METHOD OF REMOVAL OF HEAT CHECKING

Abstract

A system for removing a heat check feature on an aluminum casting formed by a high pressure die casting process is provided. The system includes a laser source, a robotic arm, and a heat check sensor. The heat check sensor develops a surface profile of at least part of the casting and transmits heat check feature information to the laser source to project the beam of laser light thereon. The projection of the beam of laser light can be varied in time and power, which can depend on surface profile information obtained from the sensor. Once at least a portion of the heat check feature is removed, the casting is placed against another part such that the joint interface is primarily the portion where the heat checking has been removed. Self-piercing rivets are then driven into the casting and the part to permanently join them together.

Claims

1. A method for removing a heat check feature from a casting comprising the steps of: providing a casting with a heat check feature; determining a location of the heat check feature; projecting a beam of laser light onto the heat check feature location; and removing at least a portion of the heat check feature with the beam of laser light.

2. The method of claim 1, wherein the step of determining the location of the heat check feature includes scanning the casting with a heat check sensor.

3. The method of claim 2, wherein the step of applying the beam of laser light includes moving the beam of laser light with a robotic arm.

4. The method of claim 3, wherein the step of scanning the casting includes moving the heat check sensor with the robotic arm.

5. The method of claim 1, further including changing the intensity of the beam of laser light based on the material used to form the casting.

6. The method of claim 1, wherein the step of determining the location of the heat check feature includes determining a location of the heat check feature on a joint interface and the step of removing the portion of the heat check layer includes removing the portion of the heat check layer on the joint interface.

7. The method of claim 6, further including providing a part and interfacing the part with the joint interface and connecting the joint interface of the casting to the part.

8. The method of claim 7, wherein the step of connecting the interface portion of the casting to the part includes driving at least one self-piercing rivet therethrough.

9. The method of claim 1, wherein the step of projecting the beam of laser light includes varying at least one of the speed of travel or intensity of projection of the beam of laser light.

10. The method of claim 1, wherein the step of projecting the beam of laser light includes pulsating the intensity of the beam of laser light.

11. The method of claim 1, wherein the step of determining the location of the heat check feature includes observing the heat check feature locations on previous castings.

12. The method of claim 1, wherein the step of determining the location of the heat check feature includes determining the depth of the heat check feature.

13. The method of claim 1, wherein the step of providing the casting with the heat check feature includes placing the casting on a casting holding fixture that includes a plurality of arms.

14. An assembly for removing a heat check feature from a casting comprising: a robotic arm; a heat check sensor for scanning a casting for a heat check feature; a control unit for receiving readings from the heat check sensor and developing a casting profile; and a laser head connected to the robotic arm, wherein the control unit directs the laser head with the robotic arm to project a beam of laser light onto at least a portion of the heat check feature based on the casting profile.

15. The assembly of claim 14, wherein the heat check sensor is located on the robotic arm.

16. The assembly of claim 14, wherein the casting profile includes a depth of the heat check feature.

17. The assembly of claim 14, wherein the laser head is configured to project the beam of laser light in a pulsating intensity.

18. The assembly of claim 14, further including a base with at least one arm for holding the casting with the heat check feature.

19. The assembly of claim 18, wherein the at least one arm includes a plurality of arms for holding the casting.

20. The assembly of claim 14, wherein the laser head is configured to project a beam of laser light of at least 3 kilowatts.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0011] The drawings described herein are for illustrative purposes only of selected embodiments and are not intended to limit the scope of the present disclosure. The inventive concepts associated with the present disclosure will be more readily understood by reference to the following description in combination with the accompanying drawings wherein:

[0012] FIG. 1A is a cross-section view of an exemplary cold chamber high pressure casting machine used with a heat checking removal system;

[0013] FIG. 1B is a plan view of a casting having a heat check feature;

[0014] FIG. 1C is a graphical representation of surface stresses on the casting resulting from cooling that relate to increased heat check feature;

[0015] FIG. 1D is a plan view of another casting with a heat check feature;

[0016] FIG. 1E is a plan view of the casting from FIG. 1D wherein the heat check feature has been partially removed by a grinding operation;

[0017] FIG. 2A is a side view of the heat checking removal system including a robotic arm and a laser;

[0018] FIG. 2B is an enlarged view of the heat check feature being removed from the casting;

[0019] FIGS. 2C and 2D illustrate a self-piercing rivet being driven into a portion of the casting that has had the heat check feature removed and another part;

[0020] FIGS. 3A and 3B illustrate a computer simulation of thermodynamic fatigue of a cover half of a mold assembly;

[0021] FIGS. 3C and 3D illustrate a computer simulation of thermodynamic fatigue of an ejector half of the mold assembly;

[0022] FIG. 4A is a method flow chart illustrating steps of removing the heat check feature with the heat checking removal system; and

[0023] FIG. 4B is another method flow chart illustrating steps of removing the heat check feature with the heat checking removal system in accordance with another aspect.

