Ex Parte WeidmannDownload PDFPatent Trial and Appeal BoardSep 27, 201813390304 (P.T.A.B. Sep. 27, 2018) Copy Citation UNITED STA TES p A TENT AND TRADEMARK OFFICE APPLICATION NO. FILING DATE 13/390,304 02/13/2012 23911 7590 10/01/2018 CROWELL & MORING LLP INTELLECTUAL PROPERTY GROUP P.O. BOX 14300 WASHINGTON, DC 20044-4300 FIRST NAMED INVENTOR Wilfried Weidmann 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 ATTORNEY DOCKET NO. CONFIRMATION NO. Ol 1235.64164US 4518 EXAMINER BEEBE, JOSHUA R ART UNIT PAPER NUMBER 3745 NOTIFICATION DATE DELIVERY MODE 10/01/2018 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): edocket@crowell.com tche@crowell.com apomeroy@crowell.com PTOL-90A (Rev. 04/07) UNITED STATES PATENT AND TRADEMARK OFFICE BEFORE THE PATENT TRIAL AND APPEAL BOARD Ex parte WILFRIED WEIDMANN 1 Appeal2017-010367 Application 13/390,304 Technology Center 3700 Before MICHAEL L. HOELTER, LEE L. STEPINA, and ALYSSA A. FINAMORE, Administrative Patent Judges. STEPINA, Administrative Patent Judge. DECISION ON APPEAL STATEMENT OF THE CASE Appellant appeals under 35 U.S.C. § 134(a) from the Examiner's decision to reject claims 12 and 14--25. We have jurisdiction under 35 U.S.C. § 6(b ). We AFFIRM. 1 The Appeal Brief indicates that MTU Aero Engines GmbH is the real party in interest. Appeal Br. 1. Appeal2017-010367 Application 13/390,304 CLAIMED SUBJECT MATTER The claims are directed to a turbomachine that enables radial movability of guide blade ring segments. Spec. ,r,r 2, 4. Claim 12, reproduced below, is illustrative of the claimed subject matter: 12. A turbomachine, comprising: a housing having a pair of radially inwardly extending housing components; a guide blade ring, wherein an outer shroud of the guide blade ring is divided into segments by respective joints; a first fastening element including a groove running in a circumferential direction to receive a first one of the pair of inwardly extending housing components; and a second fastening element defined by a second one of the pair of radially inwardly extending housing components and including a first slot and/or a first nose which meshes with a second nose and/or a second slot, respectively, in a component of the outer shroud that projects radially outwardly; wherein the component of the outer shroud that projects radially outwardly engages the first fastening element and the second fastening element such that the outer shroud is fastened to the housing by the first fastening element and the second fastening element; wherein an axial force is absorbable by the first fastening element, wherein a circumferential force is absorbable by the second fastening element, and wherein a movement in a radial direction for a segment of the outer shroud is enableable by the first fastening element and the second fastening element. Appeal Br. 11 (Claims App.). REFERENCES The prior art relied upon by the Examiner in rejecting the claims on appeal is: Petrie Vinciguerra Humhauser us 2,903,237 us 4,632,634 us 5,601,407 2 Sept. 8, 1959 Dec. 30, 1986 Feb. 11, 1997 Appeal2017-010367 Application 13/390,304 Rogers Dube Coign Durand US 2002/0197153 Al US 2006/0153683 Al US 7,094,026 B2 US 2007 /0231132 Al REJECTIONS Dec. 26, 2002 July 13, 2006 Aug.22,2006 Oct. 4, 2007 (I) Claims 12, 14--21, and 23-25 are rejected under 35 U.S.C. § 103 as unpatentable over Rogers, Durand, and Petrie. 2 (II) Claim 15 is rejected under 35 U.S.C. § I03(a) as unpatentable over Rogers, Durand, Petrie, and Coign. (III) Claim 20 is rejected under 35 U.S.C. § I03(a) as unpatentable over Rogers, Durand, Petrie, and Vinciguerra. (IV) Claim 22 is rejected under 35 U.S.C. § I03(a) as unpatentable over Rogers, Durand, Petrie, and Humhauser. OPINION Rejection (I) Claims 12, 14-21, 23, and 24 The Examiner finds Rogers teaches many of the elements recited in claim 12, including a first fastening element (front outer ring 35 or rear outer ring 37) and a second fastening element (portion including slot 55). Final Act. 2--4. However, the Examiner finds that Rogers does not teach that (i) "there is a groove formed in the first fastening element in a circumferential direction to receive a first one of the pair of inwardly extending housing components" or that (ii) "[ t ]he outer shroud radially outward projections are 2 Although not relied upon to disclose any specific claimed structure, the Examiner refers to Dube as teaching a benefit of reducing excess projecting material between projections in gas turbine engine components. Final Act. 5. 