Ex Parte XuDownload PDFPatent Trial and Appeal BoardOct 18, 201713066827 (P.T.A.B. Oct. 18, 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. 13/066,827 04/25/2011 Cheng Xu H0023099 9137 93153 7590 10/20/2017 HONEYWELL/GRIECCI Patent Services 115 Tabor Road P.O.Box 377 MORRIS PLAINS, NJ 07950 EXAMINER MCCAFFREY, KAYLA M ART UNIT PAPER NUMBER 3745 NOTIFICATION DATE DELIVERY MODE 10/20/2017 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): patentservices-us @ honey well, com pto @ griecci. com sherry, vallabh @ honey well. com PTOL-90A (Rev. 04/07) UNITED STATES PATENT AND TRADEMARK OFFICE BEFORE THE PATENT TRIAL AND APPEAL BOARD Ex parte CHENG XU Appeal 2016-0042781 Application 13/066,827 Technology Center 3700 Before JOHN C. KERINS, LEE L. STEPINA, and SEAN P. O’HANLON, Administrative Patent Judges. O’HANLON, Administrative Patent Judge. DECISION ON APPEAL STATEMENT OF THE CASE Cheng Xu (Appellant) appeals under 35U.S.C. § 134 from the Examiner’s February 4, 2015, non-final decision (“Non-Final Act.”) rejecting claims 1—5 and 7—27. We have jurisdiction over this appeal under 35 U.S.C. § 6(b). 1 The Appeal Brief identifies Honeywell International, Inc. as the real party in interest. Appeal Br. 3. Appeal 2016-004278 Application 13/066,827 SUMMARY OF THE DECISION We AFFIRM-IN-PART. SUMMARY OF THE INVENTION Appellant’s disclosure is directed to “a mixed or radial flow turbocharger wheel having contoured surfaces for secondary flow control.” Spec. 11. Claim 1, reproduced below from page 25 (Claims Appendix) of the Appeal Brief, is illustrative of the claimed subject matter: 1. A turbocharger wheel, comprising: a hub of a radial flow configuration, being characterized by an axis of rotation; and a plurality of blades, each blade having a hub edge adjoining the hub, a shroud edge opposite the hub edge, a leading edge, and a trailing edge; wherein the wheel is configured to rotate around the axis of rotation in a given direction with respect to its leading edge during turbocharger operation such that the leading edge is upstream of the trailing edge, and such that each blade is characterized by a pressurized surface and a suction surface; wherein the cross-sectional shape of each suction surface, when taken perpendicular to the flow direction at a streamwise location, is characterized by a blade intermediate portion, a concave inner portion that is closer to the hub edge than the blade intermediate portion, and a concave outer portion that is closer to the shroud edge than the blade intermediate portion; and wherein the blade intermediate portion is characterized by a curvature that is both less concave than the inner portion, and less concave than the outer portion. 2 Appeal 2016-004278 Application 13/066,827 REJECTIONS I. Claims 1—5 and 7—10 stand rejected under 35 U.S.C. § 103(a) as being unpatentable over Ghizawi (US 7,147,433 B2, issued Dec. 12, 2006) and Burton (US 2008/0152504 Al, published June 26, 2008). II. Claims 11—13 stand rejected under 35 U.S.C. § 103(a) as being unpatentable over Ghizawi, Burton, and Parsons (US 899,319, issued Sept. 22, 1908). III. Claim 14 stands rejected under 35 U.S.C. § 103(a) as being unpatentable over Ghizawi, Burton, and Jansen (US 5,215,439, issued June 1, 1993). IV. Claim 15 stands rejected under 35 U.S.C. § 103(a) as being unpatentable over Ghizawi, Burton, and Hausammann (US 2,918,254, issued Dec. 22, 1959). V. Claim 16 stands rejected under 35 U.S.C. § 103(a) as being unpatentable over Ghizawi, Burton, Hausammann, and Jansen. VI. Claim 17 stands rejected under 35 U.S.C. § 103(a) as being unpatentable over Ghizawi, Burton, Hausammann, Jansen, and Parsons. VII. Claims 18—24 stand rejected under 35 U.S.C. § 103(a) as being unpatentable over Ghizawi and Parsons. VIII. Claim 25 stands rejected under 35 U.S.C. § 103(a) as being unpatentable over Ghizawi, Parsons, and Jansen. IX. Claim 26 stands rejected under 35 U.S.C. § 103(a) as being unpatentable over Ghizawi, Parsons, and Hausammann. X. Claim 27 stands rejected under 35 U.S.C. § 103(a) as being unpatentable over Ghizawi, Parsons, Hausammann, and Jansen. 