Ex Parte Ribbe et alDownload PDFPatent Trial and Appeal BoardMar 31, 201712640540 (P.T.A.B. Mar. 31, 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. 12/640,540 12/17/2009 James A. Ribbe 08E343-US-NP 8960 18227 7590 04/04/2017 Pantnr Pnlhiirn T T P - R avthenn EXAMINER 20 Church Street 22nd Floor RODDEN, JOSHUA E Hartford, CT 06103 ART UNIT PAPER NUMBER 3649 NOTIFICATION DATE DELIVERY MODE 04/04/2017 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): US PTOPatentM ail @ cantorcolburn .com PTOL-90A (Rev. 04/07) UNITED STATES PATENT AND TRADEMARK OFFICE BEFORE THE PATENT TRIAL AND APPEAL BOARD Ex parte JAMES A. RIBBE, NASRIN AZORDEGAN, and JOHN B. MORTON Appeal 2015-005344 Application 12/640,540 Technology Center 3600 Before EDWARD A. BROWN, GEORGE R. HOSKINS, and LEE L. STEPINA, Administrative Patent Judges. BROWN, Administrative Patent Judge. DECISION ON APPEAL STATEMENT OF THE CASE James A. Ribbe et al. (Appellants) appeal under 35 U.S.C. § 134(a) from the Examiner’s decision rejecting claims 1—27.1 We have jurisdiction under 35 U.S.C. § 6(b). We AFFIRM and enter NEW GROUNDS OF REJECTION. 1 Thales-Raytheon Systems Company LLC, is identified as the real party in interest. Appeal Br. 1. Appeal 2015-005344 Application 12/640,540 INVENTION Claims 1, 10, and 19 are independent. Claim 1, reproduced below, illustrates the claimed subject matter. 1. An airspace deconfliction system comprising: a deconfliction tool comprising a computer- readable medium storing code executable by a computer processor of a computing system, the computing system coupled to a data repository storing a plurality of records that each describes an airspace object and a geographic location associated with the airspace object, the deconfliction tool operable to: determine, for at least one record representing a future route to be taken by at least two aircraft, a conflict in the geographic location associated with the one record and the geographic location associated with at least one of the other records, the conflict determined in response to a first buffer space having a predetermined shape that surrounds a first airspace object and that traverses the future route along with the first airspace object intersecting a second buffer space having the predetermined shape that surrounds a second airspace object and that traverses the future route along with the second airspace object, the first and second predetermined shapes of the first and second buffer spaces remaining constant as a position of first and second airspace objects changes while traversing the future route. Appeal Br. 13 (Claims App.). REJECTIONS 1. Claims 1—27 are rejected under 35 U.S.C. § 112, first paragraph, as failing to comply with the written description requirement. 2. Claims 1, 3, 6, 7, 10, 12, 15, 16, 19, 21, 24, and 25 are rejected under 35 U.S.C. § 103(a) as unpatentable over Wise (US 2010/0145599 Al, published June 10, 2010) and Lai (US 6,564,149 B2, issued May 13, 2003). 2 Appeal 2015-005344 Application 12/640,540 3. Claims 2, 11, and 20 are rejected under 35 U.S.C. § 103(a) as unpatentable over Wise, Lai, and Erzberger (US 6,314,362 Bl, Nov. 6, 2001). 4. Claims 4, 13, and 22 are rejected under 35 U.S.C. § 103(a) as unpatentable over Wise, Lai, and Harkness, “An Architecture for System- Wide Information Management,” 25th Digital Avionics System Conference, pp. 1—13 (Oct. 15, 2006) (hereinafter “Harkness”). 5. Claims 5, 14, and 23 are rejected under 35 U.S.C. § 103(a) as unpatentable over Wise, Lai, and Harrie et al., “Real-Time Data Generalisation and Integration using JAVA,” National Land Survey of Sweden, pp. 29-34 (2002).2 6. Claims 8, 9, 17, 18, 26, and 27 are rejected under 35 U.S.C. § 103(a) as unpatentable over Wise, Lai, and Zobell (US 2003/0078719 Al, Apr. 24, 2003). ANALYSIS Claims 1—27 as failing to comply with the written description requirement Independent claims 1,10, and 19 each recite the limitation “the first and second predetermined shapes of the first and second buffer spaces remaining constant as a position of first and second airspace objects changes while traversing the future route.” Appeal Br. 13—16 (Claims App.) (emphasis added) (hereafter “buffer shape limitation”). The Examiner determines that the original disclosure “does not describe the shape of the buffers as remaining constant along the future route.” final Act. 3. 2 We refer to this reference as “Johansson” consistent with the Examiner’s usage. 