Process for producing holes
Abstract
A method of producing holes in a component, in particular of turbomachines, wherein each hole extends from a first, outer surface to a second, inner surface of the component and wherein the method has, for example, the following steps: producing a 3D model of the actual geometry of the component, at least for the region of the holes; adopting each hole on the basis of the actual geometry of the component; generating a production program for each individual hole. In this way, the process quality and with it the quality of the holes increases, because the offset of holes caused by component tolerances is avoided and the drilling funnels are formed according to specification. Furthermore, drilling defects on account of the offset of holes and/or cores can be avoided. Overlapping holes caused by component tolerances are likewise avoided.
Claims
exact text as granted — not AI-modified1 . A process for producing holes in a component, wherein each hole extends from a first surface at the exterior of the component to a second surface at the interior of the component and wherein the process comprises the following steps:
developing a 3-D model of the geometry of said component, adapting each hole on the basis of said geometry of the component; and generating a production program for each individual hole.
2 . The process according to claim 1 wherein the geometry of said component is the actual geometry.
3 . The process according to claim 2 , wherein said component is a turbo engine.
4 . The process according to claim 2 , wherein said 3-D model of the geometry is developed for the area of the holes.
5 . The process according to claim 1 , further comprising correcting the deviation of the position of the component in a clamping device.
6 . The process according to claim 5 , wherein the correction of deviation is based on the geometry of the outer surface of the component.
7 . The process according to claim 1 , further comprising the additional step of at least one of calculating and measuring the drilling depth of at least one hole.
8 . The process according to claim 4 , further comprising the additional step of at least one of calculating and measuring the drilling depth of at least one hole.
9 . The process according to claim 5 , further comprising the additional step of at least one of calculating and measuring the drilling depth of at least one hole.
10 . The process according to claim 1 , wherein said step of generating a production program further comprises developing and storing process parameters and at least one transformation matrix.
11 . The process according to claim 5 , wherein said step of generating a production program further comprises developing and storing process parameters and at least one transformation matrix.
12 . The process according to claim 6 , wherein said step of generating a production program further comprises developing and storing process parameters and at least one transformation matrix.
13 . The process according to claim 7 , wherein said step of generating a production program further comprises developing and storing process parameters and at least one transformation matrix.
14 . The process according to claim 8 , wherein said step of generating a production program further comprises developing and storing process parameters and at least one transformation matrix.
15 . The process according to claim 9 , wherein said step of generating a production program further comprises developing and storing process parameters and at least one transformation matrix.
16 . The process according to claim 1 , wherein said developing a 3-D model step further comprises using computer tomography to develop said 3-D model of the geometry of the component.
17 . The process of claim 16 wherein said geometry of the component is the actual geometry.
18 . The process according to claim 5 , wherein said developing a 3-D model step further comprises using computer tomography to develop said 3-D model of the geometry of the component.
19 . The process of claim 18 wherein said geometry of the component is the actual geometry.
20 . The process according to claim 6 , wherein said developing a 3-D model step further comprises using computer tomography to develop said 3-D model of the geometry of the component.
21 . The process of claim 20 wherein said geometry of the component is the actual geometry.
22 . The process according to claim 7 , wherein said developing a 3-D model step further comprises using computer tomography to develop said 3-D model of the geometry of the component.
23 . The process of claim 22 wherein said geometry of the component is the actual geometry.
24 . The process according to claim 8 , wherein said developing a 3-D model step further comprises using computer tomography to develop said 3-D model of the geometry of the component.
25 . The process of claim 24 wherein said geometry of the component is the actual geometry.
26 . The process according to claim 9 , wherein said developing a 3-D model step further comprises using computer tomography to develop said 3-D model of the geometry of the component.
27 . The process of claim 26 wherein said geometry of the component is the actual geometry.
28 . The process according to claim 1 , wherein said developing a 3-D model step further comprises using an optical measuring process to develop said 3-D model of the geometry of the component.
29 . The process of claim 28 wherein said geometry of the component is the actual geometry.
30 . The process according to claim 5 , wherein said developing a 3-D model step further comprises using an optical measuring process to develop said 3-D model of the geometry of the component.
31 . The process of claim 30 wherein said geometry of the component is the actual geometry.
32 . The process according to claim 6 , wherein said developing a 3-D model step further comprises using an optical measuring process to develop said 3-D model of the geometry of the component.
33 . The process of claim 32 wherein said geometry of the component is the actual geometry.
34 . The process according to claim 7 , wherein said developing a 3-D model step further comprises using an optical measuring process to develop said 3-D model of the geometry of the component.
35 . The process of claim 34 wherein said geometry of the component is the actual geometry.
36 . The process according to claim 8 , wherein said developing a 3-D model step further comprises using an optical measuring process to develop said 3-D model of the geometry of the component.
37 . The process of claim 36 wherein said geometry of the component is the actual geometry.
38 . The process according to claim 9 , wherein said developing a 3-D model step further comprises using an optical measuring process to develop said 3-D model of the geometry of the component.
39 . The process of claim 38 wherein said geometry of the component is the actual geometry.
40 . The process according to claim 10 , further comprising the step of using respective transformation of a set of sample data to produce one or more components having a similar geometry in parallel.
41 . The process according to claim 10 , wherein said production program comprises at least one of traversing paths, removal volumes and process parameters.
42 . The process according to claim 1 , wherein the holes are generated by at least one of cutting, laser removal, electrochemical processing, and erosion.
43 . The process according to claim 5 , wherein the holes are generated by at least one of cutting, laser removal, electrochemical processing, and erosion.
44 . The process according to claim 6 , wherein the holes are generated by at least one of cutting, laser removal, electrochemical processing, and erosion.
45 . The process according to claim 7 , wherein the holes are generated by at least one of cutting, laser removal, electrochemical processing, and erosion.
46 . The process according to claim 8 , wherein the holes are generated by at least one of cutting, laser removal, electrochemical processing, and erosion.
47 . The process according to claim 9 , wherein the holes are generated by at least one of cutting, laser removal, electrochemical processing, and erosion.
48 . A production arrangement for producing holes in a component, said arrangement comprising:
a central computer unit connected to a device for developing a 3-D model of the geometry of the component; at least one device for automatically adapting each hole based on the geometry of the component; and at least one device for automatically generating production programs for each hole;
wherein each hole extends from a first surface at the exterior of the component to a second surface at the interior of the component.
49 . The production arrangement of claim 48 wherein said geometry of the component is the actual geometry.
50 . The production arrangement of claim 48 , wherein said component is a turbo engine.
51 . The production arrangement according to claim 48 , further comprising an automatic drilling tool connected to the computer unit.Join the waitlist — get patent alerts
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