The present invention relates most generally to the prevention of delamination of deposited films such as used in semiconductor manufacturing and solar cells.
Film delamination due to subsequent thermal processing is a problem that plagues the semiconductor manufacturing industry and other applications in which film deposition is utilized. Commonly, the problem is due to a poor adhesion force between the deposited film and the material upon which the film is deposited. This problem can occur when the film is the same as the material upon which it is being deposited or different than the subjacent material. The poor adhesion between the film and the material upon which it is deposited, causes delamination such as peeling, cracking and/or blistering of the film during subsequent thermal processing such that takes place at an elevated temperature in the vicinity of 300° C. or greater. For example, this phenomena is experienced when a stack of amorphous silicon films are formed. Amorphous silicon (a-Si) films may be hydrogenated to passivate dangling bonds and the hydrogenated amorphous silicon is designated a-Si:H. The aforementioned adhesion force is particularly weak at the a-Si:H/a-Si:H interface formed between two films. The upper a-Si layer will delaminate after a subsequent thermal cycle due to residual stress (compressive) formed at the interface due to the deposition characteristics and conditions of the upper a-Si:H film and also due to hydrogen diffusion at the interface. This problem is particularly egregious when the film is relatively thick, such as 1 micron or greater. The problematic subsequent thermal cycling is difficult to avoid since semiconductor devices typically undergo a number of thermal cycling processes during their manufacture. For example, the formation of a passivating film such as silicon nitride typically takes place at an elevated temperature and for a sufficient time to effectuate delamination.
Although described in conjunction with an a-Si film, the delamination problem occurs in various films used in semiconductor device and solar cell fabrication.
There have been various approaches that address this delamination problem. These efforts include fine-tuning the film deposition conditions to minimize the compressive stress of the deposited film, instituting various cleaning procedures prior to the film deposition process, de-gassing prior to the film deposition process, instituting a sticking layer prior to the film deposition process, and roughening the surface upon which the film will be deposited. The effectiveness of these conventional procedures is limited and many of the aforementioned procedures for addressing the problem, are unsuitable for various manufacturing environments.
Even when only partial delamination occurs, contamination from the cracking, peeling, blistering delaminated film degrades the quality of the entire semiconductor device, even in areas where the film does not delaminate. It would therefore be advantageous to provide a process and structure for preventing film delamination during subsequent thermal processing operations.
To address these and other needs, and in view of its purposes, the present invention provides a method for preventing delamination of a deposited film. The method includes providing a substructure with a first material thereon, depositing a thick film having a thickness of at least 1 micron, on the first material, then partitioning the thick film into a plurality of discrete portions prior to a subsequent thermal treatment, wherein the thick film does not delaminate during the subsequent thermal treatment.
The film may be uniformly partitioned into discrete portions that are regularly arranged and spaced, include a pattern density of at least 80% and are not individually functioning elements of a semiconductor device.
According to another aspect to the invention, provided is a solar cell formed on a substrate and including a film stack thereon. The film stack includes a subjacent amorphous silicon material and a superjacent amorphous silicon film disposed directly on the subjacent amorphous silicon material. The superjacent amorphous silicon film includes a thickness of at least 1.5 microns and is patterned into a plurality of discrete portions. The portions are regularly arranged and spaced and include a pattern density of at least 90 percent. The discrete portions are not separately functioning elements of the solar cell.
The present invention is best understood from the following detailed description when read in conjunction with the accompanying drawing. It is emphasized that, according to common practice, the various features of the drawing are not necessarily to scale. On the contrary, the dimensions of the various features are arbitrarily expanded or reduced for clarity. Like numerals denote like features throughout the specification and drawing.
The present invention provides a method and structure for preventing delamination of films during subsequent thermal cycling. The invention finds application in various films that are prone to delamination such as thick films, i.e., film having a thickness greater than 1 micron. In one embodiment, the thick films may be used as sacrificial layers in semiconductor devices such as MEMS (microelectromechanical structure). In other exemplary embodiments, the films may be used in other applications in other semiconductor devices. In one particular exemplary embodiment, the films may be used in solar cells devices formed on semiconductor substrates.