3 Appeal 2015-005344 Application 12/640,540 For the written description requirement of 35 U.S.C. § 112, first paragraph, “the test for sufficiency is whether the disclosure of the application relied upon reasonably conveys to those skilled in the art that the inventor had possession of the claimed subject matter as of the filing date.” See AriadPharm., Inc. v. EliLilly & Co., 598 F.3d 1336, 1351 (Fed. Cir. 2010) (en banc). In order to show “possession,” “the [Specification must describe an invention understandable to that skilled artisan and show that the inventor actually invented the invention claimed.'” Id. (emphasis added). “[Ujnder proper circumstances, drawings alone may provide a ‘written description’ of an invention as required by § 112.” Vas-Cath Inc. v. Mahurkar, 935 F.2d 1555, 1565 (Fed. Cir. 1991). “[I]t is well established that patent drawings do not define the precise proportions of the elements and may not be relied on to show particular sizes if the specification is completely silent on the issue.” Hockerson-Halberstadt, Inc. v. Avia Group Intern., Inc. 222 F.3d 952, 956 (Fed. Cir. 2000). Appellants contend that Figure 3 provides evidence of possession of the claimed subject matter. Reply Br. 3. Particularly, Appellants state: Turning to Figure 3 of Appellants’] originally filed application, the buffer space 40 is shown at a first time of the route tl as having a first shape and then traverses along the future route until it reaches a time t2 which is shown as having the same shape the buffer space had at time tl. Therefore, one of ordinary skill in the art could clearly evaluate that the shape of the buffer space 40 remains constant while travelling along the future route 24 between times tl and t2. Id. The Examiner determines, however, that Appellants’ drawings do not define precise proportions as they are not drawn to scale, and “one of ordinary skill would not be capable of fleshing out the words from the visual 4 Appeal 2015-005344 Application 12/640,540 representation of the drawings.” Ans. 3, 4. Specifically, the Examiner states, “it would not have been clear to one of ordinary skill in the art that the buffer spaces are in fact constant as a position of the buffer spaces traverse the future route(s) based solely upon the drawings of the current application.” Id. at 4. Appellants reply that Figure 3 is relied upon to show that the shape of the buffer space at time tl is the same as the buffer space at time t2, not to show a precise proportion, or to define precise proportions, of the buffer spaces. Reply Br. 2—3. We agree with Appellants that Figure 3 does not need to show that buffer space 40 has the same proportions at time tl and t2 to provide support for claim 1. Figure 3 shows that buffer space 40 at first time tl has a first shape (i.e., a first three-dimensional cylindrical shape) and then traverses along the future route until it reaches time t2, at which buffer space has a second shape (i.e., a second three-dimensional cylindrical shape). See Spec. 12:5—8. As shown, the second shape at time t2 is the same as the first shape at time tl. Also, Appellants’ Specification states that “[a]t time tl, no conflict exists. However, at time t2, a conflict exists wherein both buffer spaces 40 occupy the same space at the same future timer Id. at 12:12—14 (emphasis added). This description supports Appellants’ position that the original disclosure supports claim 1. Accordingly, we do not sustain the rejection of claims 1—27 under 35 U.S.C. § 112, first paragraph, written description requirement. Claims 1, 3, 6, 7, 10, 12, 15, 16, 19, 21, 24, and 25 as unpatentable over Wise and Lai Appellants present argument for the patentability of claims 1,10, and 19 as a group, and do not present separate argument for dependent claims 3, 5 Appeal 2015-005344 Application 12/640,540 6, 7, 12, 15, 16, 21, 24, and 25. Appeal Br. 8—11. We select claim 1 to decide the appeal as to the rejection, with claims 3, 6, 7, 10, 12, 15, 16, 19, 21, 24, and 25 standing or falling with claim 1. See 37 C.F.R. § 41.37(c)(l)(iv). As to claim 1, the Examiner finds that Wise discloses all limitations except for the buffer shape limitation. Final Act. 4—5. The Examiner finds that Wise discloses a first airspace object (aircraft 302), a second airspace object (aircraft 308), a first buffer space (predicted protected airspace 306), and a second buffer space (predicted protected airspace 312). Id. at 4. The Examiner finds that Lai teaches that the shape of buffer space 250 remains constant as a position of an airspace object changes while traversing the future route. Id. at 5 (citing Lai, col. 12,11. 