The described embodiments relate generally to aluminum enclosures for consumer products and methods for forming the same. Methods include alternative manufacturing processes for producing cosmetically appealing aluminum enclosures.
Enclosures for consumer products, such as consumer electronic products, are often made of stainless steel due to the durability and corrosion resistance of stainless steel. Typically, the enclosures are manufactured by stamp pressing stainless steel into a shape of the enclosure and then welding on metal features, such as interior brackets to support components within the enclosure. It can be difficult, however, to produce a lasting colored finish on stainless steel. Known processes, such as electrochemical or physical vapor deposition (PVD) techniques can be used to give stainless steel a colored finish. However, these colored finishes are usually susceptible to scratching and marring.
Aluminum is not only durable and corrosion resistant but it can also be anodized to provide a lasting finish having any of a number of colors. However, aluminum has different physical properties than stainless steel. For example, aluminum is generally not as stiff as stainless steel. Therefore, processes for producing stainless steel enclosures are not necessarily directly transferable to producing aluminum enclosures. For example, it can be difficult to weld features such as brackets onto enclosures made of aluminum.
This paper describes various embodiments that relate to manufacturing processes for producing aluminum consumer products. Methods for forming and treating cosmetically appealing aluminum enclosures are described.
According to one embodiment described herein, a method for forming an aluminum enclosure for an electronic device is described. The method includes performing a shaping operation on the aluminum enclosure. The method also includes comparing a current shape of the aluminum enclosure to a final shape of the aluminum enclosure. The method additionally includes performing a conditioning operation on the aluminum enclosure if, based on the comparison, the current shape is not the final shape. The method can further include repeating the shaping, comparing and conditioning operations until the current shape is the final shape. The method also includes performing a post-shaping operation on the aluminum enclosure.
According to another embodiment, an additional method for forming an aluminum enclosure for an electronic device is described. The method involves shaping the aluminum enclosure into a first shape having a back portion integrally formed with side walls. The back portion can have an interior surface and an exterior surface. The back portion and the side walls can create a cavity having a shape and size suitable for housing at least one internal component. The method also includes conditioning the aluminum enclosure such that at least a portion of the aluminum enclosure is softened to prevent cracking during a subsequent shaping process. The method additionally includes shaping the aluminum enclosure into a second shape having at least one integral feature integrally formed in the back portion and protruding a distance from the interior surface. The at least one integral feature can be configured to support at least one fastener used to fasten the at least one internal component within the cavity of the aluminum enclosure.
According to an additional embodiment, an aluminum enclosure for an electronic device is described. The aluminum enclosure includes an interior surface having a first group of nano-pores. The aluminum enclosure also includes at least one bracket secured to the interior surface and configured to support at least one component to the aluminum enclosure. The bracket includes an aluminum insert and a resinous member. The aluminum insert has an external surface having a second group of nano-pores. The resinous member has a first securing portion and a second securing portion. The first securing portion is molded within at least a portion of the interior surface having the first group of nano-pores. The second securing portion is molded within at least a portion of the external surface having the second group of nano-pores.
According to a further embodiment, a method of forming a bracket for an aluminum enclosure is described. The method includes creating a first group of nano-pores in an interior surface of an aluminum enclosure. The method also includes creating a second group of nano-pores in an exterior surface of an aluminum insert. The method additionally includes forming a supportive bracket on the interior surface of the aluminum enclosure. Forming the supportive bracket includes molding a first securing portion of a resinous member within at least a portion of the interior surface comprising the first group of nano-pores. Forming the supportive bracket also includes molding a second securing portion of the resinous member within at least a portion of the external surface comprising the second group of nano-pores.
The described embodiments and the advantages thereof may best be understood by reference to the following description taken in conjunction with the accompanying drawings. These drawings in no way limit any changes in form and detail that may be made to the described embodiments by one skilled in the art without departing from the spirit and scope of the described embodiments.