After film 7 is formed, it is partitioned into a plurality of discrete portions such as shown in
For the illustrated embodiment in which discrete sections 15 are rectangles, the orthogonal sides 19 and 20 of each rectangle, may each include a length ranging from about 10 to about 100 microns. The area of each discrete portion 15 may be about 100 to 10000 μm2, but other areas may be used in other exemplary embodiments.
After film 7 is partitioned such as shown in
According to one exemplary embodiment such as shown in
The preceding merely illustrates the principles of the invention. It will thus be appreciated that those skilled in the art will be able to devise various arrangements which, although not explicitly described or shown herein, embody the principles of the invention and are included within its spirit and scope. Furthermore, all examples and conditional language recited herein are principally intended expressly to be only for pedagogical purposes and to aid the reader in understanding the principles of the invention and the concepts contributed by the inventors to furthering the art, and are to be construed as being without limitation to such specifically recited examples and conditions. Moreover, all statements herein reciting principles, aspects, and embodiments of the invention, as well as specific examples thereof, are intended to encompass both structural and functional equivalents thereof. Additionally, it is intended that such equivalents include both currently known equivalents and equivalents developed in the future, i.e., any elements developed that perform the same function, regardless of structure.
This description of the exemplary embodiments is intended to be read in connection with the figures of the accompanying drawing, which are to be considered part of the entire written description. In the description, relative terms such as “lower,” “upper,” “horizontal,” “vertical,” “above,” “below,” “up,” “down,” “top” and “bottom” as well as derivatives thereof (e.g., “horizontally,” “downwardly,” “upwardly,” etc.) should be construed to refer to the orientation as then described or as shown in the drawing under discussion. These relative terms are for convenience of description.
Although the invention has been described in terms of exemplary embodiments, it is not limited thereto. Rather, the appended claims should be construed broadly, to include other variants and embodiments of the invention, which may be made by those skilled in the art without departing from the scope and range of equivalents of the invention.
Number | Name | Date | Kind |
---|---|---|---|
4741964 | Haller | May 1988 | A |
4776896 | Umemoto | Oct 1988 | A |
5449640 | Hunt et al. | Sep 1995 | A |
5656547 | Richards et al. | Aug 1997 | A |
5681616 | Gupta et al. | Oct 1997 | A |
6194249 | Chen et al. | Feb 2001 | B1 |
6534396 | Fahn et al. | Mar 2003 | B1 |
6586347 | Liu et al. | Jul 2003 | B1 |
7696101 | Li | Apr 2010 | B2 |
20010006846 | Cao et al. | Jul 2001 | A1 |
20010038367 | Inukai | Nov 2001 | A1 |
20020011598 | Yamazaki et al. | Jan 2002 | A1 |
20020016073 | Kondo et al. | Feb 2002 | A1 |
20030006468 | Ma et al. | Jan 2003 | A1 |
20030040195 | Chang et al. | Feb 2003 | A1 |
20030124462 | Miller | Jul 2003 | A1 |
20030151020 | Lee et al. | Aug 2003 | A1 |
20040067616 | Hachisuka et al. | Apr 2004 | A1 |
20050023145 | Cohen et al. | Feb 2005 | A1 |
20050029109 | Zhang et al. | Feb 2005 | A1 |
20050029660 | Ruttkowski et al. | Feb 2005 | A1 |
20050253268 | Hsu et al. | Nov 2005 | A1 |
Number | Date | Country |
---|---|---|
62062050 | Mar 1987 | JP |
2058322 | Feb 1990 | JP |
Entry |
---|
Cerofolini et al “Hydrogen related complexes as the stressing species in high fluence hydrogen implanted single crystal silicon” Jul. 15, 1992 Physical Rev. B vol. 46 No. 4. |
Hong et al. “Growth of H:Amorpous Si on patterned substrates for increased mechanical stability” 1994 MRS Fall Meeting. |
Number | Date | Country | |
---|---|---|---|
20070197005 A1 | Aug 2007 | US |