11—54, Figs. 1—4); see also Ans. 8. The Examiner concludes that it would have been obvious to modify the system of Wise to have the buffer shape limitation, as taught by Lai, “for the purpose[] of having the buffers shapes being constant when sensors aren’t available to more accurately display a shape of the buffer shapes.” Final Act. 5. Figures 3 and 4 of Wise show current and future separation distances of first aircraft 302 and nearby second aircraft 308. Wise Tflf 30, 32, Figs. 3, 4. First aircraft 302 has projected flight trajectory 304 and second aircraft 308 has projected flight trajectory 310. Id. 132, Figs. 3, 4. An indicator of a predicted protected air space 306 is displayed ahead of first aircraft 302 and an indicator of a predicted protected air space 312 is displayed ahead of aircraft 308. Id. Tflf 32—33, Figs. 3, 4. Figure 4 of Wise “indicates an area of overlap 320 in the predicted protected airspaces 306, 312 projected for the first aircraft 302 and 308.” Id. 134, Fig. 4. 6 Appeal 2015-005344 Application 12/640,540 Appellants contend that in Wise, predicted protected air spaces 306/312 are not surrounding aircrafts 302/308 and do not travel with aircrafts 302/308 along routes 304/310. Appeal Br. 10. Appellants point out that Wise discloses that predicted protection spaces 306/312 are displayed ahead of aircrafts 302/308. Id. Appellants contend that these figures show first aircraft 302 and second aircraft 308 at first positions outside of estimated predicted protection airspaces 306/312 at a first time period, and then within estimated predicted protection airspaces 306/312 at a later point in time. Id. Appellants add that Wise states that the vertical display of Figures 3 and 4 shows “aircraft 308 approaching a fixed predicted protected] airspace 312 located at an ‘arrival phase of the flight.’” Id. Therefore, Appellants submit, Wise does not teach or suggest the limitation [determine] ... a conflict... in response to a first buffer space having a predetermined shape that surrounds a first airspace object and that traverses the future route along with the first airspace object intersecting a second buffer space having the predetermined shape that surrounds a second airspace object and that traverses the future route along with the second airspace object. Id. (hereinafter “conflict determining limitation”). Appellants’ contentions are not persuasive. Claim 1 recites that the first airspace object, first buffer space, second airspace object, and second buffer space traverse a “future route.” In Wise, predicted protection spaces 306/312 represent future positions of respective aircrafts 302/308. See, e.g., Wise H32—33. This is indicated in Wise by aircraft symbols, like those of aircrafts 302/308, shown within the circular shapes of predicted protection spaces 306/312. Id. Accordingly, predicted protection spaces 306/312 are shown to effectively “surround” “future positions” of respective aircrafts 7 Appeal 2015-005344 Application 12/640,540 302/308 along projected flight trajectories 304, 310. Id. Appellants do not apprise us of any error in the Examiner’s determination, with regard to Wise, that “one of ordinary skill in the art would understand that the separation distances of both current and future positions of the buffer zones (306 and 312) would be calculated in order to determine the overlapping of buffer zones ([306] and 312).” Ans. 7. Such changes in the future positions of predicted protection spaces 306/312 would be along the projected flight trajectories. Id. Accordingly, we are not persuaded by Appellants’ contentions that Wise fails to teach the claimed conflict determining limitation. Appellants also contend that Lai does not teach the buffer shape limitation. Appeal Br. 11. Rather, Appellants contend, “Lai, at most, describes forming a protected airspace zone (PAZ) around only a monitoring aircraft 200.” Appeal Br. 11. Lai discloses that Ligures 2A—2C show “it may sometimes be desirable to monitor for aircraft with conflicting flight paths over a distance range from the monitoring aircraft 200 by defining, for example, a Protected Airspace Zone (‘PAZ’) 250 about the monitoring aircraft 200.” Lai, col. 7, 11. 34—38, Pigs. 2A—2C. further, Lai states that “[i]n some instances, the PAZ 250 may be defined as an upright cylinder having a defined radius S with the monitoring aircraft 200 as its center.” Id. at col. 7,11. 