Patent Grant
11155908
This disclosure is directed to a manufacturing system for parts that are formed, heat treated to increase yield strength, and assembled.
There is substantial interest in reducing the weight of parts used to manufacture vehicles such as automobiles, trucks, airplanes and boats for the purpose of improving fuel economy. One approach to reducing the weight of parts is to use light weight/high strength aluminum alloys to manufacture such parts.
The yield strength of parts made of supersaturated, heat treatable aluminum alloys may be increased by aging the parts over a substantial period of time. Waiting for natural aging to occur is generally not economically feasible in manufacturing processes due to the long period of time required, and further, will not result in the part reaching peak strength. Some parts are included in assemblies that are painted and baked in a paint oven, but the time and temperature of the paint bake oven may be inadequate to fully strengthen the parts.
Aging may be accelerated by heating the parts in a process referred to as “artificial aging.” For example, parts made of AA6111 series aluminum in the T4 temper may be artificially aged by heating the parts and can result in a doubling of the yield strength of the parts. Typically, it is not possible to form a given part after artificial aging due to the associated increase in yield strength and decrease in formability. Hence, it is desirable to manufacture such parts by forming when the parts are in the more formable T4 temper and subsequently artificially aging the parts to achieve the desired strength. Furthermore, the parts when processed in this manner will have less elastic recovery after forming. Pre-forming operations may include drawing, stretching, piercing, trimming, bending, extruding, forging or hydro-forming operations.
One problem with artificial aging is that it is impossible to determine by visual inspection whether the parts were subjected to the artificial aging process. A tensile test may be used to verify the yield stress of a part but a tensile test is destructive to the part. While a time consuming and relatively expensive hardness test could be used to test for artificial aging, these types of hardness tests may not be an accurate predictor of yield stress.
Structural beams, such as pillars, roof rails, frame parts, and the like once assembled to a vehicle may also be located in inaccessible areas that cannot be readily checked for yield strength. The yield strength of such parts may be critical to vehicle durability and/or vehicle quality. If it is determined that such structural parts lack the specified strength characteristics after the fact, costly corrective actions would be required such as replacing the part or adding a strengthening patch.
This disclosure is directed to solving the above problems and other problems as summarized below.
This disclosure provides a system and method for ensuring that parts are supplied to an assembly operation only after post forming heat treatment. A deposit of a heat sensitive ink is applied to the stamped or hydro-formed part after forming before the part has been heat treated. The heat sensitive ink irreversibly changes color during the heat treatment process to provide a visual indicator that the part was treated in the heat treatment process. A sensor or detector (such as an optical scanner, photo-detector, photocell, photoresistor, or video camera) is provided after the heat treatment process on the assembly line to verify the presence of the heat sensitive ink and the color of such heat sensitive ink. Any parts that lack the heat sensitive ink or parts that have heat sensitive ink in a color not indicative of experiencing the heat treatment process appropriately are rejected and removed from the assembly line or are otherwise prevented from advancing further in the assembly process.
According to one aspect of this disclosure, a method of manufacturing is provided that uses a part that is strengthened by heat treating. The method comprises forming the part and marking the part in a predetermined location with an irreversible thermo-chromatic composition. Next the part is heated to increase the strength of the part simultaneously changing the color of the thermo-chromatic composition. The color of the thermo-chromatic composition is detected after the heating step and a subsequent manufacturing process is controlled based upon the change in color of the thermo-chromatic composition.
According to other aspects of this disclosure, the irreversible thermo-chromatic composition may be a thermo-chromatic ink that changes color from white to a darker color, such as green or black. The step of forming the parts may include the step of stamping the parts in a sheet metal forming process. The step of marking the part may be accomplished by painting or marking with an atomizing or non-atomizing spray or contact or non-contact marker. Part marking is required in a location that is visible during the detecting step. The step of heating the part may be performed by heating the part to 170° C.-240° C. for more than 20 minutes.
The step of detecting the color of the thermo-chromatic composition may further comprise optically sensing the color of the paint with a machine vision detector that provides a signal to a controller of an assembly tool that operates on the part after the heating step. If the color of the thermo-chromatic composition has not changed or if the thermo-chromatic composition is not detected, the assembly tool is prevented from operating. The assembly tool may be, for example, a welder, a riveter, a fixture, or other tool. Alternatively, the machine vision detector may provide a signal to a data storage system that correlates the signal to an identification associated with the part and records that the color of the thermo-chromatic composition satisfactorily changed during the heating step.
According to another aspect of this disclosure as it relates to a manufacturing system, a post forming heat treatment system is disclosed for assuring part strengthening. The system includes an applicator for applying a thermo-chromatic composition to a predetermined location on the part. A heat treating oven that heats the part to a predetermined temperature for a predetermined time, wherein the heat treating oven changes the color of the thermo-chromatic composition from an as applied color to a heat changed color. A detector is directed toward the predetermined location that detects the presence of the thermo-chromatic composition and also detects whether the thermo-chromatic composition is the as applied color or the heat changed color. A controller receives a signal from the detector verifying that the thermo-chromatic composition is present and that the thermo-chromatic composition is the heat changed color.
According to other aspects of this disclosure as it relates to the manufacturing system, the system may further include a database for recording the signal from the detector and recording the signal in a field associated with a part identifier. The controller may be operatively connected to a machine that acts on the part after the heat treating oven. The machine may be prevented from operating if the signal from the detector is not received by the controller.
