Ex Parte Tozzi et alDownload PDFPatent Trial and Appeal BoardJun 28, 201814020770 (P.T.A.B. Jun. 28, 2018) Copy Citation UNITED STA TES p A TENT AND TRADEMARK OFFICE APPLICATION NO. FILING DATE 14/020,770 09/06/2013 68368 7590 07/02/2018 Barcelo, Harrison & Walker, LLP 2901 W. Coast Hwy Suite 200 Newport Beach, CA 92663 FIRST NAMED INVENTOR Luigi P. Tozzi 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. PR0-0002-P 5922 EXAMINER GIMIE, MAHMOUD ART UNIT PAPER NUMBER 3747 NOTIFICATION DATE DELIVERY MODE 07/02/2018 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): rey@bhiplaw.com josh@bhiplaw.com dwalker@bhiplaw.com PTOL-90A (Rev. 04/07) UNITED STATES PATENT AND TRADEMARK OFFICE BEFORE THE PATENT TRIAL AND APPEAL BOARD Exparte LUIGI P. TOZZI, MARIA EMMANUELLA SOTIROPOULOU, and DAVID THOMAS LEPLEY1 Appeal2017-005703 Application 14/020, 770 Technology Center 3700 Before MICHELLE R. OSINSKI, JILL D. HILL, and NATHAN A. ENGELS, Administrative Patent Judges. OSINSKI, Administrative Patent Judge. DECISION ON APPEAL STATEMENT OF THE CASE Appellant appeals under 35 U.S.C. § 134(a) from the Examiner's decision rejecting claims 1--47, which are all of the pending claims. We have jurisdiction under 35 U.S.C. § 6(b ). We AFFIRM-IN-PART. 1 Prometheus Applied Technologies, LLC ("Appellant") is the Applicant as provided in 37 C.F.R. § 1.46, and is identified as the real party in interest. Appeal Br. 2. Appeal2017-005703 Application 14/020, 770 THE CLAIMED SUBJECT MATTER Claims 1, 11, 21, 31, 41, and 43 are independent. Claim 1, reproduced below, is illustrative of the claimed subject matter on appeal. l. A two-stage precombustion chamber comprising: a first prechamber stage enclosing a first prechamber volume, the first prechamber stage comprising: one or more first stage holes communicatimr ~- ~~ between the first prechamber volume and a second prechamber volume; a primary electrode disposed within the first prechamber volume; and one or more ground electrodes disposed within the first prechamber volume and offset from the primary electrode to form one or more electrode gaps; and a second prechamber stage enclosing the second prechamber volume, the second prechamber stage comprising: one or more second stage hoks communicating ~ 0 between the second prechamber volume and a combustion chamber volume. EVIDENCE The Examiner relied on the following evidence in rejecting the claims on appeal: Genslak Crane us 4,124,000 us 5,222,993 THE REJECTIONS 2 Nov. 7, 1978 June 29, 1993 I. Claims 1-7, 9-17, 19-24, 26-34, and 36-40 stand rejected under 35 U.S.C. § 102(b) as anticipated by Crane. Final Act. 3-10. 2 The rejection of claims 1-7, 9-17, 19-24, 26-34, and 36-40 under 35 U.S.C. § 102(b) as anticipated by Genslak (Final Act. 3) has been withdrawn and is not before us on appeal (Ans. 12). 2 Appeal2017-005703 Application 14/020, 770 II. Claims 8, 18, 25, and 35 stand rejected under 35 U.S.C. § 103(a) as unpatentable over Crane. Id. at 12-13. III. Claims 41--47 stand rejected under 35 U.S.C. § 102(b) as anticipated by Genslak. Id. at 10-11. OPINION Rejection I Claims 1, 11, 21, and 31 Appellant argues independent claims 1, 11, 21, and 31 as a group. Appeal Br. 8. We select claim 1 as the representative claim, and claims 11, 21, and 31 stand or fall therewith. 37 C.F.R. § 4I.37(c)(l)(iv). The Examiner finds that Crane discloses all of the limitations of independent claim 1. Final Act. 4. In particular, the Examiner points to Crane's second precombustion chamber 54 as the claimed "first prechamber stage enclosing a first prechamber volume" and Crane's first precombustion chamber 50 as the claimed "second prechamber stage enclosing [a] second prechamber volume." Id. Appellant argues that "Crane at most discloses two pre-combustion chambers, serially arranged" which is a "configuration [that] is fundamentally different than the claimed single two-stage precombustion chamber in the fact that with a single, two-stage precombustion chamber a perfectly consistent flow dynamic can be achieved throughout the two- stages," whereas "two separate precombustion chambers, serially arranged, ... result