DESCRIPTION OF THE ENABLING EMBODIMENT

[0024] Example embodiments will now be described more fully with reference to the accompanying drawings. In general, the subject embodiments are directed to a system and process of removing heat checking from a casting surface by projecting a beam of laser light thereon. However, the example embodiments are only provided so that this disclosure will be thorough, and will fully convey the scope to those who are skilled in the art. Numerous specific details are set forth such as examples of specific components, devices, and methods, to provide a thorough understanding of embodiments of the present disclosure. It will be apparent to those skilled in the art that specific details need not be employed, that example embodiments may be embodied in many different forms and that neither should be construed to limit the scope of the disclosure. In some example embodiments, well-known processes, well-known device structures, and well-known technologies are not described in detail.

[0025] Referring to the Figures, wherein like numerals indicate corresponding parts throughout the views, the system and process of removing heat checking from a casting surface with a beam of laser light is shown to improve efficiency and accuracy. More particularly, the subject heat checking removal system 20 and process include determining the presence of heat checking on the surface of a recently casted part and selectively removing the heat check feature with the beam of laser light.

[0026] The heat checking removal system 20 may include a casting assembly 22 for initially forming the casting. A perspective view of an exemplary casting assembly 22 is shown in FIG. 1A. More particularly, the exemplary casting assembly 22 is illustrated as a cold chamber high pressure die casting assembly 22. The casting assembly 22 includes a mold 24 having an ejector half 24A and a cover half 24B. The cover half 24B and ejector half 24A move relative to one another and can be sealed together to form a cavity 40 therebetween. The cavity 40 defines the shape of the desired casting. Movement of the ejector half 24A and the cover half 24B is controlled by a clamping unit 26.

[0027] The clamping unit 26 includes a moveable platen 38 that moves towards and away from a stationary platen 32. The ejector half 24A includes an ejector plate 30 that moves with the moveable platen 38. The moveable platen 38 travels along one or more tie bars 28. Molten material may be initially stored in a furnace (not shown) and later fed into an injection assembly 34, whereafter it is injected into the cavity 40. The injection assembly 34 may include a sleeve 36 and a plunger 44 that pushes molten material therethrough and into the cavity 40. Cooling channels 48 may be located in to the mold 24. In operation, the furnace holds molten material until it is ready to be injected into the cavity 40 by the injection assembly 34. The molten material is then cooled until it solidifies into a desired shape or casting 42 and an outer heat check feature 46. Cooling may be expedited through a the cooling channels 48, however, the closer the cooling channels 48 are located to the molten material and the faster the adjacent molten material is cooled, the more the heat check feature 46 develops on the casting 42 (see FIGS. 1B and 1C). Removal of the casting 42 is facilitated by movement of the ejector plate 30. After removal, further quenching and treatment steps may be employed before removal of the heat check feature 46.

[0028] Description of the casting assembly 22 is exemplary in nature and may further utilize a high pressure die cast system (HPDC) to rapidly cool the molten material, as described in International Application No. PCT/US19/32099, entitled “Direct Chill Permanent Mold Casting System and Method of Same,” which is incorporated herein by reference. An enlarged view of the heat check feature 46 on a casting 42 is illustrated in FIG. 1B. The heat check feature 46 includes splits and channels extending into the surface of the casting 42. FIG. 1C is a graphical representation of compression and tensile stress within the casting resulting from cooling as a function of time, wherein faster cooling and increased stresses cause larger heat check features 46 that detract from athletics and workability. Another example casting 42 is shown in FIG. 1D, which may be formed from Aural-2 Aluminum Alloy. The example Aural-2 casting 42 has a thickness of 2.92 mm and the die has a heat check feature extends into the surface of the cavity at a depth of approximately 0.22 mm. Conventionally, this heat check feature transfers to the casting whereafter it is removed by a time-intensive grinding operation as shown in FIG. 1E. After the grinding operation, approximately 0.07 mm of the casting surface is removed such that the final thickness is approximately 2.85 mm and the casting suffers the afore described shortcomings including a porous surface.

