US2008183325A1PendingUtilityA1

Process for producing holes

Assignee: KRIEGMAIR JOSEFPriority: Sep 6, 2005Filed: Feb 29, 2008Published: Jul 31, 2008
Est. expirySep 6, 2025(expired)· nominal 20-yr term from priority
Inventors:Josef Kriegmair
B23P 2700/06Y10T408/03B23K 26/388Y10T408/08G05B 19/402B23K 26/389G05B 19/4099B23K 26/384
38
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Claims

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-modified
1 . 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.

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