in ... the inconsistent flow dynamic between the first prechamber and the second prechamber." Appeal Br. 8. To the extent Appellant is arguing that two serially arranged pre- combustion chambers cannot constitute a two-stage precombustion chamber, 3 Appeal2017-005703 Application 14/020, 770 Appellants have not adequately explained how the collective plurality of serially arranged precombustion chambers 50, 54 fails to meet all the requirements of the claimed two-stage precombustion chamber. To the extent Appellant is arguing that Crane fails to disclose a two-stage precombustion chamber that achieves a perfectly consistent flow dynamic throughout the two stages (Appeal Br. 8), this argument is not persuasive because it is not based on a limitation that actually appears in the claim. Arguments must be commensurate in scope with the actual claim language. In re Self, 671 F.2d 1344, 1348 (CCPA 1982). For the foregoing reasons, Appellant does not show error by the Examiner in finding that claim 1 is anticipated by Crane. We sustain the rejection of claim 1, and claims 11, 21, and 31 falling therewith, under 3 5 U.S.C. § 102(b) as anticipated by Crane. Claims 2--4, 12-14, 26--28, and 36--38 Appellant argues independent claims 2--4, 12-14, 26-28, and 36-38 as a group. Appeal Br. 9. We select claim 2 as the representative claim, and claims 3, 4, 12-14, 26-28, and 36-38 stand or fall therewith. Claim 2 recites that "a first fuel concentration in the first prechamber volume is higher than a second fuel concentration in the second prechamber volume." Appeal Br. 18 (Claims App.). The Examiner finds that, in Crane, "a first fuel concentration (rich air/fuel mixture) in the first prechamber volume (54) is higher than a second fuel concentration in the second prechamber volume (50)." Final Act. 4. Appellant argues that "the actual teaching of Crane refers at most to a relatively fuel rich concentration in the second prechamber relative to a leaner fuel/air mixture in the main chamber." Appeal Br. 9 ( citing Crane Abstract). The Examiner responds 4 Appeal2017-005703 Application 14/020, 770 that "Crane refers to prechamber 54 as a second prechamber instead of first prechamber [ which is how the Examiner has identified prechamber 54]." Ans. 13. We agree with the Examiner that Crane teaches that the fuel concentration in the first prechamber as identified by the Examiner (i.e., Crane's second precombustion chamber 54) is relatively rich and the fuel concentration in the second prechamber as identified by the Examiner (i.e., Crane's first precombustion chamber 50) is relatively lean. Id. For the foregoing reasons, Appellant does not show error by the Examiner in finding that claim 2 is anticipated by Crane. We sustain the rejection of claim 2, and claims 3, 4, 12-14, 26-28, and 36-38 falling therewith, under 35 U.S.C. § 102(b) as anticipated by Crane. Claims 9, 10, 19, 20, 29, 30, 39, and 40 Claims 9, 19, 29, and 39 recite that the "one or more first stage holes [ communicating between the first and second prechamber volumes] defines a first stage hole axis ... [that] defines an index angle, a penetration angle and a rotational offset" and that "the one or more second stage holes [ communicating between the second prechamber volume and the combustion chamber volume] defines a second stage hole axis ... [that] defines an index angle, a penetration angle and a rotational offset." Appeal Br. 19, 20, 22, 24 (Claims App.). Claims 10, 20, 30, and 40 depend therefrom, respectively, and recite that "the index angle, the penetration angle and the rotational offset of the first stage holes and the second stage holes are selected to generate a first fuel concentration in the first prechamber volume that is higher than a second fuel concentration in the second prechamber volume." Id. at 19, 21, 22, 24. The Specification describes how the penetration angle, index angle, and rotational offset may 5 Appeal2017-005703 Application 14/020, 770 be defined (Spec. 16:7-15) and indicates that they "may be selected to generate a first fuel concentration in the first prechamber 110 stage that is higher than