Ex Parte Anderson et alDownload PDFPatent Trial and Appeal BoardDec 4, 201411714750 (P.T.A.B. Dec. 4, 2014) Copy Citation UNITED STATES PATENT AND TRADEMARK OFFICE ____________________ BEFORE THE PATENT TRIAL AND APPEAL BOARD ____________________ Ex parte DEREK W. ANDERSON and RONALD N. ZAPPONE ____________________ Appeal 2012-011212 Application 11/714,750 Technology Center 3700 ____________________ Before: JOHN C. KERINS, CHARLES N. GREENHUT, and MICHELLE R. OSINSKI, Administrative Patent Judges. OSINSKI, Administrative Patent Judge. DECISION ON APPEAL STATEMENT OF THE CASE Derek W. Anderson and Ronald N. Zappone (Appellants) appeal under 35 U.S.C. § 134 from the Examiner’s final decision rejecting claims 1–15. We have jurisdiction under 35 U.S.C. § 6(b). We AFFIRM. Appeal 2012-011212 Application 11/714,750 2 THE CLAIMED SUBJECT MATTER Claim 1, reproduced below, is illustrative of the claimed subject matter on appeal. 1. A method of repairing a defect in a splitter fairing of a turbine engine, the method comprising: removing a forward portion of the splitter fairing along a radial line from a central axis of the turbine engine, the forward portion comprising an inner flange and outer surface that create a channel, wherein an original portion of the splitter fairing is salvaged; welding a replacement ring to the original portion, the replacement ring having minimum dimensions equal to the maximum height and width of the removed forward portion; removing material from the replacement ring to obtain a profile with essentially the same profile for the inner flange, outer surface, and channel as an original specifications for the splitter fairing. EVIDENCE The Examiner relied on the following evidence in rejecting the claims on appeal: Swick et al. Bogard et al. Nolan et al. Templeton Mussen Trewiler et al. Roedl et al. US 3,449,816 US 5,205,465 US 6,128,820 US 6,301,780 B1 US 2005/0172485 A1 US 6,969,826 B2 US 7,278,829 B2 June 17, 1969 April 27, 1993 Oct. 10, 2000 Oct. 16, 2001 Aug. 11, 2005 Nov. 29, 2005 Oct. 9, 2007 Appeal 2012-011212 Application 11/714,750 3 REJECTIONS Claims 1–3, 7, 9–11, and 15 stand rejected under 35 U.S.C. § 103(a) as being unpatentable over Appellants’ Admitted Prior Art1 (hereinafter “AAPA”), Bogard, and Mussen. Ans. 5–9. Claims 4 and 12 stand rejected under 35 U.S.C. § 103(a) as being unpatentable over AAPA, Bogard, Mussen, and Nolan and/or Templeton. Id. at 9–10. Claims 5 and 14 stand rejected under 35 U.S.C. § 103(a) as being unpatentable over AAPA, Bogard, Mussen, and Trewiler. Id. at 10–11. Claims 6 and 13 stand rejected under 35 U.S.C. § 103(a) as being unpatentable over AAPA, Bogard, Mussen, Trewiler, and Roedl. Id. at 11. Claim 8 stands rejected under 35 U.S.C. § 103(a) as being unpatentable over AAPA, Bogard, Mussen, 2 and Swick. Id. at 11–12. OPINION The Examiner finds that AAPA teaches that splitter fairings are known in the art and that the front hooks of splitter fairings often need repair. Ans. 5 (citing AAPA). The Examiner relies on Bogard’s teachings 1 The Examiner refers to paragraphs 2 and 3 as set forth in the “Background of the Invention” section of the Specification as Appellants’ Admitted Prior Art. Ans. 5. 2 Appellants assume claim 8 is rejected as being unpatentable over AAPA, Bogard, Mussen, and Swick, despite the Examiner’s reference to Ivakitch (US 2008/0069697 A1, pub. Mar. 20, 2008) instead of Mussen in the Final Rejection mailed June 9, 2011. Br. 4. We consider the Examiner’s failure to replace the reference to Ivakitch in the Final Rejection with a reference to Mussen in the Examiner’s Answer to be an inadvertent error in light of the prior art relied upon in the rejection of claim 1 from which claim 8 indirectly depends. Appeal 2012-011212 Application 11/714,750 4 relating to a method of repairing an airseal land 12 on a turbine that involves (i) machining away a damaged airseal land; (ii) leaving a stub of original material, and (iii) attaching an oversized ring of material to the stub, the oversized ring then being machined to match the original configuration. Id. at 6 (citing Bogard, Abstr., 3:1–2, 59–62, 4:3–6, Figs. 2, 5, 6, 7, 8, and 9). The Examiner reasons that “[i]t would have been obvious to one of ordinary skill in the art . . . to use the repair method of Bogard on the splitter fairing of AAPA to yield a predictable repair.” Id. at 7. The Examiner explains that Bogard’s airseal land repair technique is for a similar device to the AAPA’s splitter fairing and is also inside the same type of engine (i.e., a turbine). Id. The Examiner further finds that “the concept of cutting off a damaged component portion, joining . . . on an oversized replacement portion, and grinding down the replacement portion to original specifications is a well- known repair technique.” Id. (citing, for