Representative applications of methods and apparatus according to the present application are described in this section. These examples are being provided solely to add context and aid in the understanding of the described embodiments. It will thus be apparent to one skilled in the art that the described embodiments may be practiced without some or all of these specific details. In other instances, well known process steps have not been described in detail in order to avoid unnecessarily obscuring the described embodiments. Other applications are possible, such that the following examples should not be taken as limiting.
In the following detailed description, references are made to the accompanying drawings, which form a part of the description and in which are shown, by way of illustration, specific embodiments in accordance with the described embodiments. Although these embodiments are described in sufficient detail to enable one skilled in the art to practice the described embodiments, it is understood that these examples are not limiting. That is, other embodiments may be used, and changes may be made without departing from the spirit and scope of the described embodiments.
Described herein are improved methods for forming aluminum enclosures or housings, such as enclosures for consumer products. As used herein, aluminum can refer to any suitable aluminum containing material, including pure aluminum and aluminum alloys. If an aluminum alloy is used, the type of alloy can be chosen, in part, on desired physical and cosmetic properties. In some embodiments, 5000 and 6000 series aluminum alloys are used. Methods described are well suited for manufacture of enclosures for electronic devices including computers, smart phones and media players, such as those designed and sold by Apple Inc. headquartered in Cupertino, Calif.
Often, the enclosures for electronic devices have internal features, such as brackets or supports, which can be used to secure one or more internal components to enclosure. The brackets and supports should be firmly attached to the enclosures in order to adequately secure the internal components to the enclosures. If an enclosure is made of stainless steel, typically the brackets and supports are welded onto internal surfaces of the enclosure. In some cases, the brackets and supports are fastened to the enclosure using fasteners such as screws. In some applications, it may be desirable to form enclosures out of aluminum since aluminum is lightweight and can be anodized to form a colored finish. However, processes for producing stainless steel enclosures may not be directly transferable to producing aluminum enclosures. For example, it can be difficult to weld metal features onto aluminum. In many cases, the strength of a weld onto aluminum is not sufficient to adequately bond the metal features onto the aluminum enclosure and to secure an internal component to the enclosure. In addition, the welding process can produce unsightly welding marks that are visible on the exterior portion of the enclosure.
Methods described herein can be used to provide aluminum enclosures having features that can be used to secure internal components to the enclosure. In some embodiments, the methods involve shaping integral features into an aluminum enclosure using forging or other shaping techniques. These embodiments are described below with reference to
After the shaping, at 104, the current shape of the aluminum enclosure is compared to a final shape. The final shape can include a general shape of an enclosure and can also include integral features integrally formed into the general enclosure shape. In some embodiments, the integral features include protruding and/or recessed portions in internal portions of the enclosure. The one or more brackets or supports can be configured to support at least one fastener to fasten at least one internal component to the enclosure. The integral features can be formed using any suitable method of shaping aluminum. In some embodiments, the integral features are forming using one or more forging processes. Any suitable forging process can be used. In one embodiment, a press forging process is used, wherein a die is placed onto portions of the enclosure and a compressive force is applied to form the features having desired shapes. In some embodiments, the die is heated to reduce the occurrence of the aluminum cracking and to promote surface flow and shaping.
In some embodiments, the final shape of the aluminum enclosure can require more than one shaping operation. For example, a first shaping operation can be performed to form an aluminum enclosure having a first shape. Then, a subsequent shaping operation can be performed to change the shape of the aluminum enclosure to a second shape. In some cases, the first shape can correspond to a general shape of the enclosure, including a back portion with side walls and the second shape can include the integral features formed into the general shape. In some embodiments, forming the first shape can include different types of shaping operations than forming the second and subsequent shapes. For example, the first shape can be formed using one or more of an extrusion, rolling, stamping, and bending process and the second shape can be formed using one or more of a forging and cutting process. More than one shaping processes may be necessary to form integral features into the housing. For example, the final shape can have protruding integral features that protrude a distance d from the interior surface. In some cases, more than one press forging process may be necessary to form integral features that protrude a distance d from the interior surface. Similarly, more than one press forging process may be necessary to form a desire amount of recess within the enclosure.
