Ex Parte FUKUDADownload PDFPatent Trials and Appeals BoardMay 9, 201914070753 - (D) (P.T.A.B. May. 9, 2019) Copy Citation UNITED STA TES p A TENT AND TRADEMARK OFFICE APPLICATION NO. FILING DATE FIRST NAMED INVENTOR 14/070,753 11/04/2013 KokiFUKUDA 116 7590 05/13/2019 PEARNE & GORDON LLP 1801 EAST 9TH STREET SUITE 1200 CLEVELAND, OH 44114-3108 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. OBA-51824 7611 EXAMINER HUTCHENS, CHRISTOPHER D. ART UNIT PAPER NUMBER 3647 NOTIFICATION DATE DELIVERY MODE 05/13/2019 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): patdocket@peame.com PTOL-90A (Rev. 04/07) UNITED STATES PATENT AND TRADEMARK OFFICE BEFORE THE PATENT TRIAL AND APPEAL BOARD Ex parte KOK.I FUKUDA 1 Appeal2018-005850 Application 14/070,753 Technology Center 3600 Before JAMES P. CALVE, MICHELLE R. OSINSKI, and WILLIAM C. CAPP, Administrative Patent Judges. Opinion for the Board filed by Administrative Patent Judge OSINSKI. Opinion Concurring filed by Administrative Patent Judge CAL VE. Opinion Dissenting-in-Part filed by Administrative Patent Judge CAPP DECISION ON APPEAL STATEMENT OF THE CASE Appellant appeals under 35 U.S.C. § 134(a) from the Examiner's decision rejecting claims 1, 2, 4, 5, 7-12, and 14--17.2 We have jurisdiction over the appeal under 35 U.S.C. § 6(b ). We AFFIRM-IN-PART. 1 Mitsubishi Aircraft Corporation ("Appellant") is the Applicant and real party in interest. Appeal Br. 3. 2 Claim 3 is cancelled. Appeal Br. 19 (Claims App.). Claim 6 is objected to as being dependent upon a rejected base claim, but would be allowable if rewritten in independent form. Non-Final Act. 8. Claim 13 is allowed. Id. Appeal2018-005850 Application 14/070,753 THE CLAIMED SUBJECT MATTER Claims 1 and 10 are independent. Claim 1, reproduced below, is illustrative of the subject matter on appeal. 1. A nitrogen enriched air supply system comprising: a fuel tank provided in an aircraft, the fuel tank including a first tank, and a second tank arranged adjacent to the first tank; a nitrogen enrichment module that produces nitrogen enriched air upon supply of source gas obtained in the aircraft; a first gas pipe that supplies the nitrogen enriched air to the first tank from the nitrogen enrichment module; a spill-back pipe that is arranged between the first tank and the second tank to cause excessive fuel in the second tank to flow into the first tank, the spill-back pipe being configured such that fuel in the first tank is consumed first while setting an amount of fuel in the second tank at a given amount, wherein the spill-back pipe is set such that an inlet for the fuel is at a higher position than an outlet for the fuel within an assumed range of a climb angle of the aircraft; and a second gas pipe that directly or indirectly supplies the nitrogen enriched air to the spillback pipe. EVIDENCE Runnels us 4,378,920 Apr. 05, 1983 Wozniak US 6,997,415 B2 Feb. 14,2006 Lynas US 2011/0056970 Al Mar. 10, 2011 Surawski US 2011/0068231 Al Mar. 24, 2011 2 Appeal2018-005850 Application 14/070,753 REJECTIONS I. Claims 1, 5, 7-12, and 14--17 stand rejected under 35 U.S.C. § 103(a) as unpatentable over Surawski and Wozniak. Non-Final Act. 2---6. II. Claim 2 stands rejected under 35 U.S.C. § 103(a) as unpatentable over Surawski, Wozniak, and Lynas. Id. at 6-7. III. Claim 4 stands rejected under 35 U.S.C. § 103(a) as unpatentable over Surawski, Wozniak, and Runnels. Id. at 7. OPINION Rejection I Claims 1, 7-9, 11, and 16 The Examiner relies on Surawski for teaching most of the limitations of independent claim 1, but acknowledges that Surawski fails to teach "a spill-back pipe that is arranged between the first tank and the second tank." Non-Final Act. 2 ( citing Surawski, Fig. 1; ,r,r 1, 9). The Examiner finds that Wozniak teaches a spill-back pipe (i) arranged between first and second tanks to cause excessive fuel in the second tank to flow into the first tank; (ii) configured such that fuel in the first tank is consumed first while setting an amount of fuel in the second tank at a given amount, and (iii) that is set such that an inlet for the fuel is at a higher position than an outlet for the fuel within an assumed range of a climb angle of