METHOD AND TOOL FOR REMOVING A COATING FROM A SUBSTRATE
20200171617 ยท 2020-06-04
Assignee
Inventors
Cpc classification
B23B27/08
PERFORMING OPERATIONS; TRANSPORTING
B24B27/033
PERFORMING OPERATIONS; TRANSPORTING
B23B2215/24
PERFORMING OPERATIONS; TRANSPORTING
B23B29/03489
PERFORMING OPERATIONS; TRANSPORTING
B23B41/12
PERFORMING OPERATIONS; TRANSPORTING
B24B9/00
PERFORMING OPERATIONS; TRANSPORTING
C23C4/185
CHEMISTRY; METALLURGY
International classification
Abstract
The present invention relates to a method and a tool for removing a partial region of a coating from a substrate, in which the partial region to be removed is removed by a machining process in such a way that an undercutting of the partial region of the coating that is to be removed takes place. For the undercutting of the partial region of the coating that is to be removed, at least one machining tool that is rotating relative to the substrate about an axis of rotation is moved relative to the substrate along a direction of advancement that runs parallel to a surface having the coating, wherein a layer of the substrate that is directly adjacent to the coating is also removed together with the coating. Considered in the direction of advancement, the tool thereby penetrates deeper into the substrate than into the coating to be removed.
Claims
1. A method for removing a partial region of a coating from a substrate, wherein the partial region to be removed is removed by a machining process such that the partial region of the coating to be removed is undercut, wherein to undercut the partial region of the coating to be removed, at least one machining tool rotating relative to the substrate about an axis of rotation is moved relative to the substrate along a direction of advancement (V) which runs parallel to a surface having the coating, wherein together with the coating, a substrate layer directly adjacent to the coating is also removed and the tool, considered in the direction of advancement (V), penetrates deeper into the substrate than into the coating to be removed.
2. The method according to claim 1, wherein the machining tool is a cutting insert.
3. The method according to claim 1, wherein the direction of advancement (V) further runs parallel to the axis of rotation.
4. The method according to claim 1, wherein the substrate is a cylinder wall of a cylinder of a crankcase, wherein the direction of advancement (V) runs in the axial direction of the cylinder.
5. The method according to claim 1, wherein the tool is held on a rotating spindle.
6. The method according to claim 1, wherein the tool is mounted in a non-rotating manner and the substrate is rotated.
7. The method according to claim 1, wherein the tool is adjustable along the direction of advancement (V).
8. The method according to claim 1, wherein the substrate is adjustable along the direction of advancement (V).
9. The method according to claim 1, wherein the tool is held such that a cutting edge of the tool provided for removing the coating runs obliquely to the direction of advancement (V).
10. The method according to claim 1, wherein the removal of the partial region of the coating comprises a generation of a groove free of undercuts, in a partial section of the partial region of the coating to be removed, wherein the groove is generated using a tool other than the tool provided for undercutting the partial region of the coating to be removed.
11. A chipping tool, for performing a method according to claim 1, comprising a tool holder fastened to a spindle, which tool holder has at least one radially opposite cutting edge, which cutting edges are radially adjustable.
12. The method according to claim 9, wherein the tool is held such that a cutting edge of the tool provided for removing the coating runs at an angle of 30 to 60 to the direction of advancement (V).
13. The method according to claim 10, wherein the removal of the partial region of the coating comprises a generation of an annular groove.
14. The method according to claim 11, wherein the chipping tool is a grinding tool.
15. The method according to claim 11, wherein the tool holder has two radially opposite cutting edges.
16. The method according to claim 11, wherein the radially opposite cutting edge is a cutting edge arranged on a cutting insert.
Description
DRAWINGS
[0025] Further advantages result from the present description of the drawing. Exemplary embodiments of the invention are illustrated in the drawing. The drawing, the description and the claims contain numerous features in combination. The person skilled in the art will expediently also consider the features individually and combine them into useful further combinations.
[0026] Shown are:
[0027]
[0028]
[0029]
[0030]
[0031]
[0032]
[0033] An exemplary sequence of the method according to the invention is illustrated in
[0034] In the figures, identical or similar components are numbered with the same reference numerals.
[0035] The removal of a partial region 22 of a hard coating 20, which was applied by a thermal spray process on a soft substrate, namely an inner surface or cylinder wall 12 of a cylinder 10 of an aluminum crankcase 14 of an internal combustion engine, is explained by way of example.
[0036] In step 1 (
[0037] In step 2 (
[0038] In step 3 (
[0039] In step 4 (
[0040] Two opposing, radially adjustable clamping jaws 28 are provided on one end or front face of the tool holder 26, in which clamping jaws a respective cutting insert 30 is held as a machining tool. The tool holder 26 is illustrated again in
[0041] In step 5 (
[0042] In step 6 (
[0043] In step 7 (
[0044] An alternative embodiment of a tool holder 126, which also has two radially adjustable clamping jaws 128, in which a respective cutting insert 130 with a cutting edge 132 is held as a machining tool, is shown in
[0045] The tool holder 26 or 126 can advantageously have internal cooling, in which coolant is supplied to the cutting inserts 30, 130 via coolant channels provided in the interior of the spindle 24, 124 and the tool holder 26, 126.
[0046] The tool arrangement and the geometry of the cutting insert are illustrated in detail in
REFERENCE LIST
[0047] 10 cylinder [0048] 12 cylinder wall [0049] 14 crankcase, substrate [0050] 16 grinding tool [0051] 18 annular groove [0052] 20 coating [0053] 22 partial region [0054] 24, 124 spindle [0055] 26, 126 tool holder [0056] 28, 128 clamping jaw [0057] 30, 130 cutting insert [0058] 32, 132 cutting edge