a second fuel concentration in the second prechamber stage 120" (id. at 14: 16-20). The penetration angle is "defined as the angle between the plane perpendicular to the axis ... of the prechamber spark plug and the centerline of the port/hole." Id. at 16:7-9. The index angle is "defined as the angle of rotation about the axis ... of the prechamber spark plug and the location on the port where the centerline of the port meets the front plane of the prechamber spark plug." Id. at 16: 10-12. The rotational offset is "defined as the perpendicular distance between the axis ... of the prechamber spark plug and the centerline of the port/hole (measured on the plane at the front of the prechamber spark plug." Id. at 16:13-15. We do not discern where the Specification provide details regarding any specific values for these parameters. The Examiner finds that Crane discloses the subject matter of claims 9, 10, 19, 20, 29, 30, 39, and 40. Final Act. 5, 6, 8, and 9-10. Because (i) the Examiner has made findings regarding Crane disclosing first stage holes 56 and second stage holes 52, each of the holes defining axes (Final Act. 5), (ii) the index angle, penetration angle, and rotational offset are defined by relationships between the location of the holes and the location of a spark plug (Spec. 16:7-15); and (iii) Crane includes a spark plug 38 (Crane Fig.), we consider the Examiner to have reasonably supported that the axes of the holes 56, 52 necessarily define an index angle, penetration angle, and rotational offset. In addition, we consider the Examiner to have reasonably supported that the index angle, penetration angle, and rotational offset necessarily generate a first fuel concentration in the first prechamber volume 6 Appeal2017-005703 Application 14/020, 770 that is higher than a second fuel concentration in the second prechamber volume because the Examiner has made findings that, in Crane, the fuel concentration in the first prechamber volume is higher than the second prechamber volume (Final Act. 4),. Appellant argues that "Crane provides no disclosure, expressly or inherently[,] of the claimed axes and angles, much less selecting those axes and angles to generate a first fuel concentration in the first prechamber volume that is higher than a second fuel concentration in the second prechamber volume." Appeal Br. 10. Appellant's argument appears to focus on whether Crane explicitly describes the claimed axes/angles and the selection of those axes/angles to achieve a certain fuel concentration relationship. However, the relevant inquiry is whether the structure of Crane necessarily has these claimed axes/angles and achieves a certain claimed fuel concentration relationship, not whether Crane acknowledges this. See, e.g., Toro Co. v. Deere & Co., 355 F.3d 1313, 1321 (Fed. Cir. 2004)("[T]he fact that a characteristic is a necessary feature or result of a prior-art embodiment (that is itself sufficiently described and enabled) is enough for inherent anticipation, even if that fact was unknown at the time of the prior invention."). Where the Patent Office has reason to believe that a functional limitation asserted to be critical for establishing novelty in the claimed subject matter may, in fact, be an inherent characteristic of the prior art, it possesses the authority to require the applicant to prove that the subject matter shown to be in the prior art does not possess the characteristic relied on. See In re Spada, 911 F.2d 705, 708 (Fed. Cir. 1990) ("when the PTO shows sound basis for believing that the products of the applicant and the prior art are the same, the applicant has the burden of showing that they are 7 Appeal2017-005703 Application 14/020, 770 not"); In re Best, 562 F.2d 1252, 1254--55 (CCPA 1977). Appellant's argument does not tend to refute the Examiner's finding that the structure of Crane has the claimed axes/angles and achieves a certain claimed fuel concentration relationship (Final Act. 4--5), just like the claimed structure. For the foregoing reasons, Appellant does not show error by the Examiner in finding that claims 9, 10, 19, 20, 29, 30, 