the aircraft. Id. at 3 ( citing Wozniak, Fig. 4b; 2: 1-12). The Examiner concludes that it would have been obvious to have modified Surawski "to incorporate the teachings of Wozniak to disperse fuel using a spill[-]back pipe ... [because] providing a spill-back pipe between the tanks would allow fuel to be transferred from the 3 Appeal2018-005850 Application 14/070,753 wing tank into the inboard tanks, to maintain structural integrity of the outboard wing tanks during flight." Id. (citing Wozniak, Fig. 4b; 2:1-12). Appellant argues that "[a]t most[,] Wozniak ... discloses a pump (not labeled) in the outboard tank wherein fuel is positively pumped in one direction from the outboard tank to the inboard tank." Appeal Br. 11. Appellant argues that "the term 'spill-back pipe' is known to those skilled in the art to refer to a pipe wherein a fluid spills into the pipe. Accordingly, a pipe wherein a fluid is pumped by force through the pipe is not a 'spill-back pipe."' Reply Br. 2. According to Appellant, because Wozniak's pipe inlet is disposed at the lowermost point of the outboard tank, the pipe "is configured to remove substantially all the fuel in the outboard tank" and is "not a 'spill-over' pipe, i.e., a pipe that allows a fluid to 'spill-over' and flow, by gravity from one tank to another tank" and also, is not configured to remove only "excessive fuel." Appeal Br. 11. The Examiner disagrees that Wozniak fails to teach a spill-back pipe. Ans. 4. In particular, the Examiner declines to read any structural limitations into the claimed spill-back pipe beyond that which is explicitly recited-i.e., that the inlet for the fuel is at a higher position than the outlet for the fuel. Id. Appellant has not pointed to an explicit definition for "spill- back pipe" in their Specification, nor has Appellant provided evidence or persuasive reasoning to support that the term "spill-back pipe" is a term of art to which a person of ordinary skill in the art would ascribe a particular meaning, namely, that a spill-back pipe must allow fluid to flow only by gravity and may not include a pump. As to Appellant's specific argument that a "spill-back pipe" refers to a pipe where fluid 'spills into [a] pipe," which excludes a fluid pumped by force through the pipe (Reply Br. 2), we 4 Appeal2018-005850 Application 14/070,753 note that an ordinary and customary meaning of the term "spill" is "to ( cause to) flow, move, fall, or spread over the edge or outside the limits of something." Cambridge Academic Content Dictionary, available at https:// dictionary.cambridge.org/ dictionary/ english/ spill. When considering such an ordinary and customary meaning of the word "spill," Appellant has not adequately explained how "spill" requires that the flow outside the limits of something be accomplished solely by gravity, and specifically, without the aid of a pump. The ordinary and customary meaning is consistent with the claim language and Appellant's Specification. See claim 1 ("a spill-back pipe that is arranged between the first tank and the second tank to cause excessive fuel in the second tank to flow into the first tank"); Spec. 4:13-16 ("a spill-back pipe ... is arranged across the first fuel tank and the second fuel tank to cause fuel in the second fuel tank to flow into the first fuel tank.") Based on the record before us, we decline to construe "spill-back pipe" so narrowly as to exclude a pipe that uses a pump to cause excessive fuel in the second tank to flow into the first tank. Consequently, we are not persuaded that the Examiner erred in determining that "the pipe in Wozniak may be interpreted as a spill-back pipe." Id. As to Wozniak's pipe being configured to remove all fuel from the second tank to flow into the first tank, rather than only "excessive fuel" as claimed, we agree with the Examiner that "any amount of fuel may be considered as excessive" such that "any amount of fuel flowing through the pipe is best understood by the [E]xaminer to read on the limitation." Id. at 4--5. Appellant has not persuaded us of error in this specific position by the Examiner. Finally, Appellant has not otherwise argued that Wozniak's 5 Appeal2018-005850 Application 