Ex Parte Martin et alDownload PDFPatent Trial and Appeal BoardSep 26, 201713264721 (P.T.A.B. Sep. 26, 2017) 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. 13/264,721 01/25/2012 James D. Martin AG100572 3469 116439 7590 Joel G. Landau Aerojet Rocketdyne P.O. Box 7922 RLB70 Canoga Park, CA 91304 09/28/2017 EXAMINER MCDONOUGH, JAMES E ART UNIT PAPER NUMBER 1734 NOTIFICATION DATE DELIVERY MODE 09/28/2017 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): joel.landau@rocket.com nicole.holieway@rocket.com PTOL-90A (Rev. 04/07) UNITED STATES PATENT AND TRADEMARK OFFICE BEFORE THE PATENT TRIAL AND APPEAL BOARD Ex parte JAMES D. MARTIN, EDWARD O. HOSEY, and SCOTT K. DAWLEY Appeal 2016-005425 Application 13/264,721 Technology Center 1700 Before CATHERINE Q. TIMM, JAMES C. HOUSEL, and CHRISTOPHER L. OGDEN, Administrative Patent Judges. HOUSEL, Administrative Patent Judge. DECISION ON APPEAL1 1 Our decision refers to the Specification (Spec.) filed October 14, 2011, the Examiner’s Final Office Action (Final Act.) dated January 23, 2015, Appellants’ Appeal Brief (Appeal Br.) filed October 8, 2015, the Examiner’ Answer (Ans.) dated March 4, 2016, and Appellants’ Reply Brief (Reply Br.) filed April 25, 2016. Appeal 2016-005425 Application 13/264,721 Pursuant to 35 U.S.C. § 134(a), Appellants2 appeal from the Examiner’s decision finally rejecting claims 1, 5, 8, 14, and 16.3 We have jurisdiction over the appeal under 35 U.S.C. § 6(b). We AFFIRM. STATEMENT OF THE CASE The invention relates to energetic compositions and formulations to control the sensitivity of the compositions to shock. Spec. 12. Appellants disclose that a prominent cause of unintentional detonation of explosive and energetic compositions is their high sensitivity to physical shock. Id. ^ 3. Appellants further disclose that prominent energetic compounds, cyclic nitramines, can be desensitized by the addition of linear nitramine additives without loss of energy. Id. 1 5. Claim 1, reproduced below from the Claims Appendix to the Appeal Brief, is illustrative of the subject matter on appeal. 1. A low-sensitivity propellant formulation comprising a cyclic nitramine and a linear nitramine, wherein said linear nitramine is a solid energetic material having a melting point within a range of 50°C to 150°C and has the formula 2 According to Appellants, the real party in interest is Aerojet Rocketdyne, Inc., a wholly-owned subsidiary of Aerojet Rocketdyne Holdings, Inc. Appeal Br. 2. 3 Pending claims 7, 9, 10, 12, 13, 15, 17, and 18 have been withdrawn from consideration and are not before us on appeal. Final Act. 1. In addition, pending claims 6 and 11 are objected to only and are also not before us on appeal. Id. at 5. 2 Appeal 2016-005425 Application 13/264,721 R NO,!j$ i •n—4 m r i~CH2€K N(>3 tt wherein: m is zero or 1; n is 1 or 2; R1 is a member selected from the group consisting of Ci— C6 alkyl, nitrato, azido, nitrato-Ci-C6 alkyl, and azido-Ci-C6 alkyl; and R2 is a member selected from the group consisting of Ci— C6 alkyl, nitrato, azido, nitrato-(Ci-C6 alkyl) and azido-(Ci-C6 alkyl); such that the total number of non-terminal CH2CH2 groups is one, two, or three, and the total number of nitrato groups is one or two; and wherein said cyclic nitramine has the formula r R2 V K; () j -N, K" N' NO, P wherein: R2 is a member selected from the group consisting of CH2 and N-R4 in which R4 is a member selected from the group consisting of NO2, NO, C(0)CH3, CH2OCH3, CH2OC2H5, H, C1-C4 alkyl, and cyclohexyl; P is 1 or 2; and when p is 1, R3 is a member selected from the group consisting of NO2, NO, C(0)CH3,CH20CH3, CH2OC2H5, H, 3 Appeal 2016-005425 Application 13/264,721 C1-C4 alkyl, and cyclohexyl, and when p is 2, R3 is C1-C4 alkylene. REJECTIONS The Examiner maintains, and Appellants request our review of, the following grounds of rejection: 1. Claims 