Patent Application
20160380126
Photovoltaic cells, commonly known as solar cells, are devices for direct conversion of solar radiation into electrical energy. Generally, solar cells are fabricated on a semiconductor wafer or substrate using semiconductor processing techniques to form a p-n junction near a surface of the substrate. Solar radiation impinging on the surface of, and entering into, the substrate creates electron and hole pairs in the bulk of the substrate. The electron and hole pairs migrate to p-doped and n-doped regions in the substrate, thereby generating a voltage differential between the doped regions. The doped regions are connected to conductive regions on the solar cell to direct an electrical current from the cell to an external circuit coupled thereto.
Efficiency is an important characteristic of a solar cell as it is directly related to the capability of the solar cell to generate power. Likewise, efficiency and/or cost in producing solar cells is directly related to the cost effectiveness of such solar cells. Accordingly, techniques for increasing the efficiency of solar cells, or techniques for increasing the efficiency in the manufacture of solar cells, are generally desirable. Some embodiments of the present disclosure allow for increased solar cell manufacture efficiency by providing novel processes for fabricating solar cell structures. Some embodiments of the present disclosure allow for increased solar cell efficiency by providing novel solar cell structures.
The following detailed description is merely illustrative in nature and is not intended to limit the embodiments of the subject matter of the application or uses of such embodiments. As used herein, the word “exemplary” means “serving as an example, instance, or illustration.” Any implementation described herein as exemplary is not necessarily to be construed as preferred or advantageous over other implementations. Furthermore, there is no intention to be bound by any expressed or implied theory presented in the preceding technical field, background, brief summary or the following detailed description.
This specification includes references to “one embodiment” or “an embodiment.” The appearances of the phrases “in one embodiment” or “in an embodiment” do not necessarily refer to the same embodiment. Particular features, structures, or characteristics may be combined in any suitable manner consistent with this disclosure.
Terminology. The following paragraphs provide definitions and/or context for terms found in this disclosure (including the appended claims):
“Comprising.” This term is open-ended. As used in the appended claims, this term does not foreclose additional structure or steps.
“Configured To.” Various units or components may be described or claimed as “configured to” perform a task or tasks. In such contexts, “configured to” is used to connote structure by indicating that the units/components include structure that performs those task or tasks during operation. As such, the unit/component can be said to be configured to perform the task even when the specified unit/component is not currently operational (e.g., is not on/active). Reciting that a unit/circuit/component is “configured to” perform one or more tasks is expressly intended not to invoke 35 U.S.C. §112, sixth paragraph, for that unit/component.
“First,” “Second,” etc. As used herein, these terms are used as labels for nouns that they precede, and do not imply any type of ordering (e.g., spatial, temporal, logical, etc.). For example, reference to a “first” barrier region does not necessarily imply that this barrier region is the first barrier region in a sequence; instead the term “first” is used to differentiate this barrier region from another barrier region (e.g., a “second” barrier region).
“Based On.” As used herein, this term is used to describe one or more factors that affect a determination. This term does not foreclose additional factors that may affect a determination. That is, a determination may be solely based on those factors or based, at least in part, on those factors. Consider the phrase “determine A based on B.” While B may be a factor that affects the determination of A, such a phrase does not foreclose the determination of A from also being based on C. In other instances, A may be determined based solely on B.
“Coupled”—The following description refers to elements or nodes or features being “coupled” together. As used herein, unless expressly stated otherwise, “coupled” means that one element/node/feature is directly or indirectly joined to (or directly or indirectly communicates with) another element/node/feature, and not necessarily mechanically.
“Inhibit”—As used herein, inhibit is used to describe a reducing or minimizing effect. When a component or feature is described as inhibiting an action, motion, or condition it may completely prevent the result or outcome or future state completely. Additionally, “inhibit” can also refer to a reduction or lessening of the outcome, performance, and/or effect which might otherwise occur. Accordingly, when a component, element, or feature is referred to as inhibiting a result or state, it need not completely prevent or eliminate the result or state.
In addition, certain terminology may also be used in the following description for the purpose of reference only, and thus are not intended to be limiting. For example, terms such as “upper”, “lower”, “above”, and “below” refer to directions in the drawings to which reference is made. Terms such as “front”, “back”, “rear”, “side”, “outboard”, and “inboard” describe the orientation and/or location of portions of the component within a consistent but arbitrary frame of reference which is made clear by reference to the text and the associated drawings describing the component under discussion. Such terminology may include the words specifically mentioned above, derivatives thereof, and words of similar import.