14/070,753 pipe identified by the Examiner fails to meet the structural or functional limitations set forth in independent claim 1. For the foregoing reasons, Appellant does not apprise us of error in the Examiner's conclusion that the combination of Surawski and Wozniak renders obvious the subject matter of claim 1. Accordingly, we sustain the rejection of claim 1 under 35 U.S.C. § 103(a) as unpatentable over Surawski and Wozniak. We also sustain the rejection of claims 7-9, 11, and 16 under 35 U.S.C. § 103(a) as unpatentable over Surawski and Wozniak, for which Appellant relies on the same arguments and reasoning as independent claim 1. Appeal Br. 13. Claim 5 Claim 5 recites that "the nitrogen enriched air [NEA] is supplied to the second tank via the second pipe and the spill-back pipe, in a descent phase of the aircraft." Appeal Br. 19 (Claims App.). The Examiner finds that "Surawski as modified by Wozniak teach the nitrogen enriched air supply system according to claim 1, wherein the nitrogen enriched air is supplied to the second tank (40) via the second gas pipe 75 and the fuel system, in a descent phase of the aircraft." Non-Final Act. 3 (citing Surawski ,r 5) ( emphasis added). Appellant argues that the Examiner has not adequately explained how the cited references teach the NEA is supplied to the second tank via a second gas pipe and the spill-back pipe. Appeal Br. 12. The Examiner responds that "when the ... NEA ... is added to the fuel system of Surawski, the [NEA] is understood to settle into the fuel system. Therefore, at least a portion of the NEA travels anywhere that the fuel travels within the 6 Appeal2018-005850 Application 14/070,753 system, including a system modified by the teachings of Wozniak that includes a spill-back pipe." Ans. 5. As an initial matter, we note that we consider the broadest reasonable interpretation of claim 5 to extend to independent supply ofNEA to the second tank via the second pipe and independent supply ofNEA to the second tank via the spill-back pipe, rather than requiring the same supply of NEA to flow through both the second pipe and the spill-back pipe before entry to the second tank. Moreover, we note that there is no recitation in claim 5 that the NEA be supplied directly to the spill-back pipe for direct supply to the second tank. With this interpretation in mind, considering the Examiner's previous explanation that Surawski's nitrogen enrichment module has "a second gas pipe (element (75) corresponding to valve 2 (30)) that indirectly supplies the nitrogen enriched air to the fuel system ( as the air is mixing with the fuel in the tank" (Non-Final Act. 2 (citing Surawski ,r 1)), the Examiner has provided an explanation as to how nitrogen enriched air is supplied to second tank 45 via the second gas pipe (i.e., via piping 75 corresponding to valve 2 in Surawski's Figure 1). See Surawski ,r 11 ( explaining that, during descent, ambient air entering into wing tanks 40 is first mixed with NEA that has passed to mix chambers 55 via piping 75). However, we agree with Appellant that the Examiner has not adequately explained how nitrogen enriched air is supplied to the second tank (40) via the spill-back pipe, in a descent phase of the aircraft. Even considering the Examiner's previous explanation that (i) Surawski's nitrogen enrichment module has "a first gas pipe ( corresponding to valve 1 (25)) that supplies the nitrogen enriched air to the first tank ( 45) from the nitrogen enrichment module (15)" and (ii) Surawski is being modified to include a 7 Appeal2018-005850 Application 14/070,753 spill-back pipe between tanks 45 and 40 (id. at 3), it is not entirely clear how NEA would be supplied to wing tank 40 via such a spill-back pipe disposed between tanks 45 and 40 because valve 25 is closed during descent (such that it would not be supplying NEA to the center tank 45 that could then enter the wing tank 40 via the spill-back pipe) and also "[b ]ecause of increasing pressure in the wing tanks, there is a natural flow through line 70 towards the center tank," rather than a flow from the center tank 45 towards the wing tanks 40 (Surawski ,r 11 ). Even if the NEA would ultimately