3 Appeal 2016-004278 Application 13/066,827 ANALYSIS Rejection I Claims 1 and 7—10 The Examiner finds that Ghizawi discloses a turbocharger wheel substantially as recited in independent claim 1, but does not disclose the recited inner, intermediate, and outer portions of the suction surface. Non- Final Act. 4—5. The Examiner finds that Burton discloses a blade (multi lean vane 122) with a suction surface having a shape such that intermediate portion 176 thereof is less concave than either end section 174, 178, and reasons that it would have been obvious to one of ordinary skill to “to modify the blade of [Ghizawi] with a curving profile as taught by [Burton] in order to reduce the effects of secondary flow.” Id. at 5 (citing Burton 13). Appellant traverses, arguing that “Burton pertains to the profile of an axial stator vane” and “the aerodynamics of an axial stator blade [are] significantly different than the aerodynamics of a radial turbine blade.” Appeal Br. 12; see also Reply Br. 3. According to Appellant, “an axial stator blade does not spin, and is configured to have air travel across the blade without applying forces in a lateral direction (i.e., in a direction perpendicular to the flow direction, across the length of the blade between its root and outer edge),” and, “[o]n the other hand, a radial turbocharger blade, such as is claimed in claim 1, is configured to turn air between the radial and axial directions.” Appeal Br. 12. Thus, Appellant asserts, “the preferred cross-sectional shape [s] of the two blades across the blade from root to tip would not be expected to be similar” and “a person of skill in the art would 4 Appeal 2016-004278 Application 13/066,827 not find it obvious to modify the radial turbine wheel blade of Ghizawi with the profile of the Burton axial stator blade.” Id. at 12—13. Appellant’s arguments are unpersuasive of error. The assertions that a stator and rotor are so different that a skilled artisan would not apply the teachings of one to the other is unsupported by any evidence or declaration. It is well settled that arguments of counsel cannot take the place of factually supported objective evidence. See, e.g., In re De Blauwe, 736 F.2d 699, 705 (Fed. Cir. 1984). Rather, as correctly noted by the Examiner (see Non-Final Act. 2—3; Ans. 2—3), Ghizawi and Burton are both directed to the same problem as Appellant’s application — reducing pressure losses. See, e.g., Ghizawi 7:39—51; Burton 13; Spec. 13. Thus, the Examiner’s determination that one of skill in the art would combine the teachings of Burton with those of Ghizawi is supported by a rational underpinning. Appellant’s arguments are presented in conclusory fashion with no supporting evidence or persuasive technical reasoning, and thus fail to apprise us of error in the Examiner’s rejection. Accordingly, for the foregoing reasons, we sustain the rejection of claim 1 and its dependent claims 7—10, which are not argued separately, as being unpatentable over Ghizawi and Burton. Claims 2—5 Independent claim 2 recites a turbocharger wheel and, in addition to including the recitations of claim 1, also requires: wherein the cross-sectional shape of each suction surface, when taken perpendicular to the flow direction at the streamwise location, is further characterized at the streamwise location by a shape defined by a smoothly varying curve that extends across 5 Appeal 2016-004278 Application 13/066,827 the concave inner portion, the intermediate portion and the concave outer portion, with no inflection points, added to a cyclical component that extends across the concave inner portion, the intermediate portion and the concave outer portion, having at least two inflection points, two of which respectively delineate the border between inner portion and the blade intermediate portion, and the border between the blade intermediate portion and the outer portion. Appeal Br. 26 (Claims App.). The Examiner relies on Ghizawi and Burton in rejecting claim 2 similarly as with regard to the rejection of claim 1, and further finds that Ghizawi discloses a streamwise cross-sectional shape defined by a smoothly varying curve added to a