Ex Parte Suciu et alDownload PDFPatent Trials and Appeals BoardMay 3, 201914695578 - (D) (P.T.A.B. May. 3, 2019) Copy Citation UNITED STA TES p A TENT AND TRADEMARK OFFICE APPLICATION NO. FILING DATE FIRST NAMED INVENTOR 14/695,578 04/24/2015 Gabriel L. Suciu 54549 7590 05/07/2019 CARLSON, GASKEY & OLDS/PRATT & WHITNEY 400 West Maple Road Suite 350 Birmingham, MI 48009 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. 81062US02; 67097-3188PUS1 4397 EXAMINER BEEBE, JOSHUA R ART UNIT PAPER NUMBER 3745 NOTIFICATION DATE DELIVERY MODE 05/07/2019 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 GABRIELL. SUCIU, JESSE M. CHANDLER, JOSEPH BRENT STAUBACH, and BRIAND. MERRY Appeal 2018-005114 Application 14/695,578 Technology Center 3700 Before MICHAEL J. FITZPATRICK, JEREMY M. PLENZLER, and LISA M. GUIJT, Administrative Patent Judges. PLENZLER, Administrative Patent Judge. DECISION ON APPEAL STATEMENT OF THE CASE Appellant seeks our review under 35 U.S.C. § 134(a) of the Examiner's Decision rejecting claims 1-20. We have jurisdiction under 35 U.S.C. § 6(b). We AFFIRM. Appeal 2018-005114 Application 14/695,578 CLAIMED SUBJECT MATTER Claims 1 and 15 are independent. Claims 2-14 depend from claim 1 and claims 16-20 depend from claim 15. Claim 1 is reproduced below: 1. A gas turbine engine comprising; a main compressor section having a high pressure compressor with a downstream discharge, and more upstream locations; a turbine section having a high pressure turbine; and a tap tapping air from at least one of said more upstream locations in said compressor section, passing said tapped air through a heat exchanger and then to a cooling compressor, said cooling compressor compressing air downstream of said heat exchanger, and delivering air into said high pressure turbine. REJECTIONS 1. Claims 1-3 and 15 are rejected under 35 U.S.C. § I03(a) as being unpatentable over Elovic (US 4,254,618, issued Mar. 10, 1981) and Glickstein (US 5,452,573, issued Sept. 26, 1995). 2. Claim 4 is rejected under 35 U.S.C. § I03(a) as being unpatentable over Elovic, Glickstein, and "an engineering expedient." 3. Claims 5-10 and 18-20 are rejected under 35 U.S.C. § I03(a) as being unpatentable over Elovic, Glickstein, and Bruno (US 2007 /0213917 Al, published Sept. 13, 2007). 4. Claims 11 and 12 are rejected under 35 U.S.C. § I03(a) as being unpatentable over Elovic, Glickstein, Bruno, and Ress (US 2013/0199156 Al, published Aug. 8, 2013). 5. Claims 13, 14, 16, and 17 are rejected under 35 U.S.C. § I03(a) as being unpatentable over Elovic, Glickstein, and Ress. 2 Appeal 2018-005114 Application 14/695,578 OPINION Claims 1--4 and 15 The Examiner finds that Elovic teaches each limitation of claims 1 and 15, including "a tap tapping air from at least one of said more upstream locations in said compressor section, passing said tapped air through a heat exchanger" and "delivering air into said high pressure turbine," but does not expressly teach passing the tapped air "to a cooling compressor ... compressing air downstream of said heat exchanger" before delivering the air to the high pressure turbine. Final Act. 3--4, 5---6. The Examiner finds that Glickstein teaches use of a downstream compressor for cooling and proposes supplementing Elovic's teachings accordingly, explaining that [i]t would have been obvious ... to modify the heat exchange flow cooling system of [Elovic] to include a downstream compressor as taught by [Glickstein] for the purposes of providing improved pressure of cooling from lower stage, ( colder) air, but still meeting the high pressure cooling needs of the turbine. Id. at 4; see also id. at 6 (providing same finding and rationale with respect to claim 15). The Examiner supplements this finding and rationale, citing Coffinberry 1, and particularly column 1, lines 20-31 and 55---65, "as evidence in disclosing the low pressure of cooling air can be undesirable in turbine cooling and using auxiliary air to raise the pressure of such compressor bled cooling air can be desirable" and explaining that "[t]his can be used especially to increase the capacity of the turbine to handle the thermal extreme operation temperatures." Id. at 4, 6. 1 US 5,392,614, issued Feb. 28, 1995. 3 Appeal 2018-005114 Application 14/695,578 Appellant responds that although "the Examiner argues that Elovic does disclose taking air from a more upstream location ... there is no showing why it might be 'desirable' to do so." Appeal Br. 2. That contention is not persuasive. There is no modification proposed to Elovic' s teachings in this regard. Rather, as noted above, the Examiner relies on the express teaching of this limitation in Elovic. Appellant does not dispute the Examiner's finding that the "location other than the compressor discharge" referenced at column 6, line 32 in Elovic must be a "more upstream location[]" as recited in the claims. See, e.g., Final Act. 4 ("Col. 6, 11. 