Patent Application
20190360097
The present disclosure is related generally to an apparatus and method for coating specimens.
Ceramic matrix composites have been identified as candidate materials for components in the hot-section of jet engines due to their high temperature capability, low weight, and low coefficient of thermal expansion. In some instances these components are manufactured by laying up stacked 2D cloth or using 3D laminates to form a fiber preform, depositing a fiber-matrix interphase coating and rigidizing the fiber preform through chemical vapor infiltration (CVI), infiltrating the rigidized preform with a ceramic slurry to form an impregnated preform, and melt infiltrating the impregnated preform with molten silicon to render the composite nearly fully dense.
When performing CVI in a conventional “batch style” reactor 100, such as that shown in
An apparatus for coating specimens includes a reaction chamber and a plurality of reaction modules in the reaction chamber for containing specimens to be coated, where each reaction module includes a module inlet and a module outlet. A plurality of conduits are configured to be in fluid communication with at least one gas source external to the reaction chamber, and each of the conduits terminates in one of the reaction modules for delivery of gaseous reagents to the specimens to be coated. The module outlets are in fluid communication with the reaction chamber for expulsion of gaseous reaction products from the reaction modules.
A method of coating specimens includes heating a reaction chamber containing a plurality of reaction modules and a plurality of specimens to be coated, where each of the reaction modules includes a module inlet and a module outlet and contains at least one of the specimens. Gaseous reagents are flowed through the module inlets and into the reaction modules where they chemically react to form coatings on the specimens. A pressure in each of the reaction modules is higher than a pressure in the reaction chamber, and thus gaseous reaction products are expelled from the reaction modules through the module outlets and may be removed from the reaction chamber through one or more outlet ports during operation.
A new apparatus for chemical vapor infiltration (CVI) of porous specimens, such as ceramic fiber preforms, has been developed. The apparatus may also be used to coat specimens using chemical vapor deposition (CVD). The apparatus is designed to reduce or eliminate downstream contamination from reaction product gases, thereby allowing coatings to be uniformly deposited on a number of specimens throughout the apparatus. A coating method that may be carried out in the apparatus is also described below. Components referred to as being “in fluid communication with” each other in the description that follows are directly or indirectly connected or otherwise related in such a way that fluid (e.g., a gas) can flow between the components in one or both directions.
Referring to
As illustrated in
The module outlets 208 are in fluid communication with the reaction chamber 202 and configured to direct gaseous reaction products out of the reaction modules 204, e.g., toward an inner wall of the reaction chamber 202 and/or in a direction transverse to a longitudinal axis of the reaction chamber 202. Each reaction module 204 includes one or more module outlets 208. Exemplary flow paths of the gaseous reaction products are represented by unshaded arrows in
The apparatus 200 may further comprise a lid 218 secured to an end of the reaction chamber 202. The one or more inlet ports 210 may be disposed in the lid 218, which may be removed from the reaction chamber 202 as needed. The conduits 212 may also be removed and reinserted as needed. For example, after use of the apparatus 200, the lid 218 and/or conduits 212 may be readily removed to allow access to the reaction chamber 202 for cleaning and/or specimen removal. The reaction modules 204 may also be individually removable from the reaction chamber 202 to facilitate easy specimen insertion and removal. The reaction chamber 202 may be sealed during operation to maintain a controlled environment therein.
As shown in
The inlet port 210 and the module inlets 206 may be aligned with the longitudinal axis of the reaction chamber 202, as shown for the exemplary apparatus 200 of
Typically, the reaction chamber 202, the reaction modules 204 and/or other components of the apparatus 200 are made of a refractory material such as graphite or a carbon composite that can withstand temperatures in excess of 2000° C. and has good thermal properties and chemical resistance.
In addition to the apparatus described above, an improved method of coating specimens using CVI or CVD has been developed. The method is described in reference to
The method includes heating a reaction chamber 202 containing a plurality of specimens (e.g., porous specimens) 230. The reaction chamber 202 comprises a plurality of reaction modules 204, where each reaction module 204 includes a module inlet 206 and a module outlet 208 and contains at least one of the porous specimens 230. In a CVI process, gaseous reagents are flowed through the module inlets 206 and into the reaction modules 204, where they infiltrate the porous specimens 230 and chemically react to form coatings on the porous specimens 230. In a CVD process, gaseous reagents that flow through the module inlets 206 and into the reaction modules 204 chemically react to form coatings on the specimens without necessarily infiltrating the specimens, which may not be porous. In CVI or CVD, the pressure in each of the reaction modules 204 is higher than the pressure in the reaction chamber 202 to ensure that gaseous reaction products are expelled from the reaction modules 204 through the module outlets 208. The gaseous reaction products may then be removed from the reaction chamber 202 through one or more outlet ports 214. As a consequence, the reaction products from each reaction module 204 are substantially prevented from contaminating CVI or CVD reactions occurring in adjacent reaction modules 204.