travel to the spill-back pipe of modified Surawski in some way, we agree with Appellant that without more explanation, it is not clear by a preponderance of the evidence that NEA can be supplied to the second tank via the spill-back pipe in a descent phase of the aircraft. For the foregoing reasons, Appellant apprises us of error in the Examiner's conclusion that the combination of Surawski and Wozniak renders obvious the subject matter of claim 5. Accordingly, we do not sustain the rejection of claim 5 under 35 U.S.C. § 103(a) as unpatentable over Surawski and Wozniak. Claim 14 Claim 14 recites that "the spill-back pipe is configured to cause the excessive fuel in the second tank exceeding a predetermined height to overflow into the first tank." Appeal Br. 21 (Claims App.). The Examiner finds that "the spill-back pipe [of Wozniak is configured to cause the excessive fuel in the second tank (i.e., outboard wing tank) exceeding a predetermined height (i.e.[,] the height to which the pump may initiate 8 Appeal2018-005850 Application 14/070,753 transfer of fuel) to overflow into the first tank (i.e.[,] inboard wing tank ([F]ig. 4b)." Non-Final Act. 5. Appellant argues that "[a]t most, it is the pump of Wozniak ... that controls the height of fuel in the outboard tank," whereas the claim requires that the spill-back pipe itself be configured to remove the excessive fuel. Appeal Br. 13. The Examiner responds that "the pump is located at a predetermined height, and ... if the fuel is not located at the height of the pump, the fuel would not flow into the pipe" and because "the pipe is attached to the pump in Wozniak, the pipe is configured to cause the fuel to flow from the second tank into the first tank when exceeding the predetermined height." Ans. 5---6. We agree with the Examiner that the spill-back pipe is configured to cause excessive fuel in the second tank exceeding a predetermined height to overflow into the first tank in that the vertical location of the pipe and the pump attached to it affect the ability to transfer fuel from the second tank to the first tank. For the foregoing reasons, Appellant does not apprises us of error in the Examiner's conclusion that the combination of Surawski and Wozniak renders obvious the subject matter of claim 14. Accordingly, we sustain the rejection of claim 14 under 35 U.S.C. § 103(a) as unpatentable over Surawski and Wozniak. Claims 10, 12, 15, and 17 Whereas independent claim 1 requires "a second gas pipe that directly or indirectly supplies the nitrogen enriched air to the spill-back pipe" (Appeal Br. 18 (Claims App.)), independent claim 10 more particularly requires that "the nitrogen enriched air is supplied to the second tank via the 9 Appeal2018-005850 Application 14/070,753 gas pipe and the spill-back pipe, in a descent phase of the aircraft" similar to dependent claim 5 (id. at 20 (Claims App.)). For the same reasons as described above in connection with dependent claim 5, Appellant apprises us of error in the Examiner's conclusion that the combination of Surawski and Wozniak renders obvious the subject matter of claim 10. Accordingly, we do not sustain the rejection of claim 10, or claims 12, 15, and 17 depending therefrom, under 35 U.S.C. § 103(a) as unpatentable over Surawski and Wozniak. Rejection II Claim 2 recites, among other things, "a bypass pipe that penetrates a boundary between the first tank and the second tank passes through an inside of the first tank, the bypass pipe including an inlet and an outlet for the fuel, the inlet and the outlet of the bypass pipe being provided in the second tank." Appeal Br. 18 (Claims App.). The Examiner finds that "Surawski as modified by Wozniak ... teach a bypass pipe (for fuel (80)) that penetrates a boundary between the first tank and the second tank ([F]ig. 5) and passes through an inside of the first tank ... , the bypass pipe including an outlet for the fuel (where fuel (80) is exiting) and an inlet (56) ([F]ig. 7), the inlet[] and the outlet of the bypass pipe[] being provided in a second tank ([F]ig. 7)." Non-Final Act. 6. The Examiner acknowledges that "Surawski as modified by Wozniak fails to disclose the inlet (56) is a