3 Appeal2017-010367 Application 13/390,304 a single component that engages the first and second fastening elements." Final Act. 4. Regarding the above-noted groove, the Examiner finds that Durand teaches that ring sector 20 (including frustoconical wall 32) is received in a groove in vane element 13 and works as an axial location element. Final Act. 4 (citing Durand ,r,r 31-37, Fig. 2); see also Ans. 4--7. The Examiner reasons that modifying front outer ring 35 of Rogers to form a single element with a circumferential groove would reduce complexity by reducing the number of parts and would more securely axially lock the stator outer air seal. Id.; see also Ans. 6-7. Thus, instead of providing two separate elements (front outer ring 35 and rear outer ring 37) that interact with outer vane platform 23 and outer edge 39, the Examiner's proposed modification to Rogers provides a single element (including a circumferential groove) that interacts with outer vane platform 23 and outer edge 39. Ans. 6-7. As for the recited component that engages first and second fastening elements, the Examiner relies on Petrie to teach this feature. Final Act. 5 (citing Petrie, 3:57-73). Specifically, the Examiner finds that Petrie discloses radial dog 52 engaging both notch 53 and upstanding nibs 54. Id. The Examiner reasons that it would have been obvious to a person of ordinary skill in the art to modify lug member 53 3 of Rogers "such that instead of two components (35, 53), a single outer shroud component such as component (52 of Petrie) could be used, as taught by Petrie, for the purpose of reducing excess weight" and simplifying manufacture by reducing the number of required projections. Id. In support of this 3 Rogers uses reference number 53 to refer to a lug member (see Rogers ,r 21, Fig. 3), whereas Petrie uses reference number 53 to refer to a notch (see Petrie, 3:59-63, Fig. 4) 4 Appeal2017-010367 Application 13/390,304 reasoning, the Examiner states, "it is also well-known in the art to reduce excess weight in any outer shroud by removing any excess projecting space." Final Act. 5 (referencing Dube ,r 25). Appellant first argues that the Examiner erred in finding that front outer ring 35 or rear outer ring 37 of Rogers qualifies as a first fastening element as recited in claim 12. Appeal Br. 4. According to Appellant, the Examiner's characterization of these outer rings is incorrect "because neither the Rogers['] front outer ring 35 nor the Rogers['] rear outer ring 37 includes 'a groove running in a circumferential direction to receive' any component of the Rogers['] engine casing 43, identified as the 'housing' required by claim 12." Id. Appellant's argument on this point is unavailing because the Examiner acknowledges this deficiency in Rogers and proposes to modify front outer ring 3 5 of Rogers to include a groove running in a circumferential direction as recited in claim 12, based on the teachings of Durand. Final Act. 4. Accordingly, Appellant's argument on this point does not address the proposed combination of the teachings of Rogers and Durand and amounts to an attack on Rogers individually. Next, Appellant asserts the Examiner erred in finding that slot 55 in Rogers satisfies the requirement in claim 12 for a second fastening element because claim 12 recites that the second fastening element includes a slot. Appeal Br. 4. Specifically, Appellant contends, "[the Examiner's] characterization is ... inappropriate, because the Rogers slot 55, itself, does not, and the inwardly projecting walls delimiting or defining that slot 55, themselves, do not, include 'a first slot and/or a first nose' as claim 12 requires." Id.; see also Reply Br. 2-3. 5 Appeal2017-010367 Application 13/390,304 We disagree with Appellant because, to the extent claim 12 requires a distinct component including a slot as asserted by Appellant, Rogers discloses such a component. Specifically, as shown in Figure 1 of Rogers, the portion of engine casing 43 that engages lug member 53 (and including slot 55) is different in shape from the remainder of engine casing 43. We reproduce a portion4 of Figure 1 of Rogers below. :JD 58 37 ' Figure 1 of Rogers is a partial cross-sectional view through the stator of a gas turbine engine (Rogers ,r 14), and the portion reproduced above includes vane segment 19 and lug member 53 and its connection to 4 The portion of Figure 1 of Rogers reproduced below is approximately the same area from Figure 1 appearing on page 5 of the Final Office Action. 6 Appeal2017-010367 Application 13/390,304 engine casing 43. Also depicted is a section line (unnumbered) used for creating Figure 3 of Rogers, which depicts lug member 53 within slot 55. As is evident from Figure 1 of Rogers, engine casing 43 includes a projection where lug member 53 engages engine casing 43 via slot 55. Figure 3 does not show this projection because of where the section line used to create Figure 3 is located. See Rogers ,r 16 ( explaining the relationship between Figures 1 and 3). Accordingly, a preponderance of the evidence supports the Examiner's finding that Rogers discloses a second fastening element "including a first slot and/or a first nose" as recited in claim 12. Appellant next argues that even if the two arguments discussed above are not persuasive, "the Rogers ... lug members 53 would still fail to form a component of the outer shroud that projects radially outwardly that 'engages the first fastening element and the second fastening element' ( emphasis added) as claim 12 defines." Appeal Br. 5. In this regard, Appellant states, "[t]he lug members 53 ... do not engage with either the Rogers front outer ring 35 or the Rogers rear outer ring 37." Id. Therefore, according to Appellant, Rogers fails to disclose that lug member 53 engages the first fastening element (in addition to engaging the second fastening element) as recited in claim 12. Id. Appellant's argument on this point does not address the Examiner's proposed modification to Rogers' structure. See Final Act. 5. Specifically, the Examiner proposes to modify Rogers' projection "to orient in the other direction as that of Petrie, such that instead of two components (35, 53), a single outer shroud component such as component (52 of Petrie) could be used." Id. Accordingly, Appellant's argument is unpersuasive. 