example, Bogard, Mussen, and Trewiler). The Examiner acknowledges that Bogard does not explicitly teach welding the oversized ring of material to the stub. Id. The Examiner, however, finds that Mussen teaches using electron beam welding to weld replacement stator vane segments in a turbine. Id. at 8. The Examiner concludes that “[i]t would have been obvious to one of ordinary skill in the art . . . to modify Bogard to try and use the welding technique of Mussen because it is obvious to apply a known technique to a known product or method to yield predictable results.” Id. The Examiner explains that the repaired part of Mussen “need[s] to survive in the same temperature and environment as the seal component of Bogard” and that Mussen teaches, for Appeal 2012-011212 Application 11/714,750 5 example, the successful repair of vanes on a Pratt & Whitney 4000 high pressure compressor. Id. Appellants argue that Bogard “teaches away from the claimed repair by requiring forge joining of components” as Bogard states that inertia welding is unsatisfactory to maintain mechanical properties of the repaired element. Br. 4–5 (citing Bogard, 1:62–66). This argument is not persuasive because “[a] reference does not teach away . . . if it merely expresses a general preference for an alternative invention but does not ‘criticize, discredit, or otherwise discourage’ investigation into the invention claimed.” DePuy Spine, Inc. v. Medtronic Sofamor Danek, Inc., 567 F.3d 1314, 1327 (Fed. Cir. 2009) (quoting In re Fulton, 391 F.3d 1195, 1201 (Fed. Cir. 2004)). At most, Appellants have pointed out how Bogard criticizes or discredits the use of inertia welding in particular, but not other types of welding specifically contemplated by Appellants, such as electron beam welding. See Ans. 12–13. Appellants further argue that Bogard’s airseal land “is located in an entirely different area of an engine than the claimed splitter fairing of claim 1.” Br. 5. Both Bogard’s airseal land and AAPA’s splitter fairing are located in high temperature regions of a turbine engine (see, e.g., Bogard, 2:8–11), and Appellants do not persuasively explain why one of ordinary skill in the art would not have found Bogard’s method of repair to be predictable for use in connection with a splitter fairing. See also Ans. 14 (stating that “Appellant[s] ha[ve] provided no mechanical reasons that would prevent using this basic and conventional repair technique on a splitter fairing.”). Appeal 2012-011212 Application 11/714,750 6 Appellants argue that Mussen also “teaches away from the claimed invention” because “Mussen specifically teaches removal [of a portion of the component of a turbine engine] in a direction counter to the claim language,” that is, removal of material that is “either parallel or at an angle to axis of the engine, not along a generally radial line from the central axis.” Br. 5 (citing Mussen, Fig. 5). Appellants’ additional “teach away” argument is not persuasive because Appellants do not identify any passages in Mussen that criticize, discredit, or discourage the removal of material along a generally radial line from the central axis. See DePuy Spine, 567 F.3d at 1327. Appellants’ additional argument that “the part being repaired in Mussen is neither a splitter fairing . . . nor a generally cylindrical part” (Br. 5) is also not persuasive because it fails to address the rejection as articulated by the Examiner in which Mussen is relied on for the specific teaching of welding in connection with AAPA (teaching a splitter fairing) as already modified by Bogard (teaching a specific repair method). In summary, Appellants have not persuasively explained why the Examiner’s articulated reasoning for combining AAPA, Bogard, and Mussen, namely, the application of known techniques to a known product or method to yield predictable results, lacks a rational underpinning. See KSR Int’l Co. v. Teleflex Inc., 550 U.S. 398, 418 (2007) (citing In re Kahn, 441 F.3d 977, 988 (Fed. Cir. 2006) (“[R]ejections on obviousness grounds . . . [require] some articulated reasoning with some rational underpinning to support the legal conclusion of obviousness.”)). For the foregoing reasons, we sustain the Examiner’s rejection of independent claims 1 and 9, which Appellants argue as a group. Br. 4–7; 37 C.F.R. § 41.37(c)(1)(vii) (2011). We also sustain the Examiner’s Appeal 2012-011212 Application 11/714,750 7 rejections of dependent claims 2–8 and 10–15, for which Appellants rely on the same arguments and reasoning. See Br. 7. DECISION The Examiner’s decision to reject claims 1–15 is affirmed. No time period for taking any subsequent action in connection with this appeal may be extended under 37 C.F.R. § 1.136(a). See 37 C.F.R. § 1.136(a)(1)(iv). AFFIRMED llw Copy with citationCopy as parenthetical citation