Ex Parte Gyuricsko et alDownload PDFPatent Trial and Appeal BoardNov 30, 201713719541 (P.T.A.B. Nov. 30, 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. 13/719,541 12/19/2012 Frederick S. Gyuricsko 1001-0195-2CIP 8225 140282 7590 12/04/2017 Mnrtha r'lillina T T P EXAMINER One Century Tower 265 Church Street DIXON, KEITH L New Haven, CT 06510 ART UNIT PAPER NUMBER 3644 NOTIFICATION DATE DELIVERY MODE 12/04/2017 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): ipdocketing@murthalaw.com PTOL-90A (Rev. 04/07) UNITED STATES PATENT AND TRADEMARK OFFICE BEFORE THE PATENT TRIAL AND APPEAL BOARD Ex parte FREDERICK S. GYURICSKO, JAY PHOENIX, ARNOLD E. FREDERICKSEN, and JOHN H. COWLES JR. Appeal 2016-001317 Application 13/719,541 Technology Center 3600 Before JOHN C. KERINS, MICHAEL L. HOELTER, and SEAN P. O’HANLON, Administrative Patent Judges. HOELTER, Administrative Patent Judge. DECISION ON APPEAL Appeal 2016-001317 Application 13/719,541 STATEMENT OF THE CASE Appellants appeal under 35 U.S.C. § 134(a) from a non-final rejection of claims 1—9 and 11. App. Br. 4. Claim 10 has been canceled. App. Br. 4. Appellants’ counsel provided oral argument on November 7, 2017. We have jurisdiction under 35 U.S.C. § 6(b). We reverse the Examiner’s rejections, but we enter a NEW GROUND OF REJECTION with respect to claim 1 pursuant to 37 C.F.R. § 41.50(b). THE CLAIMED SUBJECT MATTER The disclosed subject matter “relates to roller bearing assemblies for use in critical applications and, more particularly, to lined track roller bearing assemblies used within an actuation system of a leading edge of a wing of an aircraft assembly.” Spec. 12. Apparatus claim 1 is the sole independent claim, is illustrative of the claimed subject matter, and is reproduced below: 1. An actuation system for deploying and retracting a lift assisting device of a leading edge of a wing of an aircraft, the actuation system comprising: a track pivotally coupled to the lift assisting device, the track having first and second outer surfaces and side surfaces; a shaft rotationally coupled within the wing of the aircraft and operable, in response to flight control signals, to deploy or retract the lift assisting device; means for actuating the lift assisting device, coupled to the shaft, between a retracted position to a deployed position along an arcuate path; a plurality of track roller bearings rotatably contacting the first and second outer surfaces of the track to guide the track along the arcuate path; and the plurality of track roller bearings including at least one lined track roller assembly; wherein each of the at least one lined track roller assemblies comprises an inner ring having an outer bearing 2 Appeal 2016-001317 Application 13/719,541 surface and an outer ring having an inner bearing surface, the inner ring being disposed at least partially in the outer ring and a self lubricating liner is disposed on at least one of the outer bearing surface and the inner bearing surface. REFERENCES Butler US 2,620,147 US 6,149,105 US 6,180,574 B1 US 6,994,475 B2 Dec. 2, 1952 Nov. 21,2000 Jan. 30, 2001 Feb. 7, 2006 Jaggard Ryan Doll REJECTIONS Claims 1—3, 5—7, and 11 are rejected under 35 U.S.C. § 103(a) as unpatentable over Jaggard, Doll, and Ryan. Claims 4, 8, and 9 are rejected under 35 U.S.C. § 103(a) as unpatentable over Jaggard, Doll, Ryan, and Butler. ANALYSIS The rejection of claims 1—3, 5—7, and 11 as unpatentable over Jaggard, Doll, and Ryan Appellants argue all the claims (i.e., claims 1—3, 5—7, and 11) together. App. Br. 9—15. We select independent claim 1 for review with the remaining claims standing or falling with claim 1. See 37 C.F.R. § 41.37(c)(l)(iv). The Examiner primarily relies on the teaching of Jaggard for disclosing the limitations of claim 1, but acknowledges that Jaggard does not teach the limitations of a “lined track roller assembly” nor a “self-lubricating liner.” See Non-Final Act. 3. The Examiner relies, respectively, on the 3 Appeal 2016-001317 Application 13/719,541 teachings of Doll and Ryan for such teachings.1 Non-Final Act. 3; see also Ans. 3^4. The stated reason to modify the combination of Jaggard and Doll with Ryan is that the resulting combination “will result in [a] coating that is easy to apply to a variety of surfaces and that would have good wear properties even under high temperature use.” Non-Final Act. 3^4 (referencing Ryan 1:27—29). Appellants take issue with the Examiner’s stated reason to combine the cited references, i.e., “because of increase in wear properties at high temperaturesApp. Br. 10; see also Reply Br. 2, 4. Appellants contend that “high temperatures do not exist in environments where an actuation system for ... a leading edge of a wing of an aircraft is utilized.” App. Br. 10 (referencing an “Inventor Declaration submitted July 8, 2014”). Appellants state that one skilled in the art would understand that such an actuation system would be employed “where temperatures are [as] low as -55°C.” App. Br. 10 (referencing section 6 of the Inventor Declaration). Hence, as per Appellants, “increasing wear properties at high temperatures [as per Ryan] would not motivate one skilled in the art to modify the cited references in a manner that would disclose or suggest the claimed invention.2 App. Br. 10. Accordingly, “one skilled in the art concerned with 1 It is noted that both Doll and Ryan disclose the use of PTFE (i.e., Teflon®) as a suitable lining material, as do Appellants. See Doll 4:16—17; Ryan 3:48-54; Spec. 129. 