[0029] Referring now to FIG. 2A, the heat checking removal system 20 includes a heat check removal assembly 100 that provides an improved heat check feature 46 removal over that illustrated in FIG. 1E. The heat check removal assembly 100 comprises a casting holding fixture 102, a laser source 104, a robotic arm 106, and a heat check sensor 108. Once the casting 42 has been cooled to solidification, ejected, and quenched, it is placed in the casting holding fixture 102. The casting holding fixture 102 preferably is configured to make limited contact with the casting 42 such that a heat check feature 46 removal operation can be applied to as much of the casting 42 as possible without interruption from the casting holding fixture 102. In one embodiment, the casting holding fixture 102 includes a base 110 and a at least one arm 112 arranged to hold the casting 42 at specific and predetermined points. The at least one arm 112 may include a plurality of thin arms 112. Once the casting 42 has been placed in the casting holding fixture 102, the heat check sensor 108 provides a surface profile of the casting 42 to determine areas and the depth of the heat check feature 46. The heat check sensor 108 may be operational during the heat checking removal operation to provide real-time or updated readings to ensure the entire heat check feature is removed. Once a profile has been developed, the laser source 104 includes a laser head 114 that focuses the beam of laser light onto the various predetermined heat check feature 46 locations. The laser head 114 is attached to and directed by the robot arm 106 based on profile readings from the heat check sensor 108. At least one power source 116 provides electrical energy to the various components of the heat checking removal system 20. The laser head 114 can also include a fiber-optic cable between the laser source 104 and the laser head 114. Alternatively, the laser source 104 may also be attached to the laser head 114 within a same housing. The laser head 114 may include a one or more lenses and mirrors and the laser source 104 may include other components to develop the initial beam of laser light. The laser head 114 may be removably attached to the robot arm 106 via a mounting bracket 115. A control unit 118 communicates with the heat check sensor 108, the robotic arm 106, and the laser source 104, and directs the laser head 114 towards the heat check feature 46 locations.

[0030] The control unit 118 may be configured such that the operation of the heat check removal assembly 100 is at least partially automated. More particularly, the control unit 118 may include a processor 120 and a memory 122 having machine readable non-transitory storage. Programs and/or software 124 (such as Arduino IDE, Windows, Linux, Android, iOS) may be saved on the memory 122 for carrying out instructions. In addition to automated software 124, a user interface 126 may be in communication with the control unit 118 for providing input data 128 or instructions for operation of the heat check removal assembly 100. In addition to the software 124 and input data 124, profile data 130 transmitted via the heat check sensor 108 may also be saved on memory. These various elements provided in conjunction with the control unit 118 allow for a specific implementation. Thus, one of ordinary skill in the art of electronics and circuits may substitute various components to achieve a similar functionality. In operation, certain values may be initially set with user interface 126, for example, the material of the casting, the shape of the casting, or a predetermined removal depth per pass of the beam of laser light. Next, the heat check sensor 108 scans the casting and develops profile data 130. The control unit 118 then directs the robotic arm 106 to move the beam of laser light over areas of the casting 42 that have been identified to have heat check features 46. After passage of the beam of laser light, the heat check sensor 108 may take a second profile to ensure that the heat check feature levels meet a quality threshold. In addition, once the heat check feature presence is at a threshold low amount, the control unit 118 may reduce the power or intensity of the beam of laser light for a final pass to provide a smooth finished surface. Depending on the depth of the heat check feature 46, the control unit 118 may increases the power of the laser head 114 via increased output from the power source 116 or slow the movement of the robotic arm 106 to increase the amount of time the laser head 114 is applied to the heat check feature 46. The control unit 118 may also instruct the projection of the beam of laser light to be pulsed to effectively dislodge the heat checking in certain instances.

[0031] The heat check sensor 108 may be attached or separate from the robotic arm 106. The heat check sensor 108 may develop a real-time profile simultaneously as the laser head 114 directs the beam of laser light to remove the heat check feature 46. For example, the heat check sensor 108 may take an initial measurement to develop a first profile and, after or during the projection of the beam of laser light, take a second profile of locations where the heat check feature 46 has been at least partially removed by the beam of laser light to determine if there has been adequate removal within a predetermined threshold. The heat check sensor 108 determines both the location and the depth of the heat check feature 46 via the presence and the depth of surface cracks. For example, during scanning, the heat check sensor 108 may measure the distance between the heat check sensor 108 and the surface such that cracks provide reading of being located at a further distance from the heat check sensor 108. Once a location of heat check features 46 is discovered by heat check sensor 108, the control unit 118 directs the robotic arm 106 to project the beam of laser light via the laser head 114 on heat check feature 46 locations. This projection can be pulsed, uniform, or otherwise of varying strength. For example, the beam of laser light may be initially pulsed in order to dislodge the heat checking from casting and then uniform for smoothing out a surface of the casting 42. Further quenching and treatment steps may be employed after removal of the heat check feature 46.