cyclical component. Non-Final Act. 6 (citing Burton, Fig. 5). The Examiner further determines that the streamwise cross- sectional shape recitation is a product-by-process limitation and, therefore, “has not been given patentable weight.” Id. at 7; see also id. at 3; and Ans. 3. Appellant traverses, first arguing that claim 2 is allowable for the same reasons as claim 1 because claim 2 includes all of the recitations of claim 1. Appeal Br. 13. This argument is unpersuasive for the reasons set forth above. Appellant also argues that the recited cross-sectional shape of the suction surface is a structural limitation, not a method-type limitation. Id. at 14; see also Reply Br. 3. “A product-by-process claim is ‘one in which the product is defined at least in part in terms of the method or process by which it is made.’” SmithKline Beecham Corp. v. Apotex Corp., 439 F.3d 1312, 1315 (Fed. Cir. 2006) (citing Bonito Boats, Inc. v. Thunder Craft Boats, Inc., 489 U.S. 141, 6 Appeal 2016-004278 Application 13/066,827 158 n. (1989)). Here, claim 2 recites that the cross-sectional shape of the suction surface is defined by a smoothly varying curve added to a cyclical component, both of which extending across the inner, intermediate, and outer portions. Appeal Br. 26 (Claims App.). This describes and further limits the recited suction surface, and, thus, is a structural limitation; the claim does not require any particular method or process by which the blades, or the suction surfaces of the blades, is to be made. Therefore, we agree with Appellant that the Examiner’s determination to the contrary is in error. Appellant also argues that although the rejection relies on Burton’s Figure 5 as disclosing the recited suction surface cross-sectional shape as being defined by a smoothly varying curve added to a cyclical component, the rejection “fails to identify how it discloses the two curves.” Appeal Br. 13-14. “[R]ejections on obviousness grounds cannot be sustained by mere conclusory statements; instead, there must be some articulated reasoning with some rational underpinning to support the legal conclusion of obviousness.” In re Kahn, 441 F.3d 977, 988 (Fed. Cir. 2006) (emphasis added) (cited with approval mKSR Int’l Co. v. Teleflex Inc., 550 U.S. 398, 418 (2007)). We are persuaded that the rejection does not satisfy these requirements. The Examiner’s rejection does little more than recite the final “wherein” clause of claim 2 and state that the recitations are shown in Burton Figure 5. The Examiner does not explain how this figure shows the recited smoothly varying curve or cyclical component, or how each of these curve components extends across the recited inner, intermediate, and outer 7 Appeal 2016-004278 Application 13/066,827 portions. Nor does the Examiner cite to any written description of the curve depicted in Figure 5 or offer any further explanation in the Examiner’s Answer. At most, we understand Burton’s Figure 5 to show a smoothly varying curve extending along the length thereof with an added component in the central portion thereof. Whether this added component is cyclical or whether it extends across inner, intermediate, and outer portions of Burton’s multi-lean vane 122, however, has not properly been established by the Examiner and is not readily apparent from our review of Burton. Accordingly, for the foregoing reasons, we do not sustain the rejection of claim 2 and its dependent claims 3—5 as being unpatentable over Ghizawi and Burton. Rejection III With respect to the rejection of claim 14, Appellant relies on the arguments presented above in regard to the rejection of claim 1. Appeal Br. 15. Accordingly, for the same reasons as discussed above, we also sustain the rejection of claim 14 as being unpatentable over Ghizawi, Burton, and Jansen. Rejection IV Claim 15 depends directly from claim 1 and further requires, in relevant part: between the hub edges of each successive pair of blades, the hub forms a hub end-wall extending between the inlet surface and the outlet surface; wherein the cross-sectional shape of each hub end-wall, when taken parallel to the flow direction