7 Appeal2017-010367 Application 13/390,304 Appellant discusses Petrie from page 5 to page 6 of the Appeal Brief, concluding the discussion by stating that Petrie: cannot properly be considered to suggest altering the Rogers turbine vane support structure so as to include at least a first fastening element "including a groove running in a circumferential direction to receive a first one of the pair of inwardly extending housing components" as lines 5-6 in claim 12 require and that is engaged by the component, purportedly formed by the Rogers lug member 53, of the outer shroud that projects radially outwardly, as lines 11-13 in claim 12 define. Id. at 6. Appellant's statement relates the disclosure of Petrie to the recited first fastening element. See Appeal Br. 11 (Claims App.). The Examiner relies on Rogers, modified based on the teachings of Durand (not Petrie), to teach the recited first fastening element. Final Act. 3--4. Accordingly, Appellant's argument relating to Petrie and the first fastening element recited in claim 12 is unpersuasive. Appellant discusses Durand from page 6 to page 7 of the Appeal Brief and contends that Rogers provides a stator stage 1 7 that is mounted between axially spaced-apart rotor stages 13 and 15, and that the stator stage 1 7 includes stator vane segments 19. Appellant further contends that "[ t ]he frustoconical wall 32 referred to in lines 1--4 of the last paragraph on page 4 of the final Office Action, while forming part of an enclosure for the Durand ... rotor 18, does not concern guide or stator vanes of the Durand ... structure." Appeal Br. 7. Appellant concludes that Durand does not suggest the modification to Rogers set forth in the Final Office Action because front outer ring 35, rear outer ring 37, and slot 55 of Rogers are all elements of Rogers's stator stage. Id. The Examiner explains that Durand was cited for the general teaching of a fastening element with a circumferential groove for receiving a housing 8 Appeal2017-010367 Application 13/390,304 component. Id. at 6. Although Appellant argues that Durand does not suggest the Examiner's proposed modification to the structure of Rogers, Appellant does not contest persuasively the Examiner's findings of fact regarding the disclosure of Durand. Appeal Br. 3-9; see also Final Act. 4. Nor does Appellant assert that the proposed modification would fail to reduce complexity or provide a more securely retained seal in Rogers as the Examiner determines on page 4 of the Final Office Action and reiterates on pages 6 to 7 of the Answer. Id. Accordingly, we are not apprised of Examiner error by Appellant's contentions. We have considered all of Appellant's arguments regarding the rejection of claim 12, but determine the Examiner has the better position. Accordingly, we sustain the rejection of claim 12 as unpatentable over Rogers, Durand, and Petrie. Appellant does not present separate arguments for dependent claims 14--21, and 23, and 24 apart from the arguments for independent claim 12. Appeal Br. 7. Therefore, we sustain the rejection of claims 14--21, 23, and 24 for the same reasons discussed above regarding the rejection of independent claim 12. Claim 25 Appellant relies on the arguments discussed above regarding the rejection of claim 12 in support of the patentability of independent claim 2 5. Appeal Br. 7-8. For the same reasons discussed above, we sustain the rejection of claim 25 as unpatentable over Rogers, Durand, and Petrie. Re} ections (II)-(IV) Claims 15, 20, and 22 Appellant does not present separate arguments for dependent claims 15, 20, and 22 apart from the arguments for independent claim 12. Appeal 9 Appeal2017-010367 Application 13/390,304 Br. 8-9. For the same reasons discussed above regarding Rejection (I), we sustain Rejections (II}-(IV). DECISION (I) The rejection of claims 12, 14--21, and 23-25 as unpatentable over Rogers, Petrie, and Durand is affirmed. (II) The rejection of claim 15 as unpatentable over Rogers, Petrie, Durand, and Coign is affirmed. (III) The rejection of claim 20 as unpatentable over Rogers, Petrie, Durand, and Vinciguerra is affirmed. (IV) The rejection of claim 22 as unpatentable over Rogers, Petrie, Durand, and Humhauser 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)(l )(iv). AFFIRMED 10 Copy with citationCopy as parenthetical citation