Machine tool control device, and machine tool
US-2024377804-A1 · Nov 14, 2024 · US
US10197987B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10197987-B2 |
| Application number | US-201514836384-A |
| Country | US |
| Kind code | B2 |
| Filing date | Aug 26, 2015 |
| Priority date | Aug 26, 2015 |
| Publication date | Feb 5, 2019 |
| Grant date | Feb 5, 2019 |
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A robotic tool is positioned relative to a feature of a component during a manufacturing process. The tool may be used to perform a manufacturing operation on the component. The tool is also be used to dispose a fiducial mark with a known registration to the feature, even if the feature is subsequently obscured. The position of tools for subsequent manufacturing operations are then set relative to the fiducial mark.
Opening claim text (preview).
What is claimed: 1. A method of creating fiducial marks on a component, the method comprising: identifying, with a sensing tool, a reference location on the component; moving a tool to a location having a predetermined spatial relationship to the reference location; using the tool, disposing a compound to create a fiducial mark on the component at the location; identifying, with the sensing tool, the fiducial mark; positioning one of the tool or a second tool relative to the identified fiducial mark; and using the one of the tool or the second tool, performing a manufacturing operation on the component. 2. The method of claim 1 , further comprising disposing a coating over the fiducial mark prior to positioning the one of the tool or the second tool relative to the fiducial mark. 3. The method of claim 1 , wherein identifying the fiducial mark comprises identifying a pattern of the fiducial mark. 4. The method of claim 1 , further comprising using a sensing system to determine a position of a tool with respect to the fiducial mark. 5. The method of claim 4 , further comprising positioning the tool for a manufacturing operation based on the position determination. 6. A method of manufacturing a wing of an airplane, the method comprising: identifying a first location on the wing; performing a manufacturing operation using a tool spatially positioned relative to the first location; creating a fiducial mark using the tool at a second location with a known spatial relationship to the first location; identifying the fiducial mark with a sensing system; determining a position of a tool with respect to the fiducial mark; and positioning the tool for a manufacturing operation based on the determined position. 7. The method of claim 6 , further comprising disposing a coating over the fiducial mark prior to identifying the fiducial mark. 8. The method of claim 6 , wherein identifying the fiducial mark comprises sensing a magnetic field generated by the fiducial mark. 9. The method of claim 6 , wherein identifying the fiducial mark comprises identifying a top edge and a side edge of the fiducial mark.
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