Application of Arthur P. Shepard

319 F.2d 194, 50 C.C.P.A. 1439
CourtCourt of Customs and Patent Appeals
DecidedJune 20, 1963
DocketPatent Appeal 6984
StatusPublished
Cited by10 cases

This text of 319 F.2d 194 (Application of Arthur P. Shepard) is published on Counsel Stack Legal Research, covering Court of Customs and Patent Appeals primary law. Counsel Stack provides free access to over 12 million legal documents including statutes, case law, regulations, and constitutions.

Bluebook
Application of Arthur P. Shepard, 319 F.2d 194, 50 C.C.P.A. 1439 (ccpa 1963).

Opinion

ALMOND, Judge.

This is an appeal from the Board of Appeals affirming the examiner’s refusal to allow claims 28 through 39 in appellant’s patent application. 1 No other claims remain in the application.

The application discloses a specified spraywelding material and its use in a spraywelding process. Claims 28 through 35 are drawn to a spraywelding powder mixture. Claims 36 through 39 are drawn to a spraywelding process.

Appellant’s disclosed invention relates to a process called spraywelding. The background of this process and the problem arising therefrom is stated in appellant’s brief as follows:

“ * * * The spraywelding process involves the flame spraying of a powder onto a surface, such as a metal surface, followed by the melting or fusing of the sprayed material in place by heating in order to form a coating. The spraying operation serves the purpose of positioning the powder particles on the surface but a satisfactory coating is not achieved until after the fusing operation. The fusing operation, which is normally effected with the use of a torch, causes the bonding of the sprayed particles to the surface and causes these particles to melt together in the form of a homogeneous material, forming a coating layer.
“The sprayweld process constitutes a commercially used and practiced process, and did so at the time that the applicant’s application was filed. As is well recognized, the spraywelding had to be effected with specific powder materials which are generally designated in the art and sold as spraywelding powders or alloys. These known spraywelding powders have a base alloy, such as a nickel base alloy, and' contain a fluxing element which is generally boron. When the conventional spraywelding alloys were utilized in the spraywelding process, after the spraying operation the operator would heat the surface with the torch until the powder was completely fused, as could be determined by a glassy, shiny appearance.
“A problem existed, however, that the coating would become highly fluid and have a tendency to run and drip during the fusing operation. This tendency would prevent the build-up of substantial layer thicknesses, and due to the fluidity and-surface tension, the coating would pull away from the edges, sharp corners or the like, rendering the finished product unsatisfactory.”

Appellant provided a solution to the problem of running and dripping during fusing by adding a material to alter the viscosity of the sprayed layer during fusing. The material added to the coating was a second nickel base alloy having a “coalescence” temperature at least 10° F. higher than that of the self-fluxing nickel base alloy powder used in the art. The second alloy

“ * * * must be of such a nature that its particles will fuse or melt together at a temperature of at least 10° F. higher than the temperature which will cause the self-fluxing sprayweld alloy to so fuse or melt together, and must be able to form a uniform alloy with the sprayweld, self-fluxing alloy within the temperature range at which the mixture will fuse together but below the temperature at which the coating will start to run and drip.”

Claims 28 and 36 are representative of the material claims and the process claims, respectively, and read as follows:

“28. In a spraywelding material comprising a self-fluxing nickel base-alloy powder, the improvement for *196 reducing the tendency of the material to run and drip during a fusing operation which comprises at least one other nickel base alloy powder, said other nickel base allow powder being substantially completely alloy-able with said self-fluxing nickel base alloy powder below the upper limit of the fusion range of said mixture, there being a temperature differential of at least 10° F. between the temperature of coalescence of the mixture component having the highest and the component having the lowest temperature of coalescence between particles of the same component, the powder mixture having a particle size below about 100 mesh with not more than about 30% below 325 mesh.
“36. In the spray-weld process in which a self-fluxing nickel base alloy powder is sprayed onto a metal base and thereafter fused in place, the improvement for reducing the tendency of the material to run and drip during the fusing operation which comprises effecting said spraying with a mixture of a self-fluxing nickel base alloy powder with at least one other nickel base alloy powder substantially completely alloyable with the self-fluxing powder below the upper limit of the fusion range of said mixture there being a temperature differential of at least 10° F. between the temperature of coalescence of the mixture component having the highest and the component having the lowest temperature of coalescence between the particles of the same component, the powder mixture having a particle size below about 100 mesh with more than 30% below about 325 mesh, and thereafter fusing the sprayed coating to form a substantially homogeneous alloy on the base.”

The sole reference relied on is:

Turner et al. 2,763,921 September 25, 1953

Turner et al. discloses materials for and a method of coating molybdenum jet engine parts to make them corrosion and impact resistant. A mixture of two nickel-chromium alloys, having differing melting points, with particle size on the order of minus 325 mesh, is sprayed on the surface of the refractory article to be coated to protect it from oxidation. (Molybdenum melts at over 4500° F., but it may begin to oxidize at 900° F.) The coated article is heated to a temperature high enough to just melt the lower melting alloy but insufficient to melt the high melting alloy. The higher melting particles then begin to dissolve in the liquid phase, the extent of solution being dependent upon the time of treatment. The patentees state that “the best coatings under these conditions are obtained by interrupting the firing cycle before the point of complete solution of the higher melting alloy in the lower melting alloy matrix is reached,” and that “The resulting coating is then uniform, tight, and integrally bonded to the base metal.” Turner et al. also states: “For best results, the coating should be applied so that the final thickness of the coating is within the range from 0.0002 inch to 0.0010 inch in thickness, with 0.0030 to 0.0040 inch thickness being an optimum range.”

The reference further indicates that the method employed therein permits one “to apply thin coatings without the danger of discontinuities,” and that the coatings produced are “extremely uniform.”

The issues to be resolved, as aptly summarized by appellant, are whether Turner et al. forms a single homogeneous alloy, and whether the record shows that the appellant’s claimed particle sizes are critical so as to patentably distinguish from the disclosure of the reference. Both of these issues are present in the' process claims, but the claims drawn to a material concern only the powder and not the resultant fused alloy.

With respect to the process of forming a homogeneous coating, the examiner rejected the claims in issue as unpatentable over Turner et al., finding that the patentee “reduced to practice coatings in which

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319 F.2d 194, 50 C.C.P.A. 1439, Counsel Stack Legal Research, https://law.counselstack.com/opinion/application-of-arthur-p-shepard-ccpa-1963.