2 Appellants also state that one skilled in the art “would also understand that the coefficient of friction for self-lubricating liners increases significantly with decreasing temperature and decreasing bearing pressure.” App. Br. 10 (referencing sections 9, 10, 14, and 16 of the Inventor Declaration). 4 Appeal 2016-001317 Application 13/719,541 actuation systems utilized in a wing of an aircraft [as claimed] would immediately discard Ryan as being irrelevant.” App. Br. 10. The Examiner acknowledges Ryan’s express teaching (i.e., “a particularly desirable bearing coating would be easy to apply to a variety of surface[s] and would have good wear properties even under high temperature use”). Ryan 1:26—29. The Examiner emphasizes Ryan’s usage of the term “even” stating that because of such usage, “Ryan teaches or suggests that the coating will result in good wear properties at high temperatures and at other than high temperatures.” Ans. 3 (emphasis added). The Examiner thus states, “[t]he motivation to combine Jaggard with Doll and Ryan is proper and the rejection should be upheld.” Ans. 3. Ryan discusses testing the coating at a temperature of 163°C. Ryan 9:1—3; 9:56—60. Ryan would not be viewed by a person skilled in the art as limited to elevated temperatures such as this, but Ryan also fails to evidence that it would be suitable for low temperature use. Hence, the temperature of the environment taught by Ryan is indeed different from that described in the Inventor Declaration where it is stated, “the aircraft wing and lined track rollers are exposed to subfreezing temperatures as low as -55°C.” Inventor Declaration | 6; see also Reply Br. 2. Accordingly, and based on the record presented and the Inventor Declaration describing the temperatures involved, we agree with Appellants that “one skilled in the art concerned with actuation systems utilized in a wing of an aircraft would immediately discard Ryan as being irrelevant.” App. Br. 10. We thus are not of the opinion that the Examiner has properly established a prima facie case of obviousness because the temperatures discussed in Ryan and those encountered by an aircraft wing are so vastly 5 Appeal 2016-001317 Application 13/719,541 different.3 We do not sustain the Examiner’s rejection of claims 1—3, 5—7, and 11 as being obvious over Jaggard, Doll, and Ryan. New Ground of Rejection under 37 C.F.R. § 41.50(b) However, because Doll, Ryan, and Appellants each disclose the use of PTFE (Teflon®) as a suitable lining material in roller assemblies (see supra), we investigate the characteristics of PTFE to ascertain what one skilled in the art might understand regarding that substance. A quick Internet search led to a “Properties Handbook” produced by the DuPont Company (the developer of PTFE) entitled “Teflon® PTFE fluoropolymer resin” dated July 1996, number 220313D, and bearing reorder number H- 37051-3 (replacing H-37051-2) (hereinafter “Handbook”).4 As stated therein, “[t]he design and engineering data presented in this handbook are intended to assist the design engineer in determining where and how Teflon® resins may best be used.” Handbook 1. Under the heading “Low Temperature Properties,” the Handbook states: Parts fabricated of Teflon® PTFE resins exhibit high strength, toughness, and self-lubrication at low temperatures. Teflon® PTFE resins are useful from—268°C (-A50°F) and are highly flexible from—79°C (—110°F). Handbook 23. Further, the Handbook states, “[ujseful but varying mechanical properties are maintained from—268 to 260°C (—450 to 500°F) for Teflon® PTFE.” Handbook 8. From the above, it can reasonably be concluded that one skilled in the art of self-lubricating bearing liners would have been aware of the ability to use a PTFE liner in the low temperature 3 “The PTO bears the initial burden of showing a prima facie case of obviousness.” In re Giannelli, 739 F.3d 1375, 1379 (Fed. Cir. 2014). 