Approaches for the metallization of solar cells and the resulting solar cells are described herein. In the following description, numerous specific details are set forth, such as specific process flow operations, in order to provide a thorough understanding of embodiments of the present disclosure. It will be apparent to one skilled in the art that embodiments of the present disclosure may be practiced without these specific details. In other instances, well-known fabrication techniques, such as lithography and patterning techniques, are not described in detail in order to not unnecessarily obscure embodiments of the present disclosure. Furthermore, it is to be understood that the various embodiments shown in the figures are illustrative representations and are not necessarily drawn to scale.
The specification first describes example solar cells having a multi-layer barrier region configured to inhibit diffusion of metal to other metal and/or metal to silicon. An example method for fabricating a solar cell having a multi-layer barrier region is then described. Numerous examples are provided throughout the specification. Although many of the described examples are back-contact solar cells, the multi-layer barrier region can apply in other contexts, for example, for front-contact metallization for solar cells or for metal structures for semiconductor devices.
Referring to
Trenches 116 can be formed between n-type doped polysilicon regions 120 and p-type doped polysilicon regions 122. Portions of the trenches 116 can be texturized to have textured features. A dielectric layer 124 can be formed above the plurality of n-type doped polysilicon regions 120, the plurality of p-type doped polysilicon regions 122, and the portions of substrate 102 exposed by trenches 116. In one embodiment, a lower surface of the dielectric layer 124 is formed conformal with the plurality of n-type doped polysilicon regions 120, the plurality of p-type doped polysilicon regions 122, and the exposed portions of substrate 102, while an upper surface of dielectric layer 124 is substantially flat. In a specific embodiment, the dielectric layer 124 is an anti-reflective coating (ARC) layer.
In embodiments, a plurality of contact openings can be formed in the dielectric layer 124. The plurality of contact openings can provide exposure to the plurality of n-type doped polysilicon regions 120 and to the plurality of p-type doped polysilicon regions 122. In one embodiment, the plurality of contact openings is formed by laser ablation.
Furthermore, the plurality of n-type doped polysilicon regions 120 and the plurality of p-type doped polysilicon regions 122 can, in one embodiment, provide emitter regions for the solar cell 100. Thus, in an embodiment, the contact structures 128 are disposed on the emitter regions. In an embodiment, the contact structures 128 are back contacts for a back-contact solar cell and are situated on a surface of the solar cell opposing a light receiving surface (direction provided as 104 in
In an embodiment, substrate 102 is a bulk monocrystalline silicon substrate, such as an n-type doped monocrystalline silicon substrate. However, in an alternative embodiment, substrate 102 includes a polycrystalline silicon layer disposed on a global solar cell substrate. Moreover, in some embodiments, substrate 102 can be a multicrystalline silicon substrate.
In some embodiments, each of the contact structures 128 can include a seed stack disposed on the emitter regions of solar cell 100. The seed stack can include first conductive region 130, multi-layer barrier region 131 and 132 disposed on the first conductive region, and in some embodiments, second conductive region 133 disposed on the multi-layer barrier region. Although the multi-layer barrier region is illustrated as two layers, first and second barrier regions 131 and 132, in other examples, the multi-layer barrier region can include more than two layers.
Also as illustrated, contact structure 128 can include an additional conductive region 134 disposed on second conductive region 133. As one example, conductive region 134 can include plated metal, such as plated nickel, plated copper, and/or plated tin, among other examples. In some embodiments, as described herein, the seed stack may not itself include second conductive region 133 but instead, the additional conductive region (e.g., plated metal) may be disposed directly on the multi-layer barrier region, for example, as plated metal disposed directly on the multi-layer barrier region. In such an example, the additional metal disposed on the multi-layer barrier region may be referred to as a second conductive region.
In one embodiment, first conductive region 130 can be a metal-containing region. For example, first conductive region 130 can include aluminum (Al) and/or an aluminum/silicon (Al/Si) alloy. In one embodiment, the first conductive region is approximately 50-100 nanometers (nm) thick.