1, 5, 8, 12, and 16 under 35 U.S.C. § 102(b) as anticipated by Flanagan;4 and 2. Claims 1, 5, 14, and 16 under 35 U.S.C. § 103(a) as unpatentable over Zeigler.5 ANALYSIS Rejection 1: § 102(b) by Flanagan Appellants do not separately argue the dependent claims, but instead focus on claim 1 only. Accordingly, the dependent claims stand or fall with claim 1. The Examiner finds Flanagan anticipates each and every limitation of claim 1. Ans. 2, 4—5. Appellants argue that Flanagan does not anticipate their claims because Flanagan’s composition has a melting point approximately 100°C lower than claimed. Appeal Br. 3^4. This argument is not persuasive because claim 1 does not require the formulation have any particular melting point. Ans. 4. Instead, claim 1 requires the formulation include a “linear nitramine [that] is a solid energetic material having a melting point within a range of 50°C to 150°C.” Appeal Br., Claims App’x. In re Self, 671 F.2d 1344, 1348 (CCPA 1982) (“Many of appellant’s arguments fail from the 4 Flanagan et al., US 4,961,380, issued October 9, 1990 (“Flanagan”). 5 Zeigler, US 5,520,756, issued May 28, 1996. 4 Appeal 2016-005425 Application 13/264,721 outset because . . . they are not based on limitations appearing in the claims.”). Flanagan teaches a formulation comprising a cyclic nitramine, 1,3,5,7- tetranitrazacyclooctane (HMX), and a linear nitramine, l,5-dinitrato-3- nitrazapentane (DINA), having a melting point of 52.5°C. Ans. 2, 4; Flanagan 1:30-37, Table 1. As the Examiner finds (Ans. 2), Appellants teach that DINA is a specific example of a linear nitramine within the claimed linear nitramine formula. Spec. 118. Further, Appellants disclose that HMX is a well-known example of a cyclic nitramine within the scope of the claimed cyclic nitramine formula. Spec. 113. Appellants state that they have consistently argued that Flanagan does not disclose a linear nitramine that is a solid energetic material having a melting point within a range of 50°C to 150°C. Reply Br. 2. However, Appellants fail to specifically address or otherwise rebut the Examiner’s finding that Flanagan teaches DINA, a linear nitramine having a melting point of 52.5°C, which is not only clearly within the range required in claim 1, but also a specific example Appellants disclose as a linear nitramine within the scope of the formula recited in claim 1. Appellants also argue that Flanagan’s linear nitramine is directed to a eutectic liquid across all operating temperatures, whereas the claimed linear nitramine is a solid. Reply Br. 2. This argument is not persuasive because Flanagan teaches that it is the propellant component of the composition that is eutectic, not the linear nitramine per se. Moreover, we discern no difference between Flanagan’s linear nitramine, DINA, and that used by Appellants, which is also DINA. “When the claimed compositions are not novel they are not rendered patentable by recitation of properties, whether or 5 Appeal 2016-005425 Application 13/264,721 not these properties are shown or suggested in the prior art.” In re Spada, 911 F.2d 705, 709 (Fed. Cir. 1990); see also, In re Papesch, 315 F.2d 381, 391 (CCPA 1963) (“From the standpoint of patent law, a compound and all of its properties are inseparable; they are one and the same thing.”). Appellants further contend that, if Flanagan’s linear nitramine would be mixed with the claimed cyclic nitramine, the Flanagan linear nitramine “would remain liquid in the mixture and not absorb into the claimed cyclic nitramine.” Reply Br. 2. According to Appellants, the resulting mixture would be a slurry and not a solid propellant having reduced sensitivity. Id. This argument is also not persuasive. To begin, we note that claim 1 does not require that the propellant formulation be a solid. We also note that claim 1 does not require that the linear