32, respectively, may be integrally formed with the impact die 10 or manufactured individually and firmly attached to the front end of the impact die 10, for example soldered. The diameter of the milling or drill head 30 and 32 should not be larger, preferably slightly less, than the cutting edge 14. In the exemplary embodiments according to
(49) Since the surface of the bottom of the blind bore is machined by rotating and axially advancing the tool, the rifling in the bore wall mentioned with reference to