Ex Parte CloftDownload PDFPatent Trial and Appeal BoardJun 9, 201713216281 (P.T.A.B. Jun. 9, 2017) Copy Citation United States Patent and Trademark Office UNITED STATES DEPARTMENT OF COMMERCE United States Patent and Trademark Office Address: COMMISSIONER FOR PATENTS P.O.Box 1450 Alexandria, Virginia 22313-1450 www.uspto.gov APPLICATION NO. FILING DATE FIRST NAMED INVENTOR ATTORNEY DOCKET NO. CONFIRMATION NO. 13/216,281 08/24/2011 Thomas G. Cloft PA0010410-U; 3815 67097-1549PU 54549 7590 06/13/2017 CARLSON, GASKEY & OLDS/PRATT & WHITNEY 400 West Maple Road Suite 350 Birmingham, MI 48009 EXAMINER BROWN, ADAM WAYNE ART UNIT PAPER NUMBER 3745 NOTIFICATION DATE DELIVERY MODE 06/13/2017 ELECTRONIC Please find below and/or attached an Office communication concerning this application or proceeding. The time period for reply, if any, is set in the attached communication. Notice of the Office communication was sent electronically on above-indicated "Notification Date" to the following e-mail address(es): ptodocket @ cgolaw. com PTOL-90A (Rev. 04/07) UNITED STATES PATENT AND TRADEMARK OFFICE BEFORE THE PATENT TRIAL AND APPEAL BOARD Ex parte THOMAS G. CLOFT Appeal 2015-0066551 Application 13/216,2812 Technology Center 3700 Before PHILIP J. HOFFMANN, JAMES A. WORTH, and KENNETH G. SCHOPFER, Administrative Patent Judges. HOFFMANN, Administrative Patent Judge. DECISION ON APPEAL STATEMENT OF THE CASE Appellant appeals under 35 U.S.C. § 134(a) from the final rejection of claims 1—5 and 7—20. We have jurisdiction under 35 U.S.C. § 6(b). We REVERSE. 1 Our decision references Appellant’s Specification (“Spec.,” filed Aug. 24, 2011), Appeal Brief (“Appeal Br.,” filed Dec. 19, 2014), and Reply Brief (“Reply Br.,” filed June 30, 2015), as well as the Final Office Action (“Final Action,” mailed Aug. 5, 2014) and Examiner’s Answer (“Answer,” mailed May 1,2015). 2 According to Appellant, “United Technologies Corporation is the real party in interest.” Appeal Br. 1. Appeal 2015-006655 Application 13/216,281 According to Appellant, the invention is directed “to a nacelle assembly for a gas turbine engine that includes an integrated afterbody mount case.” Spec. 11. Claims 1, 7, and 15 are the only independent claims on appeal. Appeal Br., Claims App. We reproduce claim 1, below, as illustrative of the appealed claims. 1. A nacelle assembly for a gas turbine engine, comprising: a fan exhaust nozzle; a core nacelle that includes an afterbody portion that extends aft of said fan exhaust nozzle and an integrated afterbody mount case connected to said afterbody portion, said integrated afterbody mount case including an outer ring having a radially outer surface and a radially inner surface; and a plurality of spokes that extend radially inwardly from said radially inner surface, wherein said plurality of spokes are circumferentially disposed about said outer ring. Id. REJECTIONS AND PRIOR ART The Examiner rejects the claims as follows: I. Claims 1, 3—5, 7—12, and 14—18 under 35 U.S.C. § 103(a) as unpatentable over Balk (WO 2010/007226 A2, pub. Jan. 20, 2010) and Brodell (US 5,524,847, iss. June 11, 1996); II. Claims 13 and 19 under 35 U.S.C. § 103(a) as unpatentable over Balk, Brodell, and Chee (US 5,064,144, iss. Nov. 12, 1991); III. Claim 20 under 35 U.S.C. § 103(a) as unpatentable over Balk, Brodell, and Kraft (US 5,864,922, iss. Feb. 2, 1999); and 2 Appeal 2015-006655 Application 13/216,281 IV. Claims 1 and 2 under 35 U.S.C. § 103(a) as unpatentable over Heyerman (US 8,313,293 B2, iss. Nov. 20, 2012) and Brodell. ANALYSIS Rejection I With respect to the rejection of independent claim 1, Appellant argues in the Appeal Brief that Brodell does not teach the claimed “core nacelle that includes an afterbody portion that extends aft of said fan exhaust nozzle and an integrated afterbody mount case connected to said afterbody portion.” Appeal Br. 3—6, Claims App. In response to Appellant’s argument, the Examiner determines that [a]s explained in the rejection[] of claim[] 1,... it is ... Balk. . . [that] teaches the integrated mount case. Brodell is cited as teaching an afterbody portion (the portion of cowl 44 extending aft of discharge plane 52, as shown in Fig. 1), including attachment links 88, 90, and 92. While links 88, 90, and 92 connect directly to the engine mount beam, cowl 44 also connects to the engine mount beam (col. 6, lines 47[—]50 of Brodell), forming an integrated mount assembly. While Brodell does not teach the specific integrated mount case claimed in independent claims, Balk does teach these limitations. Answer 9. Based on our review of the Final Office Action (see, e.g., Final Action 4—5) and the Answer (see, e.g., Answer 9-12), it is not entirely clear to what extent the Examiner relies on Balk and Brodell, either alone or in combination, to provide the claimed core nacelle afterbody portion that is connected to an afterbody mount case. Nonetheless, for the reasons discussed below, we agree with Appellant that neither Balk (see Reply Br. 2) nor Brodell (see Appeal Br. 4) discloses such an arrangement. 3 Appeal 2015-006655 Application 13/216,281 More specifically, with respect to Balk, the Examiner finds in the rejection of claim 1 in the Final Office Action and Answer, that “Balk teaches ... an integrated afterbody mount case including an outer ring (annular frame 52)...