[0032] As best illustrated in FIGS. 2C and 2D, the heat check removal assembly 100 may further include a rivet driver 132 to drive self-piercing rivets (S.P.R.) 134 into the portion of the casting 42 where the heat check feature 46 has been removed. More particularly, an interface surface 138 between the casting 44 and a second part 136 may be initially determined before removing the heat check feature 46 at least on the interface surface 138. As such, the interface surface 138 is smooth and can sit flush against the second part 136 before connection therewith. In addition to the use of self-piercing rivets 132, other means of connection could be used including adhesive, fasteners, etc.

[0033] The laser head 114 is preferably a Fiber laser with a minimum 3 kilowatt beam of laser light output and is applied to the casting in a 100 μm diameter at a motion speed of 1 m/s. The beam of laser light output may be above 900 nm, above 1000 nm, between 900 nm to 1200 nm, between 1000 nm to 1100 nm, or at approximately 1064 nm. The laser source 104 may thus include a plurality of diode-laser pump modules for power scaling the beam of laser light output. While the casting 42 has been described as aluminum or aluminum alloy, the castings may also be formed of different materials. Similarly, while the casting process has been described as a high pressure die casting process “H.P.D.C.,” other casting processes may be deployed without departure from the subject disclosure. It should also be appreciated that the laser source 104 and head 114 and interrelated parts can be provided as a cathode laser, a gas laser, a solid state laser, etc.

[0034] The heat check surface 46 can also be determined by advanced casting simulations of the mold 24 instead of the casting 44. FIGS. 3A through 3D show computer simulations of an x-ray analysis of thermodynamic fatigue on exemplary front shock tower tooling surfaces that cause heat checking. The computer simulations are based on empirical physics and can also be calibrated by overserving tool features. For example, in instances in which HPDC is utilized, the molten material enters the cavity with enough velocity to damages the walls. Based on a combinations of historical wear patterns, fluid dynamics, etc., an accurate model can be developed. With specific reference to FIGS. 3A and 3B, the cover half 24B is shown after a number of cycles showing crack initiation. Looking now to FIGS. 3C and 3D, the ejector half 24A is shown after a number of cycles showing additional problematic crack initiation. The different areas of the tooling presented in FIGS. 3A through 3D can be included in profile data 130 as problematic areas. Moreover, trends in profile data 130 taken from the heat check sensor 108 may be indicative of tooling fatigue. For example, if numerous castings exhibit localized areas affected by heat checking than others, such trends may be noted and communicated to a user via the user interface 126. The x-ray analysis may also be performed on the castings 44.

