Ex Parte ShawDownload PDFPatent Trial and Appeal BoardJan 30, 201411375486 (P.T.A.B. Jan. 30, 2014) 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. 11/375,486 03/14/2006 Robert L. Shaw FCA 0001 PA/33558.3 9953 7590 01/30/2014 DINSMORE & SHOHL LLP One Dayton Centre Suite 1300 One South Main Street Dayton, OH 45402-2023 EXAMINER KING, RODNEY P ART UNIT PAPER NUMBER 3665 MAIL DATE DELIVERY MODE 01/30/2014 PAPER 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. PTOL-90A (Rev. 04/07) UNITED STATES PATENT AND TRADEMARK OFFICE ____________________ BEFORE THE PATENT TRIAL AND APPEAL BOARD ____________________ Ex parte ROBERT L. SHAW ____________________ Appeal 2012-002214 Application 11/375,486 Technology Center 3600 ____________________ Before: JENNIFER D. BAHR, MICHAEL L. HOELTER, and NEIL T. POWELL, Administrative Patent Judges. POWELL, Administrative Patent Judge. DECISION ON APPEAL Appeal 2012-002214 Application 11/375,486 2 STATEMENT OF CASE Appellant appeals under 35 U.S.C. § 134 from the Examiner’s Final rejection of claims 1-28. We have jurisdiction under 35 U.S.C. § 6(b). We AFFIRM. THE CLAIMED SUBJECT MATTER Independent claim 1, reproduced below, is illustrative of the appealed subject matter. 1. A backup display system for use in a general aviation aircraft, said backup display system configured to provide flight condition information in the event of partial or complete inoperability of a primary flight instrument system on said general aviation aircraft, said backup display system comprising: a source of electrical power situated on said general aviation aircraft; a plurality of sensors situated on said general aviation aircraft and configured to collect flight data; a processor situated on said general aviation aircraft and cooperative with said source of electrical power and signally coupled to said plurality of sensors such that said processor operates on said collected flight data to generate at least a portion of said flight condition information with need for input from neither a global positioning system nor an inertial navigation system to said display system, said flight condition information comprising at least flight path angle, tum rate, and lateral acceleration; and a display situated on said general aviation aircraft and signally coupled to said processor such that said display conveys said at least a portion of Appeal 2012-002214 Application 11/375,486 3 said flight condition information in such a way as to provide a pilot with a reduced cognitive workload. REFERENCES The prior art relied upon by the Examiner in rejecting the claims on appeal is: Arad US 5,103,224 Apr. 7, 1992 Katz US 2001/0039467 A1 Nov. 8, 2001 Ooga US 2002/0042673 A1 Apr. 11, 2002 Lin US 2002/0116126 A1 Aug. 22, 2002 Levine US 2003/0135327 A1 July 17, 2003. REJECTIONS Appellant seeks our review of the following rejections. I. Claims 1, 2, 5, 7-17, 19-23, and 25-28 stand rejected under 35 U.S.C. § 103(a) as unpatentable over Levine and Katz.1 II. Claim 18 stands rejected under 35 U.S.C. § 103(a) as unpatentable over Levine, Katz, and Arad. III. Claims 3, 4, and 24 stand rejected under 35 U.S.C. § 103(a) as unpatentable over Levine, Katz, and Lin. IV. Claim 6 stands rejected under 35 U.S.C. § 103(a) as unpatentable over Levine, Katz, and Ooga. 1 In both the Final Rejection and the Examiner’s Answer, the opening sentence of rejection I omits mention of claims 13, 14, 16, and 17. Fin. Rej. 3; Ans. 5. The body of rejection I, however, discusses these claims in detail. Fin. Rej. 12-14; Ans. 14-16. Accordingly, we consider these claims subject to rejection I. Appeal 2012-002214 Application 11/375,486 4 ANALYSIS Rejection I Appellant argues the Examiner has not established that the “GPS-free or INS-free operational aspects of the present invention” would have been obvious. App. Br. 4-6; Reply Br. 2-5. Appellant indicates that claim 1 captures such an operational aspect in the language “said processor operates on said collected flight data to generate at least a portion of said flight condition information with need for input from neither a global positioning system nor an inertial navigation system to said display system.” See App. Br. 5. The Examiner finds that Levine does not disclose this limitation of claim 1, but that Levine’s backup display system meets the other limitations of claim 1. Ans. 5-6. Additionally, the Examiner finds that Katz discloses a processor that generates flight condition information with information from an inclined turn rate sensor and a pitch level sensor, and that Katz says nothing about using information from a global positioning system or an inertial navigation system. Id. at 6. The Examiner finds that it would have been within the level of ordinary skill in the art to apply the approach disclosed with Katz’s processor in Levine’s system. And the Examiner concludes that it