39, and 40 are anticipated by Crane. We sustain the rejection of claims 9, 10, 19, 20, 29, 30, 39, and 40 under 35 U.S.C. § 102(b) as anticipated by Crane. Rejection II Claims 8 and 18 recite that the two-stage precombustion chamber "further compris[ es] a fuel admission point configured to admit fuel into the second prechamber volume." Appeal Br. 19, 20 (Claims App.). Claims 25 and 3 5 recite that "the one or more fuel admission points is introduced into the second prechamber volume." Id. at 22, 24. Although the Examiner finds that Crane discloses "a fuel admission point ( 60) configured to admit fuel into the first prechamber volume [54]" (Final Act. 5), the Examiner finds that Crane "is silent as to admitting fuel into the second prechamber volume" (id. at 12). The Examiner concludes that "[i]t would have been an obvious matter of design choice to admit fuel into the second prechamber instead of the first prechamber on the basis of its suitability for the intended purpose." Id. at 13. Appellant argues that admitting fuel into the second prechamber instead of the first prechamber would "caus[ e] the engine to misfire or result in very unstable combustion" because "fuel [ needs to be] injected in the volume where the spark plug is located" and "in Crane, the spark plug is located in the first prechamber and there is no suitable flow dynamic 8 Appeal2017-005703 Application 14/020, 770 claimed that would make the fuel injected in the second prechamber to somehow migrate to the first prechamber to make the first prechamber richer than the second prechamber which is required for proper engine combustion operation." Appeal Br. 15-16. We find Appellant's argument persuasive as to why it would not be obvious as a matter of design choice to admit fuel into the second prechamber instead of the first prechamber. The Examiner takes an alternative position in the Answer that: Crane illustrates a main combustion chamber ( 18) connected to the second prechamber (50) through orifice (52) to admit air-fuel mixture to the second precombustion chamber through orifice (52) during compression stroke of the engine. Therefore, fuel is admitted into the second prechamber chamber as claimed at least during the compression stroke of the engine. Ans. 15. Appellant argues that the Examiner provides no adequate explanation as to how orifice 52 can satisfy both the limitation of "one or more second stage holes" and the limitation of a "fuel admission point." Reply Br. 11. Moreover, Appellant argues that Crane discloses "that it is 'the fuel/air mixture supplied into combustion chamber 22 that is forced into precombustion chamber 50,' ... , and therefore is not a fuel admission point as claimed." Id. (citing Crane 4:8-12). The Specification describes the "fuel admission point" as a separate fuel line that directly fuels the first or second prechamber stage (see, e.g., Spec. 13:8-14) and is different than (i.e., in addition to) first and second stage holes (see, e.g., id. at 8:11-12). The Examiner has not shown where Crane discloses a separate element, different from the second stage holes, through which fuel enters the second prechamber volume. We agree with Appellants that the Examiner has not supported by a preponderance of the evidence that Crane discloses "a fuel admission point configured to admit fuel into [a] second prechamber 9 Appeal2017-005703 Application 14/020, 770 volume" or that "the one or more fuel admission points is introduced into the second prechamber volume," as claimed. For the foregoing reasons, Appellant shows error by the Examiner in determining that the subject matter of claims 8, 18, 25, and 35 is unpatentable over Crane. We do not sustain the rejection of claims 8, 18, 25, 35 under 35 U.S.C. § 103(a) as unpatentable over Crane. Rejection III Claim 41 Claim 41 recites: A method for controlling the admission of fuel to a two-stage precombustion chamber utilizing an electrically actuated valve, comprising adjusting a quantity of fuel admitted and timing of admitting the quantity of fuel relative to engine position to achieve a desired fuel distribution in the two-state