HONEYWELL INTERNATIONAL INC.Download PDFPatent Trials and Appeals BoardOct 22, 202015237834 - (D) (P.T.A.B. Oct. 22, 2020) 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. 15/237,834 08/16/2016 Yufei Xiong H0054785 (002.4786) 2521 89955 7590 10/22/2020 HONEYWELL/LKGLOBAL Intellectual Property Services Group 300 S. Tryon Street Suite 600 Charlotte, NC 28202 EXAMINER GRAVES, TIMOTHY P ART UNIT PAPER NUMBER 2856 NOTIFICATION DATE DELIVERY MODE 10/22/2020 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): DL-PMT-SM-IP@Honeywell.com honeywell@lkglobal.com patentservices-us@honeywell.com PTOL-90A (Rev. 04/07) UNITED STATES PATENT AND TRADEMARK OFFICE ____________ BEFORE THE PATENT TRIAL AND APPEAL BOARD ____________ Ex parte YUFEI XIONG, RONNIE HAUGLAND, and SCOT COFFEY ____________ Appeal 2020-000342 Application 15/237,834 Technology Center 2800 ____________ Before KAREN M. HASTINGS, N. WHITNEY WILSON, and WESLEY B. DERRICK, Administrative Patent Judges. PER CURIAM DECISION ON APPEAL Appellant1 seeks our review under 35 U.S.C. § 134(a) of the Examiner’s Final Rejection of claims 1–4 and 11–14 under 35 U.S.C. § 103(a) as being unpatentable over Rowe (US 2013/0319092, published December 5, 2013), and claims 8 and 18 as unpatentable over the 1 We use the word “Appellant” to refer to the “applicant” as defined in 37 C.F.R. § 1.42. Appellant identifies Honeywell International, Inc. as the real party in interest (Appeal Br. 2). Appeal 2020-000342 Application 15/237,834 2 combined prior art of Rowe and Larkin (US 5,303,545, issued April 19, 1994).2 We have jurisdiction over the appeal under 35 U.S.C. § 6(b). We REVERSE. Claim 1 is illustrative of the claimed subject matter (emphasis added to highlight key disputed limitations): 1. A method for detecting a shaft break in a turbofan gas turbine engine, the turbofan engine including at least a fan and a turbine, the method comprising the steps of: sensing fan rotational speed; sensing turbine engine rotational speed; determining, in a processor, a rate of change of rotational speed difference between the sensed fan rotational speed and the sensed turbine engine rotational speed; and determining, in the processor, that a shaft break has occurred based at least in part on the rate of change of the rotational speed difference. Appeal Br. 15 (Claims Appendix). Independent claim 11 is directed to a system which requires a processor configured to “determine a rate of change of rotational speed difference between the sensed fan rotational speed and the sensed turbine engine rotational speed” (Appeal Br. Claims Appendix 18, 19). 2 The Examiner withdrew the rejection of claims 1–20 under 35 U.S.C. §101 (Ans. 3). The Examiner indicated that claims 5–7, 9, 10, 15–17, 19, and 20 would be “allowable subject matter” (Ans. 17). Appeal 2020-000342 Application 15/237,834 3 ANALYSIS The Examiner bears the initial burden of presenting a prima facie case of obviousness. In re Oetiker, 977 F.2d 1443, 1445 (Fed. Cir. 1992). “[R]ejections on obviousness grounds cannot be sustained by mere conclusory statements; instead, there must be some articulated reasoning with some rational underpinning to support the legal conclusion of obviousness.” In re Kahn, 441 F.3d 977, 988 (Fed. Cir. 2006), quoted with approval in KSR Int’l Co. v. Teleflex Inc., 550 U.S. 398, 418 (2007). After review of the respective positions provided by Appellant and the Examiner, we conclude that the preponderance of the evidence supports Appellant’s position that the Examiner has not met the burden in this case for substantially the reasons set forth by Appellant in the Briefs. Accordingly, we reverse the Examiner’s § 103 rejections of all the claims on appeal. We add the following primarily for emphasis. This appeal hinges on whether Rowe renders obvious a method or system that determines “a rate of change of rotational speed difference in combination between the sensed fan rotational speed and the sensed turbine engine rotational speed” as recited in claims 1 and 11. The Examiner relies in part upon an embodiment in Rowe that calculates a rate of change of rotational speed of the engine shaft and calculating the difference in rotational speed between two shafts, stating: It would have been obvious to one of ordinary skill in the art before the effective filing date of the claimed invention to incorporate Rowe's alternative embodiment scheme of basing a shaft break indication on a change in the difference between Appeal 2020-000342 