Ex Parte McIver et alDownload PDFPatent Trial and Appeal BoardJun 28, 201612961123 (P.T.A.B. Jun. 28, 2016) Copy Citation UNITED STA TES p A TENT AND TRADEMARK OFFICE APPLICATION NO. FILING DATE 12/961, 123 12/06/2010 63759 7590 06/30/2016 DUKEW, YEE YEE & AS SOCIA TES, P.C. P.O. BOX 802333 DALLAS, TX 75380 FIRST NAMED INVENTOR Keith L. Mclver 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. 10-0472-US-NP 8589 EXAMINER KONG, SZE-HON ART UNIT PAPER NUMBER 3661 NOTIFICATION DATE DELIVERY MODE 06/30/2016 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): ptonotifs@yeeiplaw.com mgamez@yeeiplaw.com patentadmin@boeing.com PTOL-90A (Rev. 04/07) UNITED STATES PATENT AND TRADEMARK OFFICE BEFORE THE PATENT TRIAL AND APPEAL BOARD Ex parte KEITH L. MCIVER, RUSSELL LEE KELLER, CONG NGHIEP DUONG, NICOLETTE P. YOVANOF, MYLES LEONARD BAKER, SCOTT MICHAEL YOUNG, KEVIN MICHAEL ROUGHEN, and KELLY M. GREENE Appeal2014-001744 1 Application 12/961,123 2 Technology Center 3600 Before BIBHU R. MOHANTY, ROBERT L. KINDER, and TARA L. HUTCHINGS, Administrative Patent Judges. HUTCHINGS, Administrative Patent Judge. DECISION ON APPEAL STATEMENT OF THE CASE Appellants appeal under 35 U.S.C. § 134(a) from the Examiner's final rejection of claims 1-8 and 10-20. We have jurisdiction under 35 U.S.C. § 6(b ). We REVERSE. 1 Our decision references Appellants' Appeal Brief ("App. Br.," filed July 31, 2013) and Reply Brief ("Reply Br.," filed Nov. 12, 2013), and the Examiner's Answer ("Ans.," mailed Sept. 27, 2013) and Final Office Action ("Final Act.," mailed May 1, 2013). 2 Appellants identify The Boeing Company as the real party in interest. App. Br. 2. Appeal2014-001744 Application 12/961, 123 CLAIMED fNVENTION Appellants' claimed invention "relates generally to maintenance and particularly to systems and methods for determining rework plans that address inconsistencies in vehicles such as aircraft." Spec. i-f 1. Claim 1, reproduced below, is illustrative of the subject matter on appeal: 1. A rework system for a vehicle having an inconsistency on a component of the vehicle, the rework system compnsmg: a rework assessor configured to examine a rework parameter array to ascertain whether a rework procedure is to be performed, wherein the rework parameter array defines at least volumetric dimensions of the component, a type of the inconsistency, and location coordinates of the inconsistency with respect to the component or the vehicle; [and] a rework interrogator in communication with the rework assessor, the rework interrogator configured to, when a rework is to be performed, identify a candidate for addressing the inconsistency, the candidate selected based on both an ascertainment by the rework assessor and a received input comprising a rule of thumb criteria, the candidate further selected from the group consisting of: a candidate part, a candidate rework procedure, and both the candidate part and the candidate rework procedure. REJECTIONS Claims 1-8 and 11-20 are rejected under 35 U.S.C. § 103(a) as unpatentable over Perkins (US 2009/0234616 Al, pub. Sept. 17, 2009) and Xu (US 2012/0109660 Al, pub. May 3, 2012). Claim 10 is rejected under 35 U.S.C. § 103(a) as unpatentable over Perkins, Xu, and Goebel (US 7,933,754, iss. Apr. 26, 2011). 2 Appeal2014-001744 Application 12/961, 123 ANALYSIS Independent Claim 1 and Dependent Claims 2---8 and 11-15 We are persuaded by Appellants' argument that the Examiner erred in rejecting independent claim 1 under 35 U.S.C. § 103(a) because Perkins, on which the Examiner relies, does not disclose or suggest "a rework interrogator ... configured to, when a rework is to be performed, identify a candidate for addressing the inconsistency, the candidate selected based on both an ascertainment by the rework assessor and a received input comprising a rule of thumb criteria, the candidate further selected from the group consisting of: a candidate part, a candidate rework procedure, and both the candidate part and the candidate rework procedure," as recited in claim 1. App. Br. 10-12; see also Reply Br. 7-9. The Examiner relies on Perkins as disclosing the argued limitation. Ans. 6 (citing Perkins i-fi-1 4 7, 57); see also Final Act. 5 (citing Perkins i-fi-147, 57, 100). Appellants' Specification defines "rules of thumb" as "guidelines for rework plans, rework procedures, or parts." Spec. i176. Appellants' Specification also defines "reworking" as a sub-category