pipe." Id. The Examiner turns to Lynas as teaching "a fuel tank system having a conduit (202) for transferring fuel from an outboard tank (107) to an inboard tank (102)." Id. The Examiner concludes that it would have been obvious to have further modified 10 Appeal2018-005850 Application 14/070,753 Surawski/Wozniak "to have a pipe at the inlet" that "would create space for a valve to control the return of fuel from the outboard tank." Id. at 7. Appellant argues that "[p]lacing the pipe ofLynas ... into the opening 56, at most, simply replaces the opening for a pipe. [However,] [t]he inlet of the pipe would still be in one tank and the outlet of the pipe would be in a different tank." Reply Br. 5. We agree with Appellant. Modifying opening 56 of Figure 7 of Wozniak so as be a pipe does not adequately explain how the particular pipe, of which the outlet has been indicated as being where fuel 80 is exiting in a tank, has an inlet that is provided in the same tank. For the foregoing reasons, Appellant apprises us of error in the Examiner's conclusion that the combination of Surawski, Wozniak, and Lynas renders obvious the subject matter of claim 2. Accordingly, we do not sustain the rejection of claim 2 under 35 U.S.C. § 103(a) as unpatentable over Surawski, Wozniak, and Lynas. Rejection III Appellant relies on the same arguments and reasoning we found unpersuasive in connection with independent claim 1 as the basis for seeking reversal of the rejection of claim 4. Appeal Br. 16. Accordingly, we also sustain the rejection of claim 4 under 35 U.S.C. § 103(a) as unpatentable over Surawski, Wozniak, and Runnels. DECISION The Examiner's decision to reject claims 1, 7-9, 11, 14, and 16 under 35 U.S.C. § 103(a) as unpatentable over Surawski and Wozniak is AFFIRMED. 11 Appeal2018-005850 Application 14/070,753 The Examiner's decision to reject claims 5, 10, 12, 15, and 17 under 35 U.S.C. § 103(a) as unpatentable over Surawski and Wozniak is REVERSED. The Examiner's decision to reject claim 2 under 35 U.S.C. § 103(a) as unpatentable over Surawski, Wozniak, and Lynas is REVERSED. The Examiner's decision to reject claim 4 under 35 U.S.C. § 103(a) as unpatentable over Surawski, Wozniak, and Runnels 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). See 37 C.F.R. § 1.136(a)(l )(iv). AFFIRMED-IN-PART 12 UNITED STATES PATENT AND TRADEMARK OFFICE BEFORE THE PATENT TRIAL AND APPEAL BOARD Ex parte KOK.I FUKUDA Appeal2018-005850 Application 14/070,753 Technology Center 3600 Before JAMES P. CAL VE, MICHELLE R. OSINSKI, and WILLIAM C. CAPP, Administrative Patent Judges. CAL VE, Administrative Patent Judge, concurring. I concur with the decision authored by Judge Osinski; however, additional issues support the decision to affirm the Examiner's rejection. The Appeal Brief shall contain arguments, which "shall explain why the examiner erred as to each ground of rejection contested by appellant." 37 C.F.R. § 41.37(c)(l)(iv). The Board has interpreted this provision (and its predecessor) to require an applicant to identify the alleged error in an examiner's rejections. In re Jung, 637 F.3d 1356, 1365 (Fed. Cir. 2011) ("Moreover, even assuming that the examiner had failed to make a prima facie case, the Board would not have erred in framing the issue as one of 'reversible error."); Ex parte Frye, 94 USPQ2d 1072, 1075 (BPAI 2010) (precedential) ("The panel then reviews the obviousness rejection for error based upon the issues identified by appellant, and in light of the arguments and evidence produced thereon.") (cited with approval in Jung, 637 F.3d at 1365). As a result, we limit our review to arguments raised by Appellant. Appeal2018-005850 Application 14/070,753 Regarding the rejection of claim 1, Appellant argues that Figure 4b of Wozniak teaches pump that conveys fuel from an outboard fuel tank to an inboard fuel tank through a pipe. Appeal Br. 10. Thus, this fact is admitted. The Examiner correctly finds that Wozniak discloses all the structure recited in claim 1 for the claimed system. Ans. 4--5. In response, Appellant argues that Wozniak's pipe is disposed at a lowermost part of the outerboard tank and a pump removes substantially all of the fuel in the