Curvature retaining device for plate-shaped workpiece, curvature retaining method for plate-shaped workpiece, and curvature forming method for plate-shaped workpiece
US-9802234-B2 · Oct 31, 2017 · US
US9682418B1 · US · B1
| Field | Value |
|---|---|
| Publication number | US-9682418-B1 |
| Application number | US-48696009-A |
| Country | US |
| Kind code | B1 |
| Filing date | Jun 18, 2009 |
| Priority date | Jun 18, 2009 |
| Publication date | Jun 20, 2017 |
| Grant date | Jun 20, 2017 |
A practical reading order for non-experts. Skip the full description unless you need deep technical detail.
What the patent document calls the invention.
A short plain-language summary of the technical disclosure.
Who owns or filed the patent and who is credited as inventor.
Filing, priority, publication, and grant dates set the timeline.
The legal scope of protection — read this for what is actually claimed.
Technology tags used to group this patent with similar filings.
Prior art links and similar publications in this corpus.
Official abstract text for this publication.
A method and apparatus for processing a sheet of material. The sheet of material may be secured relative to a tool in an incremental sheet metal forming machine. The sheet of material may be incrementally shaped into a shape of a part using a stylus. The stylus may comprise a rod having a first end and a second end, a substantially curved surface on the first end, and a texture on at least a portion of the substantially curved surface on the first end. The texture may be configured to channel a lubricant onto the first end.
Opening claim text (preview).
What is claimed is: 1. An incremental sheet forming apparatus comprising: a rod having a first end and a second end; a substantially curved surface on the first end in which the first end is configured to impinge a sheet of material to form a shape for a part; and a texture on at least a portion of the substantially curved surface on the first end, wherein the texture is configured to channel a lubricant onto the sheet of material; a platform configured to hold the sheet of material; a motion control system configured to control movement of the substantially curved surface to impinge the sheet of material to form the part; a lubrication system configured to supply the lubricant along an outer surface of the rod to the substantially curved surface while the substantially curved surface impinges the sheet of material; and wherein the lubricant on the substantially curved surface reduces undesired deformation of the sheet of material while the substantially curved surface impinges the sheet of material. 2. The incremental sheet forming apparatus of claim 1 , wherein the lubrication system comprises a storage tank configured to supply directly the lubricant along the outer surface of the rod to the substantially curved surface. 3. The incremental sheet forming apparatus of claim 2 further comprising: a number of sensors that identify a location of the rod and detect a force and a temperature sensed during impingement of the sheet of material by the substantially curved surface. 4. The incremental sheet forming apparatus of claim 2 , wherein the texture comprises one of grooves, dimples, pits, and holes. 5. The incremental sheet forming apparatus of claim 2 , wherein the storage tank is configured to be placed on top of the rod. 6. An incremental sheet forming apparatus for forming aircraft parts comprising: a stylus comprising a rod having a first end and a second end, a cradle associated with the first end, a ball associated with the cradle, a substantially curved surface on the ball, texture on at least a portion of the substantially curved surface on the first end, and a channel extending through the rod and the cradle to the ball, wherein the channel is configured to cause a lubricant to flow through the rod and the cradle and onto the substantially curved surface on the ball; a platform configured to hold a sheet metal material; a motion control system configured to control movement of the stylus to impinge the sheet metal material to form an aircraft part; and a lubrication system configured to supply the lubricant to the ball while the ball impinges the sheet metal material through the channel in the rod and in which the lubrication on the substantially curved surface reduces undesired deformation of the sheet metal material while the stylus impinges the sheet metal material; wherein the cradle has a first outside diameter and the rod has a second outside diameter and the first outside diameter is greater than the first outside diameter; and wherein the cradle surrounds and continuously contacts an approximate half of an outer spherical surface of the ball except for a region of the approximate half of the outer spherical surface of the ball where the cradle surrounds the channel. 7. The incremental sheet forming apparatus for forming aircraft parts of claim 6 , wherein the lubrication system comprises a storage tank configured to supply directly the lubricant to the ball through the channel in the rod. 8. The incremental sheet forming apparatus for forming aircraft parts of claim 7 , further comprising: a number of sensors that identify a location of the stylus and detect a force and a temperature sensed during impingement of the sheet metal material by the stylus. 9. The incremental sheet forming apparatus for forming aircraft parts of claim 7 , wherein the texture comprises one of grooves, dimples, pits, and holes. 10. The incremental sheet forming apparatus for forming aircraft parts of claim 7 , wherein the storage tank is configured to be placed on top of the stylus. 11. A method for processing a sheet of material, the method comprising: securing the sheet of material relative to a tool in an incremental sheet metal forming machine; incrementally shaping the sheet of material into a shape of a part using a stylus in which the stylus comprises a rod having a first end and a second end, a ball rotatably engaged in the first end, and a texture on at least a portion of the ball; and supplying a lubricant to the ball by supplying the lubricant along an outer surface of the stylus to the ball while the ball impinges the sheet of material. 12. The method for processing a sheet of material of claim 11 , wherein the supplying the lubricant to the ball comprises supplying directly from a storage tank the lubricant along the outer surface of the stylus to the ball. 13. The method for processing a sheet of material of claim 12 , the method further comprising: identifying a location of the stylus and detecting a force and a temperature during impingement of the sheet of material by the stylus, wherein the location, the force, and the temperature are sensed by a number of sensors. 14. The method for processing a sheet of material of claim 12 , wherein the texture comprises one of grooves, dimples, pits, and holes. 15. The method for processing a sheet of material of claim 12 , wherein the storage tank is configured to be placed on top of the stylus. 16. A method for manufacturing a part for an aircraft, the method comprising: securing a sheet metal material relative to a tool in an incremental sheet metal forming machine; and incrementally shaping the sheet metal material into a shape of the part by impinging the sheet metal material with a stylus in which the stylus comprises a rod having a first end and a second end; a substantially curved surface on the first end; a number of holes in at least a portion of the substantially curved surface on the first end, and a channel extending through the rod to the first end, in which the channel is configured to cause a lubricant to flow directly from a storage tank through the rod and through the number of holes onto the sheet metal material to maintain the lubricant on the sheet metal material; and wherein the rod and the substantially curved surface form the stylus in one piece. 17. The method for manufacturing a part for an aircraft of claim 16 , the method comprising: identifying a location of the stylus and detecting a force and a temperature during impingement of the sheet metal material by the stylus, wherein the location, the force, and the temperature are sensed by a number of sensors. 18. The method for manufacturing the part for the aircraft of claim 16 , wherein the storage tank is configured to be placed on top of the stylus. 19. The method for manufacturing the part for the aircraft of claim 16 , wherein the number of holes prevent the lubricant from being pressed away from a location where the stylus impinges on the sheet metal material.
Incremental shaping or bending, e.g. stepwise moving a shaping tool along the surface of the workpiece (B21D22/14 takes precedence) · CPC title
Incremental forging · CPC title
Lubricating during forging or pressing (lubricating in general F16N) · CPC title
Related publications grouped by family.
Answers are generated from the same data shown on this page.