would have been obvious to do so. Id. Appellant argues that Levine and Katz teach away and therefore do not support the Examiner’s conclusion of obviousness. App. Br. 5-6. Appellant argues that Levine unequivocally discloses using GPS and INS information in its backup display system. Id. at 5. With respect to Katz, Appellant asserts that one could interpret Katz’s silence regarding GPS and INS as either disavowing or not disavowing Levine’s use of GPS and INS. Appeal 2012-002214 Application 11/375,486 5 Id. at 5-6. If one interprets Katz as disavowing GPS and INS, Appellant argues, the rejection constitutes an excellent example of a prohibited combination of disclosures that teach away because one disavows the approach used by the other. Id. at 5. If one interprets Katz as not disavowing GPS and INS, Appellant argues, “the proposed combination would, in toto, continue to teach away from all of the independent claims that expressly exclude a GPS or INS.” Id. at 6. As Appellant notes (Id. at 5-6), a reference teaches away from a claimed invention if “a person of ordinary skill, upon reading the reference, would be discouraged from following the path set out in the reference, or would be led in a direction divergent from the path that was taken by the applicant.” In re Kubin, 561 F.3d 1351, 1357 (Fed. Cir. 2009) (citing In re Gurley, 27 F.3d 551, 553 (Fed. Cir. 1994)). Under this test, Appellant’s arguments do not convince us that the cited references teach away from the claimed invention. Appellant provides no support for the speculation that one might interpret Katz as disavowing the approach disclosed by Levine. Nor does Appellant present any evidence that either reference suggests anything negative about operating a backup display system without using INS or GPS information. Indeed, Appellant provides no evidence or reasoning to convince us that the differences between the disclosures of Levine and Katz amount to anything other than disclosures of alternative approaches for a processor to generate flight condition information in a backup display system. Without more, the fact that Levine and Katz disclose alternative approaches does not convince us that reading Levine and Katz would have discouraged or led a Appeal 2012-002214 Application 11/375,486 6 person of ordinary skill in the art away from any approach for generating flight condition information, including Appellant’s claimed approach. Appellant and the Examiner also dispute whether Levine’s system generates flight condition information without need for GPS or INS information. Reply Br. 2-5. Because Appellant does not convince us of error in the Examiner’s determination that it would have been obvious in view of Katz to modify Levine generate flight condition information without need for GPS or INS information, Appellant’s arguments that Levine itself does not disclose such an approach do not apprise us of error in the conclusion of obviousness. For the foregoing reasons, Appellant’s arguments do not apprise us of error in the rejection of claim 1. Appellant does not present separate arguments for claims 2, 5, 7-17, 19-23, and 25-28. Accordingly, we sustain rejection I Rejection II Appellant traverses the rejection of claim 18 by referring to the arguments advanced against the rejection of claim 1. App. Br. 6. For the reasons discussed above, these arguments do not apprise us of error in the rejection. Accordingly, we sustain rejection II. Rejection III Appellant argues claims 3, 4, and 24 as a group. See App. Br. 6-7. We select claim 3 as representative. Claims 4 and 24 stand or fall with representative claim 3. Appeal 2012-002214 Application 11/375,486 7 Appellant argues that Lin discloses using GPS in its system. Id. Accordingly, Appellant argues, “there is nothing in Lin that rectifies the inability to combine Levine and Katz.” Id. As discussed above, Appellant’s arguments regarding claim 1 do not convince us of any error in the Examiner’s reasoning that it would have been obvious to combine the disclosures of Levine and Katz, as Appellant does not convince us that the references teach away from the claimed invention. For substantially the same reasons, the mere fact that Lin discloses an approach that involves GPS does not convince us that Lin teaches away from the claimed invention. Accordingly, we sustain rejection III. Rejection IV Appellant traverses the rejection of claim 6 by referring to the arguments advanced against the rejection of claim 1. App. Br. 7. For the reasons discussed above, these arguments do not apprise us of error in the rejection. Accordingly, we sustain rejection IV. DECISION We affirm the Examiner’s decision rejecting claims 1-28. No time period for taking any subsequent action in connection with this appeal may be extended under 37 C.F.R. § 1.136(a)(1)(iv). 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