outboard tank. Appeal Br. 11. Appellant argues the pipe of Wozniak is not a "spill-back" pipe because it does not allow excessive fluid to spill-over or flow by gravity from one tank to another. Id. Appellant's arguments regarding the position of Wozniak's pipe in a lowermost part of the outboard tank is not persuasive because claim 1 does not exclude such a position or recite any particular position of an outlet in either tank. Claim 1 merely requires an inlet for the fuel to be at a higher position than an outlet for the fuel. The Examiner identifies structure in Wozniak that places one end of the pipe in Figure 4b at a higher position than another end of the pipe, i.e., the end of the pipe located in the outboard tank is shown as "higher" than the other end in the inboard tank. Claim 1 requires no more in this regard, and Appellant's arguments do not apprise me of Examiner error in these findings. Nor does Appellant's attorney provide any evidence that a spill-back is an art-recognized term or element. See Reply Br. 2; see also Invitrogen Corp. v. Clontech Labs., Inc., 429 F.3d 1052, 1068 (Fed. Cir. 2005) ("Unsubstantiated attorney argument regarding the meaning of technical evidence is no substitute for competent, substantiated expert testimony."). 2 Appeal2018-005850 Application 14/070,753 Furthermore, Appellant's arguments that the claimed spill-over must allow a fluid to spill-over or flow by gravity from one tank to another is not commensurate with the scope of claim 1. Claim 1 recites that a spill-back pipe is arranged between the first and second tank "to cause excessive fuel in the second tank to flow into the first tank." As Appellant points out, the spill-back pipe does not cause fluid to flow; gravity does. Claim 1 does not recite this critical feature of the spill-back pipe, particularly given the many orientations of an aircraft during flight. Thus, Appellant has not explained persuasively why the fuel flow pipe in Wozniak cannot be a spill-back pipe. Moreover, Appellant has not explained why the presence of a pump prevents fluid flow in Wozniak's pipe due to gravity. Essentially, Appellant wants us to interpret "spill-back pipe" to mean an element having an "inlet" and an "outlet" without a pump attached either to the inlet or to the outlet such that fluid flows through the spill-back pipe via gravity. Appellant points to no lexicographic definition that requires us to interpret this term in such a limited manner. Under a broadest reasonable interpretation, we are not required to read limitations from the Specification into the claims or to limit the claims to a particular embodiment when the claim language is broader than that embodiment as it is here. Essentially, Appellant wants us to interpret "spill-back pipe" as imposing a negative limitation such that no other element is connected to an inlet or an outlet. The Examiner correctly finds that Wozniak's pump would "cause excessive fuel in the second tank to flow into the first tank" and Appellant has not apprised us of error in that finding except to argue that Wozniak does not prevent "excessive" fuel in the second tank. See Final Act. 3; Appeal Br. 11; Reply Br. 2 ( arguing that a pump where fluid is pumped 3 Appeal2018-005850 Application 14/070,753 through the pipe is not a "spill-back pipe"). Appellant's argument raises an issue regarding the clarity of claim 1. Appellant's interpretation of claim 1 to require fluid to be "allowed" to flow by "gravity" when claim 1 merely requires the pipe to "cause excessive fuel ... to flow" without specifying that such flow is caused only by gravity should be clarified. During patent examination the pending claims must be interpreted as broadly as their terms reasonably allow .... The reason is simply that during patent prosecution when claims can be amended, ambiguities should be recognized, scope and breadth of language explored, and clarification imposed .... An essential purpose of patent examination is to fashion claims that are precise, clear, correct, and unambiguous. Only in this way can uncertainties of claim scope be removed, as much as possible, during the administrative process. In re Zietz, 893 F.2d 319, 321-22 (Fed. Cir. 1989) (quoted in Packard, 751 F.3d at 1313). Because applicants are in the best position to resolve any ambiguity in the patent claims, patent examiners should demand that they do so in appropriate circumstances so the application can be amended during prosecution rather than attempting to resolve the ambiguity in litigation. Halliburton Energy Servs., Inc. v. M-I LLC, 514 F.3d 1244, 1255 (Fed. Cir. 2008) (quoted in Packard, 751 F.3dat 1313). The term "excessive" raises similar issues of clarity. It is well settled that claim language whose meaning depends entirely on a person's purely subjective opinion, personal taste, or opinion without any guidance in the claim language or written description is indefinite. E.g., Sonix Tech. Co. v. Publ'ns Int'!, Ltd., 844 F.3d 1370, 1378 (Fed. Cir. 2017); Interval Licensing LLC v. AOL, Inc., 766 F.3d 1364, 1373-74 (Fed. Cir. 2014); Datamize, LLC v. Plumtree Software, Inc., 417 F.3d 1342, 1352 (Fed. Cir. 2005). 4 Appeal2018-005850 Application 14/070,753 Appellant's arguments do not provide any objective standard or other explanation to guide a skilled artisan to determine what is an "excessive" amount of fuel. Nor has Appellant explained why Wozniak's arrangement does not satisfy this limitation. See Appeal Br. 11; Reply Br. 2-3; see also In re Schreiber, 128 F.3d 1473, 1478 (Fed. Cir. 1997) (holding that a patent applicant may recite features of an apparatus structurally or functionally; however, if the PTO has a reason to believe that the prior art possesses that functional feature as an inherent characteristic, it has the authority to require the applicant to prove that the subject matter does not possess the claimed functional feature.). Notably, claim 1 does not even clearly tie the inlet and outlet to the spill-back pipe. The spill-back pipe is "set such that an inlet for the fuel is at a higher position than an outlet for the fuel." 5 UNITED STATES PATENT AND TRADEMARK OFFICE BEFORE THE PATENT TRIAL AND APPEAL BOARD Ex parte KOK.I FUKUDA Appeal2018-005850 Application 14/070,753 Technology Center 3600 Before JAMES P. CALVE, MICHELLE R. OSINSKI, and WILLIAM C. CAPP, Administrative Patent Judges. CAPP, Administrative Patent Judge, dissenting-in-part. I do not agree with the majority's decision to sustain the Examiner's rejection of claim 1. In my opinion, the Examiner and panel majority use an overly broad interpretation of the "spill-back pipe" limitation. During examination of a patent application, pending claims are given their broadest reasonable construction consistent with the specification. In re Am. A cad. of Sci. Tech Ctr., 367 F.3d 1359, 1364 (Fed. Cir. 2004). Under the broadest reasonable interpretation standard, claim terms are given their ordinary and customary meaning as would be understood by one of ordinary skill in the art in the context of the entire disclosure. In re Translogic Tech., Inc., 504 F.3d 1249, 1257 (Fed. Cir. 2007). However, a construction that is "unreasonably broad" and which does not "reasonably reflect the plain language and Appeal2018-005850 Application 14/070,753 disclosure" will not pass muster. Microsoft Corp. v. Proxyconn, Inc. v 789 F.3d 1292, 1298 (Fed. Cir. 2015). It is a "bedrock principle" of patent law that "the claims of a patent define the invention to which the patentee is entitled the right to exclude." Innova/Pure Water, Inc. v. Safari Water Filtration Systems, Inc., 381 F.3d 1111 (Fed. Cir. 2004); see also Vitronics Corp. v. Conceptronic, Inc., 90 F.3d 1576 (Fed.Cir.1996) ("we look to the words of the claims themselves ... to define the scope of the patented invention"); Markman v. Westview Instruments, Inc., 52 F.3d 967,980 (Fed.Cir.1995) (en bane), ajfd, 517 U.S. 370 (1996) ("The written description part of the specification itself does not delimit the right to exclude. That is the function and purpose of claims."). It is well settled that the claims themselves provide substantial guidance as to the meaning of particular claim terms. Phillips v. A WH Corp., 415 F.3d 1303, 1314 (Fed. Cir. 2005); see also ACTV, Inc. v. Walt Disney Co., 346 F.3d 1082, 1088 (Fed.Cir.2003) ("the context of the surrounding words of the claim also