nitramine absorb into the cyclic nitramine. Self supra. Notwithstanding these facts, we note that Flanagan teaches a solid propellant composition including HMX and DINA. Moreover, Appellants fail to direct our attention to any disclosure in Flanagan or other evidentiary support for this argument. A preponderance of the evidence supports the Examiner’s finding of anticipation by Flanagan. We, therefore, sustain the Examiner’s anticipation rejection. Rejection 2: § 103(a) over Zeigler Appellants do not separately argue the dependent claims, but instead focus on claim 1 only. Accordingly, the dependent claims stand or fall with claim 1. The Examiner finds Zeigler teaches a composition comprising cyclotrimethylene trinitramine (RDX) and methyl nitratoethyl nitramine. Ans. 3. The Examiner also finds Zeigler teaches use of one compound from 6 Appeal 2016-005425 Application 13/264,721 Table 1 mixed with one compound from Table 2. Id. at 6. Zeigler, Table 1, teaches three compounds including DINA having a melting point of 52.5°C as an alternative to methyl nitratoethyl nitramine. Id.; Zeigler, Table 1. The Examiner finds that although DINA is not the particularly preferred or exemplified compound from Table 1, the list of possible compounds in Table 1 is finite and DINA has a higher energy density than the other compounds which makes it desirable in energetic materials. Id. As such, the Examiner concludes that the selection of DINA for use in a propellant formulation along with HMX would have been obvious to one of ordinary skill in the art. Id. Appellants state that the rejection states that “Zeigler’s methyl nitratoethyl nitramine renders obvious [the] claimed chemical composition.” Appeal Br. 4. This statement mischaracterizes the Examiner’s rejection. It is not the methyl nitratoethyl nitramine, compound 2 in Zeigler’s Table 1, that renders obvious the composition of claim 1, but the nitratoethyl nitramine, compound 1 in Zeigler’s Table 1, which the Examiner finds is a linear nitramine within the scope of the formula in claim 1 having a melting point between 50°C and 150°C. Appellants argue that the Examiner has not established a prima facie case of obviousness. Appeal Br. 4. In particular, Appellants argue that because Zeigler requires that the first compound from Table 1 is at least partially soluble in the second compound from Table 2, the resulting two part plasticizer composition is a liquid polymer used for gelation of the matrix component. Id. Appellants assert, therefore, that both compounds of the plasticizer composition are liquid, whereas claim 1 requires a “linear 7 Appeal 2016-005425 Application 13/264,721 nitramine is a solid energetic material having a melting point within a range of 50°C to 150°C.” Id. Appellants’ argument is not persuasive. As the Examiner indicates Zeigler teaches a linear nitramine, compound 1 from Table 1 (DINA), having a melting point in the claimed range. We discern no difference between Zeigler’s compound 1 (DINA) and that used by Appellants, which is also DINA. As such, Zeigler’s compound 1 is a solid energetic material. Papesch, 315 F.2d at 391. Though Zeigler dissolves compound 1 into compound 2, claim 1 does not exclude such dissolution and Appellants have not shown that the linear nitramine is a different compound in solution, or more germane, in the final propellant formulation when mixed with HMX. A preponderance of the evidence supports the Examiner’s findings and conclusion of obviousness over Zeigler. We, therefore, sustain the Examiner’s obviousness rejection. DECISION Upon consideration of the record, and for the reasons given above and in the Examiner’s Answer, the decision of the Examiner rejecting claims 1, 5, 8, 12, 14, and 16 is affirmed. 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). AFFIRMED 8 Copy with citationCopy as parenthetical citation