[0035] A process 200 of removing a heat check feature 46 is presented in FIG. 4A. The process 200 begins by introducing 202 molten material in a mold. The molten material is cooled 204 until it is at least partially solidified. Once the casting has solidified, it is transferred 206 to a casting holding fixture. The step of transferring the casting 206 can also include initially transferring the casting to a water quench tank off the die casting machine and afterwards placing it into a shear trim to remove any biscuit, gate, runner, and overflow. The step of transferring the casting 206 may also include performing an x-ray analysis on the casting or mold to developing a quality profile (see FIGS. 3A through 3D) before the part is transferred to a casting holding fixture. The casting is then placed 208 on discrete points of the casting holding fixture. After placement, a heat check sensor scans 210 the surface of the casting for heat check cracks to develop a profile 212 that includes the location of heat checking. Profile information may include inputs from a user interface as previously described. The heat check sensor may determine the location 214 and depth 215 of the heat checking and incorporate that information into the profile. Profile information is sent to a control unit 216 and may be saved in a local memory. Based on the profile, the control unit provides instructions 218 to a robotic arm to project a beam of laser light onto areas of the casting that have heat checking. The instructions can include projecting a pulsed, uniform, or varying strength beam of laser light. These instructions can include outlining where regions 220 the beam of laser light needs to be applied, providing a length of time or speed 221 that the beam of laser light needs to be applied to the surface, and providing a recommended power or intensity of the beam of laser light 222. These additional instructions can depend on profile data including the location of the heat checking, the shape 223 of the desired casting, and the depth of the heat check feature. The robotic arm then applies a beam of laser light 224 to the regions of heat checking and burns the heat check feature 226 until it is at least partially, substantially, or completely removed. For example, the beam of laser light may be initially pulsed in order to dislodge the heat checking from casting and then uniform for a constant surface. While these steps may be in chronological order, they can occur real-time as the heat checking sensor can be attached directly on the robotic arm to develop a profile on one area of the casting while the beam of laser light removes heat checking from another area of the casting, simultaneously. The step of projecting the beam of laser light may include using a diode laser to project a beam of laser light at 100 μm and 1 m/s at a 3 kilowatt power. The application step may further include pulsing the beam of laser light strength or intensity to effectively dislodge portions of the heat checking. The beam of laser light can be applied to the heat checking until the surface has aesthetic criteria (Ra) equal to 10. For certain applications, the projection of the beam of laser light and corresponding burning and removal of the heat check feature is only provided to certain areas of the casting. More particularly, the beam of laser light is only projected onto a localized area 228 that is predetermined based on a certain operational criteria. For example, when the casting is to be joined to another part, the contact area of the localized area of the casting (i.e., the joint) may be the only localized area to receive a beam of laser light projection. Once the heat checking is removed from the localized area, the casting placed over the part such that the localized area forms a majority of the joint 230 interface, with the joint being primarily flush contact. Self-piercing rivets (S.P.R.) are then driven 232 into either the part and/or the casting to join them together.

[0036] Another method 200′ is presented in FIG. 4B. The method 200′ is similar to the method illustrated in FIG. 3A but does not include using a sensor to locate the heat check feature. Instead, the method 200′ includes a step of checking or hypothesizing the heat check layer/feature 211 location with other means. The step of locating the heat check feature 211 can include associating the heat check locations based on previous castings, automatically projecting the beam of laser light to certain areas of the casting to remove a specific amount of surface, or may alternatively include other methods of locating the heat check feature 211 in order to direct the beam of laser light. These other methods can include visual or computer assisted locating (see FIGS. 3A through 3D). Moreover, the step of locating the heat check feature 211 may include initially forming the casting with excess thickness and using the beam of laser light to remove the excess thickness.

[0037] The casting may comprise of non-ferrous alloys such as aluminum, aluminum alloy, magnesium, or zinc.

[0038] In one embodiment illustrated in FIG. 5A, the aluminum alloy of the casting 42 comprises, in weight percent (wt. %) based on the total weight of the alloy: Silicon (minimum 9.5 wt. %, maximum 11.5 wt. %); Iron (no minimum, maximum 0.25 wt. %); Manganese (minimum 0.40 wt. %, maximum 0.60 wt. %); Magnesium (minimum 0.10 wt. %, maximum 0.60 wt. %); Strontium (minimum 0.010 wt. %, maximum 0.025 wt. %); Titanium (no minimum, maximum 0.12 wt. %); Aluminum; and other elements individually not more than 0.05 w. % and in aggregation not more than 0.15 w. %.

[0039] In yet another embodiment illustrated in FIG. 5B, the aluminum alloy of the casting 42 comprises, in weight percent (wt. %) based on the total weight of the alloy: Silicon (minimum 6.0 wt. %, maximum 8.0 wt. %); Iron (no minimum, maximum 0.25 wt. %); Manganese (minimum 0.40 wt. %, maximum 0.60 wt. %); Magnesium (minimum 0.10 wt. %, maximum 0.60 wt. %); Strontium (minimum 0.010 wt. %, maximum 0.030 wt. %); Titanium (no minimum, maximum 0.15 wt. %); Aluminum; and other elements individually not more than 0.05 w. % and in aggregation not more than 0.15 w. %.

[0040] It should be appreciated that the foregoing description of the embodiments has been provided for purposes of illustration. In other words, the subject disclosure it is not intended to be exhaustive or to limit the disclosure. Individual elements or features of a particular embodiment are generally not limited to that particular embodiment, but, where applicable, are interchangeable and can be used in a selected embodiment, even if not specifically shown or described. The same may also be varies in many ways. Such variations are not to be regarded as a departure from the disclosure, and all such modifications are intended to be included within the scope of disclosure.