30-40 disclose extracting the cooling air [from] the compressor at locations other than (therefore they must be upstream) of the discharge."). Appellant also does not dispute the specific findings made by the Examiner in connection with Glickstein, but contends that "Glickstein does not supply air to cool a turbine" and "[t]he air tap at 101 in Glickstein appears to be delivered to a compressor 60, but then to a heat exchanger." Appeal Br. 3. Appellant explains that "[n]ot only does this not disclose compressing air on the way to the turbine, it also does not meet the order of the air encountering the heat exchanger and a cooling compressor as required by claims 1 and 15." Id. The problem with this argument is that it does not address the rejection presented by the Examiner. The Examiner finds that Elovic teaches the recited air tap and supplying air to cool the turbine. Final Act. 4, 5. Appellant further contends that "[t]o find the proposed combination is proper requires including an extra compressor into the system of Elovic in view of Glickstein et al." Appeal Br. 3. Appellant reiterates that "the Examiner proposes no reason why it 'might be desirable' to tap Elovic at a 4 Appeal 2018-005114 Application 14/695,578 location other than the discharge," which is unpersuasive as explained above, and then concludes that "there is certainly no reason to include the cost and complexity of an extra compressor as alleged[ly] suggested by Glickstein." Id. Appellant, however, never addresses the rationale set forth by the Examiner and, therefore, does not apprise us of error. Moreover, Appellant's contentions support a determination that one skilled in the art would have found it obvious to include an additional compressor in Elovic' s system when extracting cooling air at a location other than discharge (i.e., an upstream location). See Appeal Br. 2-3 Appellant explains that because "the air must pass into the high pressure turbine, it would desirably be at a high pressure, and not at a lower pressure." Id. Without a pressurizing mechanism for the cooling air, such as an additional compressor, in Elovic's system, Appellant explains that "[i]t is counterintuitive to tap the air from a lower pressure location." Id. at 3. Appellant does not present separate arguments for the patentability of claims 2--4, which depend from claim 1. For at least the reasons set forth above, we are not apprised of error in the Examiner's decision to reject claims 1--4 and 15. Claims 5-10 and 18-20 Appellant argues claims 5-10 and 18-20 as a group. Appeal Br. 3--4. We select claim 5 as representative. Claims 6-10 and 18-20 stand or fall with claim 5. See 37 C.F.R. § 4I.37(c)(l)(iv). Claim 5 depends from claim 1 and further recites "said turbine section driving a tower shaft, said tower shaft further driving an impeller of said cooling compressor." The Examiner finds that Bruno teaches the additional features recited in claim 5 and proposes further modifying the teachings of Elovic 5 Appeal 2018-005114 Application 14/695,578 accordingly. Final Act. 7-8. The Examiner explains, for example, that such a modification would provide "powering said pump with the advantage of controllable power of the compressor." Id. at 8. Appellant does not dispute the Examiner's findings or rationale related to claim 5. Rather, Appellant alleges, generally, and without meaningful explanation, that "[t]here is no reason why one would modify Glickstein in view of Bruno to have a tower shaft drive" and "to do so would complicate Glickstein et al. and provide no apparent benefit." App. Br. 3--4. These general allegations do not apprise us of error in the specific findings and rationale set out by the Examiner. For at least these reasons, we are not apprised of error in the Examiner's decision to reject claims 5-10 and 18-20. Claims 11-14, 16, and 17 Appellant argues claims 11 and 12 as a group and claims 13, 14, 16, and 17 as a group. Appeal Br. 4. We select claims 11 and 13 as representative of the respective groups. Claim 12 stands or falls with claim 11, and claims 14, 16, and 17 stand or fall with claim 13. Claim 11 depends from claim 1 via dependency from claim 5, and claim 13 depends from claim 1. Claims 11 and 13 each further recite that "an auxiliary fan is positioned upstream of the heat exchanger." The Examiner finds that Ress teaches the additional features recited in claims 11 and 13, and proposes further modifying the teachings of Elovic accordingly. Final Act. 10, 11. Specifically, the Examiner reasons that "[i]t would have been obvious ... to include an auxiliary fan downstream of the primary fan and upstream of the bypass flow" to "improve[ e] the engine[] transient operating conditions and its ability to operate in variable thrust and 6 Appeal 2018-005114 Application 14/695,578 bypass modes as desired." Id. at 10; see also id. at 11 (providing same rationale for claim 13). Again, Appellant does not dispute the Examiner's findings or rationale in any meaningful way. Appellant simply alleges that "there is no reason why Ress would suggest incorporating additional structure into Elovic" and further alleges, without explanation, that "[t]his combination appears to be driven solely by hindsight reconstruction." Appeal Br. 4. For at least the reasons set forth above, we are not apprised of error in the Examiner's decision to reject claims 11-14, 16, and 17. DECISION We AFFIRM the Examiner's decision to reject claims 1-20. No time period for taking any subsequent action in connection with this appeal may be extended under 37 C.F.R. § 1.136(a)(l)(iv). AFFIRMED 7 Copy with citationCopy as parenthetical citation