and represented 8 Appeal 2016-004278 Application 13/066,827 meridionally, is further characterized at the cross-stream location by a shape defined by a smoothly varying curve that extends across the concave upstream portion, the streamwise intermediate portion and the concave downstream portion, with no inflection points, added to a cyclical component that extends across the concave upstream portion, the streamwise intermediate portion and the concave downstream portion, having at least two inflection points, two of which respectively delineate the border between the upstream portion and the streamwise intermediate portion, and the border between the streamwise intermediate portion and the downstream portion. Appeal Br. 29 (Claims App.). The Examiner relies on Ghizawi and Burton as discussed above with respect to the rejection of claim 1, and further finds that this combination of references does not disclose the cross-sectional shape of the hub end-wall surface having a meridional cross-sectional shape defined by a smoothly varying curve added to a cyclical component as recited in claim 15. Non- Final Act. 10. The Examiner finds that Hausammann discloses a hub surface having downstream, intermediate, and upstream portions having a shape defined by a smoothly varying curve added to a cyclical component. Id. at 10-11 (providing a copy of Hausammann Figure 3a annotated to show concave and convex surfaces). The Examiner clarifies that it is the combination of Hausammann’s cyclic component added to the smoothly varying curve of Ghizawi’s hub surface that results in the recited meridional surface shape. Ans. 4. The Examiner reasons that it would have been obvious to one of ordinary skill to modify Ghizawi’s hub with Hausammann’s contoured surface “to reduce frictional losses of the flow stream at the hub surface.” Non-Final Act. 12 (citing Hausammann, 1:58— 60). The Examiner further determines that the cross-sectional end-wall 9 Appeal 2016-004278 Application 13/066,827 shape recitation is a product-by-process limitation and, therefore, “has not been given patentable weight.” Id. at 11; see also Ans. 5. Appellant traverses, first arguing that “Hausammann does not define the cross-sectional shape of each hub end-wall when taken parallel to the flow direction and represented meridionally.” Appeal Br. 17 (emphasis omitted). Although Appellant does not offer an explicit definition of meridionally, we understand this term to mean a projection onto the plane defined by the rotational axis and the radial direction (which is defined by the blades extending away from the hub). See Spec. 148, Fig. 7; see also Ghizawi 5:41—43, Fig. 3. With the term thus defined, we agree with the Examiner that Hausammann Figure 3a illustrates a meridional cross- sectional view of hub surface 4, regardless of whether Hausammann explicitly describes the view as such. See Ans. 4; Hausammann Figs. 1—3a. Appellant also argues that the recited shape of the cross-sectional shape of the end-wall is a structural limitation, not a method-type limitation. Appeal Br. 17. We agree for the same reasons as set forth above regarding the rejection of claim 2. Appellant also argues that “Hausammann fails to disclose a shape that includes a component that is a smoothly varying curve with no inflection points extending across the upstream, intermediate and downstream portions.” Id.', see also Reply Br. 4. Although Appellant may be correct that Hausammann alone does not disclose the recited hub end-wall shape, we are unpersuaded of error because the Examiner relies on the combination of the smoothly varying curve of 10 Appeal 2016-004278 Application 13/066,827 Ghizawi’s hub surface added to Hausammann’s cyclic component. Ans. 4. Appellant’s arguments are not persuasive because they attack the individual teachings of Hausammann and do not address what the combination of references teaches, as explained by the Examiner. “Nonobviousness cannot be established by attacking references individually where the rejection is based upon the teachings of a combination of references.” In re Merck & Co., Inc., 800 F.2d 1091, 1097 (Fed. Cir. 