The system may alternatively include an apparatus for applying an applique that bears at least in part an irreversible thermo-chromatic composition to a predetermined location on the part. In the applique embodiment, a label or a hang tag is attached to the part instead of applying the thermo-chromatic ink or paint to the part directly.
The above aspects of this disclosure and other aspects will be described in greater detail below in the detailed description with reference to the attached drawings.
A detailed description of the illustrated embodiments of the present invention is provided below. The disclosed embodiments are examples of the invention that may be embodied in various and alternative forms. The figures are not necessarily to scale. Some features may be exaggerated or minimized to show details of particular components. The specific structural and functional details disclosed in this application are not to be interpreted as limiting, but merely as a representative basis for teaching one skilled in the art how to practice the invention.
Referring to
The blank is formed in its pre-treatment stage (e.g., T4 for aluminum alloys). The part may be formed in a conventional sheet metal forming line and may include a drawing operation, flanging operation, piercing operation, hemming operation, and the like. Alternatively, the part may be formed at 14 in a hydro-forming operation. In either event, the material is easier to form the desired part before heat treatment because the material is more malleable.
An irreversible thermo-chromatic ink is applied to the part at 16. The step of applying the thermo-chromatic ink is described with reference to
Alternatively, instead of applying paint to the part at 16, a hang tag, pressure sensitive label, or other applique that has a thermo-chromatic ink or paint may be attached to the part before the post forming heat treatment. The applique, hang tag, pressure sensitive label may be permanently attached to the part to prevent removal and must be heat resistant so that it is not harmed during the heat treatment process. The applique may be formed of or coated with a thermo-chromatic composition or otherwise bears the composition. The applique may be applied manually or with an attachment apparatus to a predetermined location on the part.
Referring to
In one example, a part made of AA6111 had an initial yield stress of about 150 MPa as received. One set of parts were cycled through a paint bake operation and the yield strength increased to about 175 MPa. Another set of parts were subjected to heat treatment over a period of 0 to 100 minutes at a temperature of 225° C. without prior exposure through the paint bake cycle and achieved a yield stress of about 280 MPa after 20 minutes. The parts were strengthened by more than 100 MPa as a result of heat treating as compared to parts that are only heated in the course of the paint baking operation. Parts that were heat treated as received were strengthened by more than 115 MPa after 30 minutes.
Referring to
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While exemplary embodiments are described above, it is not intended that these embodiments describe all possible forms of the invention. Rather, the words used in the specification are words of description rather than limitation, and it is understood that various changes may be made without departing from the spirit and scope of the invention. Additionally, the features of various implementing embodiments may be combined to form further embodiments of the invention.
This application is a division of U.S. application Ser. No. 13/928,580 filed Jun. 27, 2013, now U.S. Pat. No. 9,567,660 issued Feb. 14, 2017, the disclosure of which is hereby incorporated in its entirety by reference herein.
| Number | Name | Date | Kind |
|---|---|---|---|
| 3096184 | Gallop | Jul 1963 | A |
| 3750904 | Wisler | Aug 1973 | A |
| 4827423 | Beasley et al. | May 1989 | A |
| 5583178 | Oxman et al. | Dec 1996 | A |
| 5655592 | Sullivan | Aug 1997 | A |
| 5728241 | Gupta et al. | Mar 1998 | A |
| 6126730 | Yoshida et al. | Oct 2000 | A |
| 7491278 | Kropfl | Feb 2009 | B2 |
| 8057884 | Hauser et al. | Nov 2011 | B2 |
| 9657385 | Choi et al. | May 2017 | B2 |
| 20020025490 | Shchegolikhin | Feb 2002 | A1 |
| 20050139686 | Helmer et al. | Jun 2005 | A1 |
| 20050221514 | Pasadyn et al. | Oct 2005 | A1 |
| 20060099423 | Hauser et al. | May 2006 | A1 |
| 20070186417 | Smyth | Aug 2007 | A1 |
| 20090272171 | Golovashchenko | Nov 2009 | A1 |
| 20100107962 | Ricard et al. | May 2010 | A1 |
| 20120237694 | Lorentzen et al. | Sep 2012 | A1 |
| 20140236336 | Irick et al. | Aug 2014 | A1 |
| Number | Date | Country |
|---|---|---|
| 1665754 | Sep 2005 | CN |
| 103158290 | Jun 2013 | CN |
| 1055919 | Nov 2000 | EP |
| 63264683 | Nov 1988 | JP |
| 20050119996 | Dec 2005 | KR |
| 2008059242 | May 2008 | WO |
| 2010032002 | Mar 2010 | WO |
| Entry |
|---|
| Defense Quality and Standardization Office, Military Specification Heat Treatment of Aluminum Alloys, MIL-H-6088G, Apr. 1, 1991. |
| Disclosed Anonymously, “Post-Forming Heat Treatment of Aluminum Panels for High Strength Applications”, IP.com Prior Art Database Disclosure, Feb. 3, 2010, 1 page. |
| Number | Date | Country | |
|---|---|---|---|
| 20170130308 A1 | May 2017 | US |
| Number | Date | Country | |
|---|---|---|---|
| Parent | 13928580 | Jun 2013 | US |
| Child | 15405815 | US |