Application 15/237,834 4 shaft speeds with Rowe's first embodiment measuring the speeds at a fan and turbine to determine a shaft break. Doing so would reliably distinguish shaft break from surge or other engine events that require different control response so that the engine is not erroneously shut down. (Final Act. 11) Appellant contends that Rowe does not disclose the feature as claimed and that the Examiner has taken an unreasonably broad interpretation of the claim language (Appeal Br. 10, 11; Reply Br. 5). Appellant points out that calculating the rate of change of rotational speed as is not the same as calculating a rate of change of rotational speed difference, nor is calculating a change in expected difference in rotational speeds “remotely suggestive of calculating a rate of change of rotational speed difference” (Appeal Br. 11; Reply Br. 5). While we appreciate the Examiner’s position that Rowe describes a shaft break detection system based on rotational speed difference using data collected over time (e.g., Ans. 4, Rowe ¶ 48), it does not follow that what is disclosed amounts to determining the difference in the rotational speed of the fan and turbine as a function of time, that is, calculating “the rate of change in rotational speed difference” as claimed. The detection of rotational speed differences reaching a predetermined threshold is simply not the same as calculating the rate of change in rotational speed difference, even if the system to detect those differences operates over a period of time. “[D]uring examination proceedings, claims are given their broadest reasonable interpretation consistent with the specification.” In re Translogic Tech., Inc., 504 F.3d 1249, 1256 (Fed. Cir. 2007) (quoting In re Hyatt, 211 F.3d 1367, 1372 (Fed. Cir. 2000)). Appeal 2020-000342 Application 15/237,834 5 As stated in In re Smith, The correct inquiry in giving a claim term its broadest reasonable interpretation in light of the specification is not whether the specification proscribes or precludes some broad reading of the claim term adopted by the examiner. And it is not simply an interpretation that is not inconsistent with the specification. It is an interpretation that corresponds with what and how the inventor describes his invention in the specification, i.e., an interpretation that is “consistent with the specification.” In re Smith Int’l, Inc., 871 F.3d 1375, 1382–83 (Fed. Cir. 2017) (quoting In re Morris, 127 F.3d 1048, 1054 (Fed. Cir. 1997)). Cf. Phillips v. AWH Corp., 415 F.3d 1303, 1315 (Fed. Cir. 2005) (“[T]he specification ‘is always highly relevant to the claim construction analysis. Usually, it is dispositive; it is the single best guide to the meaning of a disputed term.’” (internal citation omitted)). Appellant’s Specification consistently describes determining the rate of change of the rotational speed difference between the fan rotational speed and the turbine rotational speed (e.g., Spec. ¶¶ 21, 32, 34, 36). We agree with Appellant that the broadest reasonable interpretation of the claim language consistent with the Specification does not encompass merely calculating the rate of change of rotational speed of the fan and/or turbine or a change in expected difference in rotational speeds as proposed by the Examiner (see also, Final Act. 10, where the Examiner relies in part upon Rowe ¶ 6; Final Act. 11). A preponderance of the evidence also supports Appellant’s position that the proposed combination of the two embodiments described in Rowe relied upon by the Examiner to result in the claimed method (or corresponding system of claim 11) would be based on improper hindsight Appeal 2020-000342 Application 15/237,834 6 reconstruction for the reasons discussed by Appellant in the Briefs. The fact finder must be aware “of the distortion caused by hindsight bias and must be cautious of arguments reliant upon ex post reasoning.” KSR, 550 U.S. at 421 (citing Graham v. John Deere Co., 383 U.S. 1, 36 (1966) (warning against a “temptation to read into the prior art the teachings of the invention in issue”)). The Examiner does not rely upon any other reference (e.g., Larkin) to cure these deficiencies. Accordingly, we reverse the § 103 rejections of claims 1–4, 8, 11–14, and 18. CONCLUSION In summary: Claims Rejected 35 U.S.C. § Reference(s)/Basis Affirmed Reversed 1–4, 11–14 103 Rowe 1–4, 11–14 8, 18 103 Rowe, Larkin 8, 18 Overall Outcome 1–4, 8, 11–14, 18 REVERSED Copy with citationCopy as parenthetical citation