Returning to flowchart 100, if the final shape has been attained, a post-shaping treatment 108 can be performed. If the final shape has not been attained, the aluminum enclosure can undergo a conditioning process 106. The conditioning process conditions and prepares the aluminum enclosure for an additional shaping process 102. In this way, shaping 102 and conditioning 106 processes are repeated until a final shape of the aluminum enclosure is attained. The conditioning process can include a softening operation where the aluminum is made more compliant. In some embodiment the softening operation is an annealing process, which generally involves heating the aluminum to a temperature and for a time period sufficient to soften at least a portion of the aluminum. During the forming process of 102, the aluminum material is worked, which can cause adjoining crystals within the aluminum to slip against each other along slip planes. As the aluminum is worked, the resistance to movement along the slip planes can increase and the aluminum can become work hardened. Over working the aluminum can cause the aluminum to crack or break. By using a softening process such as annealing, the microstructure of the aluminum can be restored to a crystalline state, thereby altering the aluminum into a more resilient and workable state. In some cases, it can be beneficial to monitor the mechanical properties or temper rating of the aluminum prior to forging. In one embodiment, for example, it is found that forging an aluminum alloy having a T6 temper rating can cause breaking or cracking of the aluminum. Therefore, if the aluminum is found to have a T6 temper or higher, an annealing process can be used to soften the aluminum to a temper rating of T5 or less prior to a subsequent shaping process. The annealing can occur, for example, in an air furnace. The temperature and time can vary depending upon the type of aluminum or aluminum alloy used. In some embodiments, the aluminum is heated to a temperature of about 415 C+/−30 C for between about 30 minutes to 2 hours. In some cases the rate of cooling is controlled after the heating to achieve an optimal amount of softening.
After the aluminum is conditioned, at 102 an additional shaping procedure can be performed. Generally, it is advantageous to change the shape of the enclosure incrementally with conditioning operations 106 between each of the shaping operations. For example, incremental forging can be used to prevent the aluminum from becoming overworked and crack or break as described above. In addition, the incremental forging can reduce the occurrence of forging related defects that can be formed on the interior and/or exterior surfaces of the aluminum enclosure. The incremental forging can involve slightly modifying the shape of the one or more integral features with each forging until integral features having a final shape is formed. For example, the shapes of the integral features can become slightly more defined with each forging process until a final shape having integral features with well-defined edges and protrude or recess a final distance d from a surface of the enclosure.
Returning to flowchart 100, after a final shape of the enclosure is attained, the aluminum enclosure can undergo a post-shaping treatment 108.
After the impurities have been removed, at 204 the aluminum is hardened using an aging process or age hardening process. The aging process can involve heating the aluminum to reorder the microstructure of the aluminum and allow the aluminum to settle to a more hardened state. The process parameters of the aging process can be tuned to provide a microstructure having a small average grain size. In general, an aluminum microstructure having a small grain size can have high yield strength and also a visibly uniform surface. In one embodiment, the aluminum is hardened until a tensile and/or yield strength corresponding to aluminum alloy 6063-T6 temper is achieved. Aluminum alloy 6063-T6 temper typically has a tensile strength of about 30,000 psi (196 MPa) and a yield strength of about 25,000 psi (165 MPa). In some embodiments, the process parameters are tuned to provide an average grain size less than about 100 nm in diameter. This is because, in general, the smaller grain sizes are associated with a more visibly uniform appearance. In one embodiment, the process parameters were tuned to provide an average grain size between about 10 nm and 100 nm in diameter. Typically, the aging process involves heating and holding the aluminum to a prescribed temperature for a considerable period of time. In some embodiments, the aging process involves heating the aluminum to temperatures of between about 15° C. and 375 C for between about 8 to 12 hours.
At 206, the aluminum enclosure can undergo a surface finishing treatment.