In various embodiments, the multi-layer barrier region can include first barrier region 131, closest to the substrate that is selective to inhibit diffusion from or to first conductive region 130 and/or from or to second barrier region 132. Similarly, second barrier region 132, farther from the substrate than first barrier region 131, can be selective to inhibit diffusion from or to second conductive region 133 and/or from or to first barrier region 132.
In some embodiments, a barrier layer containing TiW may make up two-thirds of the material cost of the seed stack and may also need a complex multi-step and expensive etching process to pattern the TiW and other metals of the seed stack. Additionally, in some instances, some barrier layers can flake more than others such that preventive maintenance for manufacturing equipment must be performed more frequently. Moreover, single layer barrier layers that are lower cost and easier to etch such as Mo or Ni may suffer from performance issues, as shown and described at
In one embodiment, one or more of the barrier regions can be diffusion-barrier conductive layers, and can include a refractory metal, such as tungsten (W) and/or molybdenum (Mo), and in some embodiments, can include a near-noble or transition metal (e.g., titanium (Ti)). In some embodiments, nickel or a nickel alloy can be used as a barrier region. In one particular example, first barrier region can include Mo (e.g., Mo, Mo—Ti alloy) and the second barrier region can include Ni (e.g., Ni-vanadium alloy, Ni-chromium alloy) and/or Ti.
In various embodiments, the collective multi-layer barrier region can be formed such that it has one or more of the following properties: low solubility of the first and second regions (e.g., Al and Cu) at a range of temperatures (e.g., up to an annealing temperature of approximately 400 degrees Celsius) and not be reactive with either of the first or second regions, have a grain structure that is not conducive to the transport of the metals of the conductive regions along grain boundaries, etch in a low-cost etch chemistry, and/or have good sputtering properties (e.g., electrically and thermally conductive, inhibits flaking).
In some embodiments, the thickness of the multi-layer barrier region can be approximately 60 nanometers (nm) or less but in some examples can be thicker than 60 nm, for example, 100 nm. In some examples, the thickness can be approximately 10 nm or less and still adequately inhibit diffusion. For example, in one embodiment, a first diffusion region of approximately 5 nm of Mo and a second diffusion region of approximately 5 nm of nickel-vanadium (NiV) can be used and the resulting solar cell structure can achieve state of the art efficiency and short circuit current, among other metrics of performance. Utilizing such a thin and lower cost barrier region can reduce material cost significantly and also speed throughput of the deposition and/or patterning processes by reducing the amount of time needed to deposit and/or etch the stack. Although the example above assumed an approximately equal thickness of the first and second barrier regions, in some embodiments, the thickness of the barrier regions can be different from one another. For example, in one embodiment, the thickness of a Mo barrier region can be approximately 5 nm and the thickness of the NiV barrier region can be approximately 10 nm. Other examples also exist.
Although the illustrated examples show a two-layer barrier stack, in other embodiments, the multi-layer barrier stack can include more than two layers. Each region/layer can have a distinct composition (e.g., Mo first barrier region, Ti second barrier region, NiV third barrier region) or one layer can repeat (e.g., Mo first barrier region, NiV second barrier region, Mo third barrier region).
In various embodiments, the described barrier regions in the multi-layer barrier stack can have high crystallization temperatures, which can allow them to be deposited in an amorphous or small-grained state, which can reduce the rate of grain boundary diffusion through the barriers.
In one embodiment, as was the case with first conductive region 130, second conductive region 133 can also be a metal-containing region. Second conductive region 133 can be copper, among other examples. In one embodiment, the second conductive region is approximately 50-200 nanometers (nm) thick.
In embodiments, the layers/regions of the seed stack can be formed on the semiconductor region by sputtering or other deposition technique. Various ones of the regions of the seed stack may include solvents, frit material, and/or binders to make the paste viscous enough and adhesive enough for deposition or other application to the semiconductor region.
In an embodiment, contact structure 128 can further include an additional conductive region, for example, approximately 35 microns of plated Cu.