The gaseous reagents may be flowed into the reaction modules through a plurality of conduits 212 in fluid communication with one or more gas sources outside the chamber 202, where each conduit 212 terminates in one of the reaction modules 204. Each conduit 212 may pass through or be connected to one or more inlet ports 210 in the reaction chamber 202, as described above. Each conduit 212 may pass through at least one of the module inlets 206. As shown in
The outlet port(s) 214 of the reaction chamber 202 may be in fluid communication with a vacuum pump. Also or alternatively, the flow rate of the gaseous reagents into the reaction modules 204 may be controlled. Thus, a suitable pressure differential between the reaction chamber 202 and the reaction modules 204 may be achieved along with forced flow of the gaseous reagents through the reaction modules 204. The pressure in each of the reaction modules 204 may be in a range from about one to about five orders of magnitude higher than that in the reaction chamber 202. In other words, the pressure may be from about 10 times to about 100,000 times higher in the reaction modules 204 than in the reaction chamber 202. For example, the pressure in each of the reaction modules 204 may be in a range from about 1 Torr to about 50 Torr, and the pressure in the reaction chamber 202 may be in a range from about 1 mTorr to about 50 mTorr. Typically, the method is carried out with each of the reaction chamber 202 and the reaction modules 204 at a pressure below atmospheric pressure (760 Torr). Thus, prior to introducing the gaseous reagents into the reaction modules 204, the reaction chamber 202 and the reaction modules 204 may be evacuated to a desired vacuum level (i.e., to a desired a sub-atmospheric pressure level) using one or more vacuum pumps.
Typically, the reaction chamber 202 is heated to an elevated temperature in a range from about 700° C. to about 1800° C. The heating may comprise inductive heating, radiative heating, microwave heating, or another heating method capable of increasing the temperature of the reaction chamber 202 to the desired elevated temperature. The reaction chamber 202 is maintained at the elevated temperature during the CVI or CVD process, which may be carried out for a period of 15 minutes to 100 hours.
The gaseous reagents employed in the process may include a reaction precursor and a carrier gas and may depend on the coating to be formed. In one example involving porous specimens, the specimens to be coated may be fiber preforms comprising silicon carbide (SiC) and the coating may be a fiber interphase coating comprising carbon or boron nitride. In another example involving porous specimens, the specimens to be coated may be SiC fiber preforms and the coating may be a matrix (or rigidization) coating comprising SiC. If desired, both a fiber interphase coating and a matrix coating may be applied to the fiber preform in separate but sequential CVI processes, which may be carried out as described above and/or in the apparatus described above. The fiber preforms that undergo coating may be fabricated using fiber arrangement and lay-up processes known in the art.
If a matrix coating comprising SiC is to be formed by CVI on a SiC fiber preform, the gaseous reagents may include methyltrichlorosilane (CH3SiCl3; reaction precursor) and hydrogen gas (H2; carrier gas). During the chemical reaction, methyltrichlorosilane may decompose to form solid SiC and gaseous hydrochloric acid (HCl), the former of which is deposited on the fiber preform as the coating while the latter is removed from the reaction modules by entrainment in the carrier gas. Other gaseous reagents (including reaction precursors and carrier gases) suitable for forming matrix coatings and fiber interphase coatings are known in the art and may be employed in the above-described method and apparatus.
As would be apparent to the skilled artisan, the method described here may be carried out in the apparatus described above, including any of the components, configurations, and/or capabilities shown in
As would also be recognized by the skilled artisan, the above-described apparatus and method may be used to coat specimens using CVI or CVD. Porous specimens are typically coated by CVI, whereas the specimens coated by CVD need not be porous. The apparatus employed for CVD may be similar or identical to the apparatus employed for CVI. Other aspects of the method and apparatus described for CVI may apply also to CVD.
To clarify the use of and to hereby provide notice to the public, the phrases “at least one of <A>, <B>, . . . and <N>” or “at least one of <A>, <B>, . . . <N>, or combinations thereof” or “<A>, <B>, . . . and/or <N>” are defined by the Applicant in the broadest sense, superseding any other implied definitions hereinbefore or hereinafter unless expressly asserted by the Applicant to the contrary, to mean one or more elements selected from the group comprising A, B, . . . and N. In other words, the phrases mean any combination of one or more of the elements A, B, . . . or N including any one element alone or the one element in combination with one or more of the other elements which may also include, in combination, additional elements not listed.
Although considerable detail with reference to certain embodiments has been described, other embodiments are possible. The spirit and scope of the appended claims should not be limited, therefore, to the description of the preferred embodiments contained herein. All embodiments that come within the meaning of the claims, either literally or by equivalence, are intended to be embraced therein.
Furthermore, the advantages described above are not necessarily the only advantages, and it is not necessarily expected that all of the described advantages will be achieved with every embodiment.