[,] but fails to teach ... a core nacelle that includes an afterbody portion that extends aft of said fan exhaust nozzle wherein the afterbody mount case is connected to said afterbody portion.” Final Action 4; see also Answer 2. Restated, it appears that the Examiner finds that Balk teaches the claimed afterbody mount case, but teaches neither the claimed afterbody portion nor the claimed connection between the afterbody mount case and afterbody portion. Regardless, we agree with Appellant that “[n]o portion of the . . . mount case of Balk [as identified by the Examiner] is ‘connected’ to an afterbody portion of the core nacelle.” Reply Br. 2. With respect to Brodell, the Examiner finds in the rejection of claim 1 in the Final Office Action and Answer, that “Brodell teaches ... a core nacelle (core cowl 44) that includes an afterbody portion that extends aft of said fan exhaust nozzle (reference Fig. 1)[,] wherein afterbody mount hardware (including links 88, 90 and 92) is connected to said afterbody portion (reference Fig. 2).” Final Action 4; see also Answer 2—3. But, even assuming arguendo that Brodell’s afterbody mount hardware teaches the claimed afterbody mount case, we agree with Appellant that “as shown in Figure 1 [of Brodell], the links 88, 90[,] and 92 are not connected to the core cowl 44 of Brodell. Instead, these links are positioned radially inward of the core cowl 44 and extend between an engine mount beam and an engine case that is separate from the core cowl 44.” Appeal Br. 4 (italics omitted). Thus, Brodell does not disclose the claimed connection between the afterbody mount case and afterbody portion. 4 Appeal 2015-006655 Application 13/216,281 Based on the foregoing, neither reference teaches an afterbody mount case connected to an afterbody portion. Further, we determine that neither the Final Office Action nor Answer explains adequately how to combine the teachings of Balk and Brodell to provide an afterbody mount case connected to an afterbody portion. See Appeal Br. 5—6. For example, although the Final Office Action and Answer state that “Balk teaches that using a [sic] circumferentially arranged mounting structures avoids creating undesirable loading on the casing .... Therefore[,] it would have been obvious ... to modify the mounting arrangement of Balk by using it to attach the afterbody portion of a fan as taught by Brodell” (Final Action 4—5; see also Answer 3), the referenced “circumferentially arranged mounting structures” clearly refer to the claimed “plurality of spokes,” which provide a connection between an afterbody mount cases’ outer ring and a turbine exhaust case in which a core engine is disposed (see, e.g., Spec. ]Hf 29-33), and not an integrated connection between an afterbody mount case and an afterbody portion. Regardless, it is not clear that the Examiner proposes combining Balk and Brodell to provide the claimed afterbody mount case connected to an afterbody portion. Thus, for the above reasons, we do not sustain this rejection of independent claim 1, or of its dependent claims 3—5. Inasmuch as independent claims 7 and 15 recite similar recitations, and are rejected for similar reasons by the Examiner, we also do not sustain the rejection of claims 7 and 15 or of dependent claims 8—12, 14, and 16—18. Rejections II and III Because each of claims 13, 19, and 20 depends from an independent claim whose rejection we do not sustain, and the Examiner does not 5 Appeal 2015-006655 Application 13/216,281 establish that any other reference remedies the deficiency in any independent claim’s rejection, we also do not sustain the rejections of these dependent claims. Rejection IV With respect to the rejection of claim 1, the Examiner determines that “Heyerman teaches an integrated mount case while Brodell teaches an afterbody portion of a core nacelle.” Answer 12. Even assuming arguendo that is correct, we do not sustain the rejection for reasons similar to the reason we do not sustain the rejection of claim 1 based on Balk and Brodell—i.e., because neither the Final Office Action nor Answer explains adequately how to combine the teachings of Heyerman and Brodell to provide an afterbody mount case connected to an afterbody portion. See Appeal Br. 6. For example, although the Final Office Action and Answer state that “Heyerman teaches that using circumferentially arranged mounting structures avoids creating undesirable loading on the casing. . . . Therefore[,] it would have been obvious ... to modify the mounting arrangement of Heyerman by using it to attach the afterbody portion of a fan as taught by Brodell” (Final Action 9; see also Answer 7), the referenced “circumferentially arranged mounting structures” clearly refer to the claimed “plurality of spokes,” which provide a connection between an afterbody mount cases’ outer ring and a turbine exhaust case in which a core engine is disposed (see, e.g., Spec. ]Hf 29-33), and not an integrated connection between an afterbody mount case and an afterbody portion. Regardless, it is not clear that the Examiner proposes combining Heyerman and Brodell to provide the claimed afterbody mount case connected to an afterbody portion. 6 Appeal 2015-006655 Application 13/216,281 Thus, based on the above, we do not sustain this rejection of claim 1 or its dependent claim 2. DECISION We REVERSE the Examiner’s obviousness rejections of claims 1—5 and 7—20. REVERSED 7 Copy with citationCopy as parenthetical citation