38-41. PAZ 250 defines a desired separation distance S between monitoring aircraft 250 and another aircraft. Id. at col. 8,11. 5—8, Pigs. 2A—2C. As shown in figures 2A—2C, PAZ 250 has the same circular shape, that is, a shape that remains constant. Appellants’ contentions with regard to Lai are not persuasive. 8 Appeal 2015-005344 Application 12/640,540 Furthermore, in Wise, as aircrafts 302 and 308 move along their respective projected flight trajectories 304, 310, associated predicted protected airspaces 306, 312 will also move along projected flight trajectories 304, 310. Although we find no explicit description in Wise that the circular shape of predicted protected airspaces 306, 312 remains constant during this movement, Figures 3 and 4 show predicted protected airspaces 306, 312 as only having the same shape (i.e., circular). Accordingly, at least based on these figures, Wise does appear to teach the buffer shape limitation, although the Examiner determined otherwise. Consequently, we sustain the rejection of claims 1,10, and 19, and claims 3, 6, 7, 12, 15, 16, 21, 24, and 25 depending therefrom, as unpatentable over Wise and Lai. However, because our analysis differs from the Examiner’s, we designate our affirmance as a new ground of rejection pursuant to 37 C.F.R. § 41.50(b) to provide Appellants with a fair opportunity to respond. Claims 2, 11, and 20 as unpatentable over Wise, Lai, and Erzberger Claims 4, 13, and 22 as unpatentable over Wise, Lai, and Harkness Claims 5, 14, and 23 as unpatentable over Wise, Lai, and Johansson Claims 8, 9, 17, 18, 26, and 27 as unpatentable over Wise, Lai, and Zobell Claims 2, 4, 5, 8, 9, 11, 13, 14, 17, 18, 20, 22, 23, 26, and 27 depend, respectively, from claim 1, 10, or 19. Appellants do not present separate argument for these dependent claims. Appeal Br. 8—11. Accordingly, we sustain the Examiner’s rejection of these dependent claims for the same reasons discussed above for the rejection of claims 1, 10, and 19 over Wise and Lai, and designate our affirmance as a new ground of rejection pursuant to 37 C.F.R. § 41.50(b). 9 Appeal 2015-005344 Application 12/640,540 DECISION We reverse the Examiner’s decision to reject claims 1—27 under 35 U.S.C. § 112, first paragraph, as failing to comply with the written description requirement. We affirm the Examiner’s decision to reject claims 1—27 under 35 U.S.C. § 103(a), and designate our affirmance as a new ground of rejection pursuant to 37 C.F.R. § 41.50(b). FINALITY OF DECISION This decision contains new grounds of rejection pursuant to 37 C.F.R. § 41.50(b). 37 C.F.R. § 41.50(b) provides “[a] new ground of rejection pursuant to this paragraph shall not be considered final for judicial review.” 37 C.F.R. § 41.50(b) also provides: When the Board enters such a non-final decision, [Appellants], within two months from the date of the decision, must exercise one of the following two options with respect to the new ground[s] of rejection to avoid termination of the appeal as to the rejected claims: (1) Reopen prosecution. Submit an appropriate amendment of the claims so rejected or new Evidence relating to the claims so rejected, or both, and have the matter reconsidered by the examiner, in which event the prosecution will be remanded to the examiner. The new ground[s] of rejection [are] binding upon the Examiner unless an amendment or new Evidence not previously of Record is made which, in the opinion of the examiner, overcomes the new ground[s] of rejection designated in this decision. Should the examiner reject the claims, [Appellants] may again appeal to the Board pursuant to this subpart. (2) Request rehearing. Request that the proceeding be reheard under § 41.52 by the Board upon 10 Appeal 2015-005344 Application 12/640,540 the same Record. The request for rehearing must address any new ground of rejection and state with particularity the points believed to have been misapprehended or overlooked in entering the new ground of rejection and also state all other grounds upon which rehearing is sought. Further guidance on responding to a new ground of rejection can be found in the Manual of Patent Examining Procedure § 1214.01. No time period for taking any subsequent action in connection with this appeal may be extended under 37 C.F.R. § 1.136(a)(l)(iv). AFFIRMED; 37 C.F.R, $ 41.50(b) 11 Copy with citationCopy as parenthetical citation