Ex Parte Grylls et alDownload PDFBoard of Patent Appeals and InterferencesApr 23, 201011214292 (B.P.A.I. Apr. 23, 2010) Copy Citation UNITED STATES PATENT AND TRADEMARK OFFICE ____________________ BEFORE THE BOARD OF PATENT APPEALS AND INTERFERENCES ____________________ Ex parte RICHARD JOHN GRYLLS and THEODORE ROBERT GROSSMAN ____________________ Appeal 2009-013895 Application 11/214,292 Technology Center 1700 ____________________ Decided: April 23, 2010 ____________________ Before CATHERINE Q. TIMM, JEFFREY T. SMITH, and JEFFREY B. ROBERTSON, Administrative Patent Judges. TIMM, Administrative Patent Judge. DECISION ON APPEAL I. STATEMENT OF CASE Appellants appeal under 35 U.S.C. § 134 from the Examiner’s decision to reject claims 14 and 18-35 under 35 U.S.C. § 102(b) as anticipated by, or under 35 U.S.C. § 103(a) as unpatentable over, Rigney (US 6,153,313, issued November 28, 2000). We have jurisdiction under 35 U.S.C. § 6(b). Appeal 2009-013895 Application 11/214,292 2 We AFFIRM. Appellants’ invention relates to an airfoil of a turbine engine having a predominately β phase NiAl alloy composite coating achieved by an electroplating technique (Spec. ¶ [0001] and [0025]). Claim 14 is illustrative: 14. An article for use in a gas turbine substrate comprising: a superalloy substrate, wherein the superalloy is selected from the group of nickel base superalloys, cobalt base superalloys, iron base superalloys and combinations thereof; and a coating applied over the substrate, the coating being formed by a method comprising: plating a nickel matrix and embedded powders, the powders selected from the group consisting of Ni, Cr, Al, Zr, Hf, Ti, Ta, Si, Ca, Fe, Y, Ga, and combinations thereof, such that upon deposition, the powders form a second phase dispersed in the substantially nickel matrix which forms a first phase; and depositing aluminum by an aluminiding process over the nickel matrix and embedded powders, the aluminum deposited in sufficient amount to provide a NiAl stoichiometry to the nickel matrix and embedded powders to form a substantially β phase NiAl coating having additional alloying elements. II. DISPOSITIVE ISSUE Appellants first present arguments with respect to independent claims 14, 26, and 31 as a group (Br. 10), for which we select claim 14 to represent the group. Appeal 2009-013895 Application 11/214,292 3 Appellants contend that, because Rigney teaches a plasma vapor deposition process (PVD), Rigney does not teach the process steps of plating a nickel matrix and embedded powders and depositing aluminum by an aluminiding process for obtaining the NiAl coating (Br. 10-11). Appellants also assert that the use of heat for homogenization taught by Rigney is not needed when a coating is applied using the claimed process steps and that Appellants’ invention need not obtain a homogenized composition because only a “substantially β-phase NiAl coating” is claimed (Br. 11). Appellants also assert that the PVD process taught by Rigney “does not allow for coating of complex articles, such as airfoils” (Br. 11). The issue raised by the contentions of Appellants and the Examiner is: has the Examiner erred in finding that Rigney anticipates the claimed β- phase NiAl coated article, specifically turning on the fact that Rigney does not teach the claimed “plating” and “depositing aluminum by an aluminiding process” steps recited in claim 14? III. FINDINGS OF FACT The Examiner has made several unrebutted findings in support of his ultimate finding that the claimed coated article would be identical to or substantially identical to Rigney’s coated article in terms of structures and compositions (Ans. 4), including: 1. Rigney teaches a layer predominately comprised of β-NiAl and Appellants claim a layer formed substantially of β-NiAl, each including alloying elements (Ans. 5; see Rigney, col. 5, ll. 19-21); 2. The range represented by the term “substantially beta phase NiAl” as claimed is considered to overlap the range represented by the Appeal 2009-013895 Application 11/214,292 4 description of Rigney et al. of a coating formed 'predominantly' in the beta- NiAl phase (Ans. 7); 3. Both the claimed process and Rigney process result in a layer with a 1:1 ratio of Ni to Al, whether by use of heat or without, to form a homogeneous composition (Ans. 7); 4. The plasma vapor deposition taught by Rigney is a common method for coating articles such as an airfoil (Ans. 8); and 5. Rigney teaches applying the coating to turbine blades, which include an airfoil (Ans. 8; see Rigney, col. 4, ll. 40-62). IV. PRINCIPLES OF LAW It has long been held that “[i]f the product in a product-by-process claim is the same as or obvious from a product of the prior art, the claim is unpatentable even though the prior product was made by a different process.” In re Thorpe, 777 F.2d 695, 697 (Fed. Cir. 1985); In re Brown, 459 F.2d 531, 535 (CCPA 1972) (“[I]t is the patentability of the product claimed and not of the recited process steps which must be established.”); In re Wertheim, 541 F.2d 257, 271 (CCPA 1976) (“the patentability of the products defined by the claims, rather than the processes for making them, is what we must gauge in light of the prior art.”). “Where a product-by-process claim is rejected over a prior art product that appears to be identical, although produced by a different process, the burden is upon the applicants to come forward with evidence establishing an unobvious difference between the claimed product and the prior art product.” In re Marosi, 710 F.2d 799, 803 (Fed. Cir. 1983). Appeal 2009-013895 Application 11/214,292 5 V. ANALYSIS We sustain this rejection for the reasons cogently presented by the Examiner in the answer. Specifically, claim 14 is a product-by-process claim for which we look to the product claimed, not the process steps, for patentability. The Examiner has provided reasonable and unrebutted evidence to support a finding that the claimed coated article and the coated article taught by Rigney are identical or substantially identical, despite being formed by different processes. Appellants have provided no evidence establishing a structural or compositional difference between the two coatings. We agree with the Examiner that, without evidence to the contrary, “an end-product beta-NiAl layer including alloying elements is considered to be just that no matter what method is used in its formation” (Ans. 5-6). See In re Papesch, 315 F.2d 381, 391 (CCPA 1963) (“[A] compound and all of its properties are inseparable; they are one and the same thing.”). Appellants present no other arguments with respect to any of the dependent claims in addition to those discussed above (Br. 11). VI. CONCLUSION On the record before us1 and for the reasons discussed above, we sustain the rejection maintained by the Examiner. VII. DECISION We affirm the decision of the Examiner. 1Only those arguments actually made by Appellants have been considered in this decision. Arguments which Appellants could have made but chose not to make have not been considered and are deemed to be waived. See 37 C.F.R. § 41.37(c)(1)(vii) (2008). Appeal 2009-013895 Application 11/214,292 6 VIII. TIME PERIOD FOR RESPONSE No time period for taking any subsequent action in connection with this appeal may be extended under 37 C.F.R. § 1.136(a). AFFIRMED cam MCNEES WALLACE & NURICK LLC 100 PINE STREET P.O. BOX 1166 HARRISBURG, PA 17108-1166 Copy with citationCopy as parenthetical citation