of maintenance that includes replacing components to address inconsistencies or to address other issues, removal of components, and other such information. Id. i-f 26. A "rework procedure" refers to a technique or series of steps used to perform a rework. Id. i132. And a "rework plan" refers to a proposed series of steps for implementing a rework, and/or one or more parts proposed to be used during the rework. Id. i133. Perkins relates to automated analysis for repair and maintenance of composite aircraft parts. Id. i12. Perkins describes that the basic chemistry of composite materials obviates the validity of "rules of thumb" as a way to 3 Appeal2014-001744 Application 12/961, 123 determine that a repaired part will satisfactory provide the same form, fit, and function as the original composite part. Id. i-f 3. As a result, Perkins provides an automatic repair planning and part archival system ("ARPP AS") that supports the need for individual part analysis and the need for a comprehensive database of aircraft parts damaged. Id. i-fi-110, 37. In operation, a user selects an aircraft part from a list of available parts, and a view of an area of the selected part to be analyzed for repair. Id. i-fi-142--43. ARPPAS posts an engineering drawing of the selected part view and displays the part's previous repairs. Id. i-fi-143, 100. The user enters repair area geometry, which ARPPAS transforms into a digitized part structural model coordinate system. Id. i-fi-1 44, 46. The user selects a solver associated with an engineering analysis subroutine from among several options. Id. i-f 47. ARPPAS records analysis process information and engineering reference data as a new record unique for that part ID and repair instance. Id. i-fi-147, 100. Information is submitted to the selected solver for analysis, ARPP AS assembles additional data needed to execute the analysis. Id. i-f 48. ARPPAS provides the user with the option to select an alternative solver, and can support a multiplicity of such analysis by encapsulating the unique requirements of each analysis type's data file formats. Id. i-f 51. ARPP AS compares the engineering analysis results with approved values obtained from structural analysis programs used as acceptance criteria. Id. ,-r 57. There is no question that Perkins discloses a tool to perform an analysis on a particular composite aircraft part and archive any repairs made. But we find nothing in the cited portions of Perkins that discloses or suggests that a rework interrogator identifies a candidate for addressing the 4 Appeal2014-001744 Application 12/961, 123 inconsistency based on both an ascertainment by the rework assessor and a received input comprising a rule of thumb criteria, as recited in claim 1. For example, we fail to see, and the Examiner does not adequately explain, how Perkins teaches a rework interrogator receiving a rule of thumb criteria as input, let alone the rework interrogator selecting a candidate based on an ascertainment by the rework assessor and a received input comprising a rule of thumb criteria. Rather, Perkins' ARPP AS performs engineering analysis based on data input by a user and a solver associated with an engineering analysis subroutine selected by the user, and compares the results of the analysis with acceptable data stored by the selected engineering analysis program. In view of the foregoing, we do not sustain the Examiner's rejection of independent claim 1 and dependent claims 2-8 and 11-15 under 3 5 U.S.C. § 103(a). Independent Claim 16 and Dependent Claims 17-20 Independent claim 16 recites language substantially similar to the language of claim 1 and stands rejected based on the same rationale applied with respect to claim 1. Therefore, we do not sustain the Examiner's rejection of independent claim 16 and dependent claims 17-20 under 35 U.S.C. § 103(a) for the same reasons set forth above with respect to claim 1. Dependent Claim 10 Claim 10 depends from claim 1. The Examiner's rejection of claim 10 does not cure the deficiency in the Examiner's rejection of claim 1, discussed above. Therefore, we do not sustain the rejection of claim 10 under 35 U.S.C. § 103(a) for the same reasons set forth above with respect to claim 1. 5 Appeal2014-001744 Application 12/961, 123 DECISION The Examiner's rejections of claims 1-8 and 10-20 under 35 U.S.C. § 103(a) are reversed. REVERSED 6 Copy with citationCopy as parenthetical citation