precombustion chamber. Appeal Br. 24 (Claims App.). The Examiner finds that Genslak discloses all of the limitations of independent claim 41. Final Act. 10. Appellant argues that "Genslak discloses two pre-combustion chambers, serially arranged," rather than a two-stage precombustion chamber. Appeal Br. 11. For the reasons described supra in connection with Rejection I, we do not find this argument persuasive of error by the Examiner. As to the Examiner's finding that Genslak discloses "utilizing an electrically actuated valve (fuel valve 38 or 78; controlled much the same manner as occurs in diesel engine, col. 3 and 63---68)" (Final Act. 10), Appellant argues that the differences between the diffusive combustion process that occurs in a diesel engine and the pre-mixed combustion process of the present application create different requirements for the fuel injection strategies, and thus, Genslak does not disclose the limitations of claim 41. 10 Appeal2017-005703 Application 14/020, 770 Appeal Br. 12. This argument is not persuasive in that the referenced feature (e.g., specific fuel injection strategies that are designed for a pre-mixed combustion process) does not actually appear in the claim and so the argument is not commensurate with the actual claim language. Appellant does not adequately identify how Genslak fails to disclose the claimed method. For the foregoing reasons, Appellant does not show error by the Examiner in finding that claim 1 is anticipated by Genslak. We sustain the rejection of claim 41 under 35 U.S.C. § 102(b) as anticipated by Genslak. Claims 42--47 As to claims 42--47, the Examiner finds that Genslak discloses all of the limitations of these claims. Final Act. 10-11. Appellant argues that the Examiner points to nothing in Genslak that explicitly or inherently discloses these additional limitations. Appeal Br. 12- 15. 3 Although we appreciate the breadth of these claims, this does not relieve the Examiner of providing a sufficiently informative rejection that allows Appellant to recognize and counter the grounds of rejection. The Examiner does not provide any indication of where in Genslak the claimed features are disclosed ( e.g., by citation to column/line number or by identifying any particular elements by 3 For example, with respect to claims 42 and 44, Appellant argues that Genslak does not disclose any sort of feedback loop. Appeal Br. 12, 13. With respect to claim 43, Appellant argues that Genslak does not disclose the characteristics of the spark discharge event. Id. at 13. With respect to claims 45 and 4 7, Appellant argues that Genslak does not disclose providing cooling to the first and second stage prechambers. Id. at 14. With respect to claim 46, Appellant argues that Genslak does not disclose a passive prechamber spark plug with a specific heat range. Id. at 14--15. 11 Appeal2017-005703 Application 14/020, 770 reference number). The Examiner provides no clarification in the Answer. Accordingly, the Examiner's rejection "is so uninformative that it prevents the applicant from recognizing and seeking to counter the grounds of rejection," and thus fails to provide sufficient notice under 35 U.S.C. § 132, thereby failing to satisfy the initial burden of establishing a prima facie case of anticipation. See In re Jung, 637 F.3d 1356, 1362 (Fed. Cir. 2011) (quoting Chester v. Miller, 906 F.2d 1574, 1578 (Fed. Cir. 1990)). For the foregoing reasons, we do not sustain the rejection of claims 42--47 under 35 U.S.C. § 102(b) as anticipated by Genslak. DECISION The Examiner's decision to reject claims 1-7, 9-17, 19-24, 26-34, and 36-40 under 35 U.S.C. § 102(b) as anticipated by Crane is affirmed. The Examiner's decision to reject claims 8, 18, 25, and 35 under 35 U.S.C. § 103(a) as unpatentable over Crane is reversed. The Examiner's decision to reject claim 41 under 35 U.S.C. § 102(b) as anticipated by Genslak is affirmed. The Examiner's decision to reject claims 42--47 under 35 U.S.C. § 102(b) as anticipated by Genslak is reversed. 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-IN-PART 12 Copy with citationCopy as parenthetical citation