must be considered in determining the ordinary and customary meaning of those terms"). Thus, the context in which a term is used in the asserted claim can be highly instructive. Phillips, at 1314. The Phillips court cited numerous examples in which the use of a term within the claim provides a firm basis for construing the term. Id., citing Mars, Inc. v. HJ. Heinz Co., 377 F.3d 1369, 1374 (Fed. Cir. 2004) (claim term "ingredients" construed in light of the use of the term "mixture" in the same claim phrase); Process Control Corp. v. HydReclaim Corp., 190 F.3d 1350, 1356 (Fed. Cir. 1999) (claim term "discharge rate" construed in light of the use of the same term in another limitation of the same claim). 2 Appeal2018-005850 Application 14/070,753 In my opinion, the majority decision relies too heavily on a plain English language dictionary definition of "spill" to derive an ordinary and customary meaning for "spill-back pipe." Phillips highlighted the problem with over reliance on dictionary definitions in construing claim language. The main problem with elevating the dictionary to such prominence is that it focuses the inquiry on the abstract meaning of words rather than on the meaning of claim terms within the context of the patent. Properly viewed, the "ordinary meaning" of a claim term is its meaning to the ordinary artisan after reading the entire patent. Yet heavy reliance on the dictionary divorced from the intrinsic evidence risks transforming the meaning of the claim term to the artisan into the meaning of the term in the abstract, out of its particular context, which is the specification. Phillips, 415 F.3d at 1321. In the instant case, the word "spill" is used in the context of aircraft fuel systems. Persons of ordinary skill in such field understand that fuel can be transferred between fuel tanks by means of either gravity or fuel transfer pumps. Persons of ordinary skill also understand that aircraft and their associated fuel systems are affected by various forces and changes of orientation vis-a-vis the Earth's gravitational force. For example, banking an aircraft left and right, changing an aircraft angle of attack during climb or descent, and G-forces experienced in aircraft maneuvering may have different effects on various aspects of an aircraft fuel system depending on whether those aspects operate under gravity flow or via a fuel transfer pump. Here, the claimed "spill-back pipe" is arranged between a first tank and a second tank. Claims App., claim 1. Such arrangement causes "excessive fuel" in the second tank to flow into the "first tank." Id. Furthermore, the spill-back pipe is configured so that fuel in the first tank is 3 Appeal2018-005850 Application 14/070,753 consumed first while setting an amount of fuel in the second tank at a given amount. Id. Furthermore, a spill-back pipe inlet situated so that it is in a higher position than an outlet. Id. Moreover, situating an inlet in a higher position than an outlet takes into account a climb angle of the aircraft. Id. Taking the foregoing into account, it is my opinion that a person of ordinary skill in the art of aircraft fuel system design would understand that the claimed "spill-back" pipe entails fuel transfer between tanks by gravity flow and without the assistance of a fuel transfer pump. It strikes me as incongruent that person of ordinary skill in the art would understand a "spill- back pipe" to encompass a fuel transfer pump in the overall context of a system that contemplates "excessive fuel," "setting an amount ... in the second tank," and the height of an inlet and outlet relative to climb angle. Therefore, taking the surrounding context of the language of the claim into account and applying the correct construction, the Wozniak reference fails to satisfy the "spill-back pipe" limitation of claim 1 as Wozniak relies on a fuel transfer pump rather than gravity to transfer fuel from a first tank to a second tank. For the foregoing reasons, I would reverse the Examiner's rejection of claim 1 as well as the rejection of any other claims that are based on finding that Wozniak discloses a "spill-back pipe." 4 Copy with citationCopy as parenthetical citation