4 See http://www.rjchase.com/ptfe_handbook.pdf 6 Appeal 2016-001317 Application 13/719,541 environment described in the Inventor Declaration section 6 (i.e., in “subfreezing temperatures as low as -55°C”). Appellants also address pressure, stating that, with respect to aircraft actuation systems, there is a limit “as to how much force they can apply.” App. Br. 14 (referencing Inventor Declaration section 7). On this point, Appellants acknowledge, “Ryan is particularly concerned with the performance of the coating under certain conditions” which include “high pressure.” Reply Br. 3 (referencing Ryan 1:38-40). Since Ryan is directed to providing “a low friction surface” (Ryan 1:34—35), the use of Ryan’s surface would result in less force being required. Further, the Handbook states, “Figure 13 indicates that static friction of Teflon® PTFE resins decreases with increases in pressure.” Handbook 26. Hence, the use of PTFE as both Doll and Ryan suggest appears to resolve Appellants’ pressure-related issues, i.e., “[ajnother problem with lined track rollers is that the coefficient of friction decreases with decreasing bearing pressure.” App. Br. 14 (referencing Inventor Declaration, section 10). Hence, Appellants’ argument regarding a need to minimize the applied force is not persuasive the Examiner erred in view of such teachings. Accordingly, the Examiner’s statement that “Ryan teaches or suggests that the coating will result in good wear properties at high temperatures and at other than high temperatures” (Ans. 3) is supported by the Handbook’s teachings, which one skilled in the art is presumed to be aware of.5 Thus, 5 See In re Bozek, 416 F.2d 1385, 1390 (CCPA 1969) (“Having established that this knowledge was in the art, the examiner could then properly rely, as put forth by the solicitor, on a conclusion of obviousness ‘from common knowledge and common sense of the person of ordinary skill in the art without any specific hint or suggestion in a particular reference.’”). 7 Appeal 2016-001317 Application 13/719,541 the motivation expressed by the Examiner (i.e., “such a predictable arrangement will result in [a] coating that is easy to apply to a variety of surfaces . . . even under high temperature use” has rational underpinning that supports the Examiner’s conclusion of obviousness.6 Non-Final Act. 3^4. Additionally, the statements addressing temperature and pressure made in the Inventor Declaration (see supra) are not persuasive of error in view of the teachings found in the Handbook. Further, Appellants’ discussion of unexpected results is not persuasive of error since the Handbook discusses the use of PTFE in such situations.7 See App. Br. 13—15; Reply Br. 8—10. However, because we rely on additional evidence not relied on by the Examiner in supporting the rationale advanced by the Examiner, we designate our action a NEW GROUND of rejection to provide Appellants a full and fair opportunity to respond. For the above reasons, we affirm the Examiner’s rejection of claim 1, but we designate this affirmance a NEW GROUND of rejection. We elect not to specifically address dependent claims 2, 3, 5—7, and 11 under this NEW GROUND, leaving that for the Examiner to consider. The rejection of claims 4, 8, and 9 as unpatentable over Jaggard, Doll, Ryan, and Butler Appellants contend, “Butler fails to remedy the deficiencies” previously discussed. App. Br. 16. In view of the above NEW GROUND of rejection, we are not persuaded there are deficiencies to be cured. 6 See KSR Int’l Co. v. Teleflex Inc., 550 U.S. 398, 418 (2007). 7 Additionally, Appellants’ arguments regarding Doll are not persuasive since the Examiner relied on either Jaggard for such teachings or such teachings can also be found in Ryan (alone) or its combination with Jaggard. App. Br. 11—13; see also Reply Br. 4—8. 8 Appeal 2016-001317 Application 13/719,541 Accordingly, and as above, we leave it to the Examiner to consider dependent claims 4, 8, and 9 in view of the new evidence (i.e., Handbook) not previously relied upon by the Examiner. DECISION We REVERSE the Examiner’s decision to reject claims 1—9 and 11 under 35 U.S.C. § 103(a), however, as indicated supra, we designate our decision to reject claim 1 as a NEW GROUND of rejection because the Board relies on reasons and evidence different from and/or additional to those stated by the Examiner, and also to provide Appellants a fair opportunity to respond. FINALITY OF DECISION This decision contains a new ground of rejection pursuant to 37 C.F.R. § 41.50(b). Section 41.50(b) provides “[a] new ground of rejection pursuant to this paragraph shall not be considered final for judicial review.” Section 41.50(b) also provides: When the Board enters such a non-final decision, the appellant, within two months from the date of the decision, must exercise one of the following two options with respect to the new ground 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 of rejection is 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 of rejection designated in the decision. Should the examiner reject the 9 Appeal 2016-001317 Application 13/719,541 claims, appellant 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 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). REVERSED; 37 C.F.R, $ 41.50(b) 10 Copy with citationCopy as parenthetical citation