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At 504, nano-pores are formed in one or more inserts. In some embodiments, the inserts are fastening features used to fasten one or more internal components to the aluminum enclosure. In one embodiment, the inserts are threaded metal pieces, such as threaded nuts, that can couple with corresponding threaded screws used to fasten the one or more internal components to the enclosure. In some embodiments the inserts are made of aluminum so that they are compatible with a subsequent anodizing procedure. This is because stainless steel and other metals can contaminate an aluminum anodizing bath. The nano-pores can be formed on at least exterior surfaces of the inserts to enhance the bonding of the metal inserts to the resinous material formed in subsequent process 506. In some embodiments, the nano-pores are formed by exposing at least the exterior surfaces of the inserts to an oxidative treatment. In one embodiment, the nano-pores are formed by exposing the exterior surfaces to an electrolytic bath comprising an oxidizing agent such as phosphoric acid or sodium hydroxide. In some embodiments, portions of the one or more inserts are masked or plugged to prevent exposure of these portions to the oxidative treatment. For example, threaded portions of nut inserts can be plugged to prevent exposure of the threads from exposure to the oxidative treatment. In this way, nano-pores can be prevented from forming on threaded portions of the inserts to maintain their structural integrity.
At 506, a plastic or resinous member is molded over at least a portion of the aluminum enclosure and over at least a portion of the one or more inserts. This can be done using an insert molding process where resinous material in liquid form is injected into a mold. After the liquid resinous material is allowed to harden, the hardened resinous material can retain a corresponding shape of the mold. In the present application, the liquid resinous material can be molded over surfaces that have been treated to have nano-pores, which includes surfaces of the aluminum enclosure and inserts. As the liquid resinous material is molded over the treated surfaces, the liquid resinous material can flow within the elongated voids of the nano-pores. Once the resinous material hardens, part of the hardened resinous material remains within the voids and can act as an anchor that enhances the bonding of the resinous material to aluminum enclosure and inserts. Note that since both the aluminum enclosure and the inserts have been pre-treated to form nano-pores, the resinous material is anchored to both. After the resinous material is molded over the aluminum enclosure and the one or more inserts, the one or more inserts can be used to fasten an internal component to the resinous member. For example, if the inserts are threaded nuts, corresponding screws can be used to fasten the internal components to the resinous member and the aluminum enclosure.
In some embodiments, aluminum enclosure assembly 700 undergoes a subsequent anodizing process to form an oxide layer on exposed surfaces of aluminum. During the anodizing process, aluminum enclosure assembly 700 can be immersed in an anodizing bath. As described above, stainless steel can contaminate and ruin an anodizing process. Therefore, in some embodiments, inserts 724 are made of a material that is compatible with an anodizing bath solution, such as aluminum. In alternative embodiments, inserts 724 can be masked prior to exposure to the anodizing bath to prevent contamination.
The various aspects, embodiments, implementations or features of the described embodiments can be used separately or in any combination. Various aspects of the described embodiments can be implemented by software, hardware or a combination of hardware and software. The described embodiments can also be embodied as computer readable code on a computer readable medium for controlling manufacturing operations or as computer readable code on a computer readable medium for controlling a manufacturing line. The computer readable medium is any data storage device that can store data which can thereafter be read by a computer system. Examples of the computer readable medium include read-only memory, random-access memory, CD-ROMs, HDDs, DVDs, magnetic tape, and optical data storage devices. The computer readable medium can also be distributed over network-coupled computer systems so that the computer readable code is stored and executed in a distributed fashion.
The foregoing description, for purposes of explanation, used specific nomenclature to provide a thorough understanding of the described embodiments. However, it will be apparent to one skilled in the art that the specific details are not required in order to practice the described embodiments. Thus, the foregoing descriptions of specific embodiments are presented for purposes of illustration and description. They are not intended to be exhaustive or to limit the described embodiments to the precise forms disclosed. It will be apparent to one of ordinary skill in the art that many modifications and variations are possible in view of the above teachings.