In a second exemplary cell, a multi-layer barrier stack is used for a solar cell having emitter regions formed in a substrate of the solar cell. For example,
Referring to
Furthermore, the plurality of n-type doped diffusion regions 220 and the plurality of p-type doped diffusion regions 222 can, in one embodiment, provide emitter regions for the solar cell 200. Thus, in an embodiment, the contact structures 228 are disposed on the emitter regions. In an embodiment, the contact structures 228 are back contacts for a back-contact solar cell and are situated on a surface of the solar cell opposing a light receiving surface, such as opposing a texturized light receiving surface 205, as depicted in
Although certain materials are described specifically above with reference to
Furthermore, the formed contacts need not be formed directly on a bulk substrate, as was described in
Turning now to
As shown at 302, a first conductive region can be formed on a semiconductor region disposed in or above a substrate. An example of forming first conductive region 430 formed on the semiconductor region (not shown) disposed in or above substrate 402 is shown in
Turning back to
Similar to forming the first conductive region, the multi-layer barrier region can also be formed by deposition. In one embodiment, the layers of the multi-layer barrier region can be applied one layer at a time.
In various examples, and as described throughout the specification, the barrier region closest to the substrate can include Mo and the other barrier region can include one or more of Ti, Ni, V, W among other examples. The collective thickness of the multi-layer barrier region can be approximately 100 nm or less and in some instances, can be approximately 10 nm or less, 20 nm or less, or 60 nm or less, among other examples. By having a thinner barrier region, material cost of the actual metal layers and etchants can be dropped significantly as can processing time (e.g., etch time) by using a single etch process (e.g., a single bath of a dilute solution of ferric chloride, sulfuric acid, phosphoric acid, and peroxide) to etch all the seed stack layers rather than having a separate etchant and separate step for each layer.
Note that in some embodiments, more than two layers can be used in the multi-layer barrier region.
At 306, a second conductive region can be formed over the multi-layer barrier region. An example of the second conductive region being formed is shown in
In some embodiments, the seed stack itself may not have a second conductive region. Instead, in such embodiments, the second conductive region can be plated metal plated directly to the multi-layer barrier region. In one embodiment, plating of the second conductive region to the multi-layer barrier region can be performed after the annealing at block 308.
As shown at 308, the first conductive region, multi-layer barrier region, and second conductive region can be annealed. Annealing can be performed as a forming gas anneal at a temperature below approximately 450 degrees Celsius. Annealing can help improve electrical contact and remove contaminants, and/or sputtering damage.
In one embodiment, the multi-layer barrier region layers can remain substantially separate after annealing such that the layers do not substantially alloy together. Accordingly, layers of the multi-layer barrier region can therefore maintain their respective properties for inhibiting diffusion of certain materials. For example, after annealing, Mo can remain separate from NiV such that the Mo can still inhibit diffusion of Al to Ni and vice versa and NiV can remain separate from the Mo such that the NiV can still inhibit diffusion of Cu to Al or Si and vice versa.
Moreover, in some embodiments, in addition to inhibiting Al from reaching the Ni, the Mo containing layer can also inhibit the Ni from diffusing out of the Ni or Ni alloy layer into the Al. More generally, one of the barrier region layers can be selected such that it can inhibit diffusion out of the other barrier region layer and into either of the conductive layers.
As illustrated at 310, the annealed first conductive region, multi-layer barrier region, and second conductive region can be patterned. Patterning can include etching the first conductive region, multi-layer barrier region, and second conductive region with a single etchant, for example, an etchant that includes a dilute solution of ferric chloride, sulfuric acid, phosphoric acid, and peroxide.
In one embodiment, before patterning the seed stack at 310, a patterned mask, as shown as mask 802 in
Although specific embodiments have been described above, these embodiments are not intended to limit the scope of the present disclosure, even where only a single embodiment is described with respect to a particular feature. Examples of features provided in the disclosure are intended to be illustrative rather than restrictive unless stated otherwise. The above description is intended to cover such alternatives, modifications, and equivalents as would be apparent to a person skilled in the art having the benefit of this disclosure.
The scope of the present disclosure includes any feature or combination of features disclosed herein (either explicitly or implicitly), or any generalization thereof, whether or not it mitigates any or all of the problems addressed herein. Accordingly, new claims may be formulated during prosecution of this application (or an application claiming priority thereto) to any such combination of features. In particular, with reference to the appended claims, features from dependent claims may be combined with those of the independent claims and features from respective independent claims may be combined in any appropriate manner and not merely in the specific combinations enumerated in the appended claims.