1986). Finally, Appellant argues that “Hausammann fails to teach that the frictional losses are reduced by the shape of the hub surface,” and, thus, the Examiner’s rationale for combining Hausammann with Ghizawi and Burton is improper. Appeal Br. 17. Appellant asserts that “as a whole, ... the Hausammann invention reduces friction losses by overcoming the requirement of a high number of small length blades, which allows for greater blade spacing, and thereby removes the hub conditions that occur with blades that are too close.” Id. at 18. Continuing, Appellant asserts that such a teaching is inapplicable to the turbocharger wheel of claim 15 because radial turbines “are not known to require a large number of closely spaced blades.” Id. Hausammann discloses that its contoured hub surface provides an asymmetrical pressure distribution on its partition walls (i.e., blade surfaces). Hausammann 4:73—5:24. As noted by Appellant, this, in turn, reduces friction losses. Id.', see also Appeal Br. 18. Thus, in considering Hausammann’s teachings as a whole, we agree with the Examiner that incorporating Hausammann’s hub end-wall contour into Ghizawi’s hub would act, at least to some degree, to redirect pressure forces on its blades 11 Appeal 2016-004278 Application 13/066,827 and thereby reduce losses. See Ans. 5. We further note that this is the same purpose Appellant discloses for the recited hub end-wall shape. See, e.g., Spec. 148. Accordingly, for the foregoing reasons, we sustain the rejection of claim 15 as being unpatentable over Ghizawi, Burton, and Hausammann. Rejection V With respect to the rejection of claim 16, Appellant relies on the arguments presented above in regard to the rejection of claim 15. Appeal Br. 19. Accordingly, for the same reasons as discussed above, we also sustain the rejection of claim 16 as being unpatentable over Ghizawi, Burton, Hausammann, and Jansen. Rejection IX With respect to the rejection of claim 26, Appellant relies on the arguments presented above in regard to the rejection of claim 15. Appeal Br. 20-23. Accordingly, for the same reasons as discussed above, we also sustain the rejection of claim 26 as being unpatentable over Ghizawi, Parsons, and Hausammann. Rejection VII Independent claim 18 recites a turbocharger wheel having a hub and a plurality of blades similarly to that of claim 1, and further requires: wherein the cross-sectional shape of each suction surface, when taken perpendicular to the flow direction, is characterized by a cropped comer extending along the shroud edge of the suction surface; and 12 Appeal 2016-004278 Application 13/066,827 wherein the cross-sectional shape of each pressurized surface, when taken perpendicular to the flow direction, is characterized by a comer that is not cropped along the shroud edge of the pressurized surface. Appeal Br. 31 (Claims App.). The Examiner finds that Ghizawi discloses a turbocharger wheel substantially as recited in claim 18, but does not explicitly disclose a cropped comer extending along the shroud edge of the suction surface. Non-Final Act. 13—14. The Examiner finds that Parsons discloses a suction surface having a cross-sectional shape perpendicular to the flow direction that includes a cropped comer extending along the shroud edge, and reasons that it would have been obvious to one of ordinary skill to include Parson’s cropped comer with Ghizawi’s blade “to reduce stress at the outer edge of the blade during operation due to friction.” Id. at 14 (citing Parsons, 1:26— 32). The Examiner explains that in embodiment “f’ of Figure 2, Parsons teaches “the radially outer edge of the blade adjacent the shroud is cropped, i.e. cutback, on the suction side only, wherein this cutback, or chamfer, is along the entire shroud edge.” Ans. 6. Appellant traverses, arguing that “Parsons fails to disclose [a] blade tip cropped on a suction side but not on a pressure side.” Appeal Br. 20. Parsons discloses a turbine blade in which the ends are narrowed to reduce skin friction between the blade and the shroud, which may be caused by the presence of a liquid (e.g., water in a steam turbine). Parsons 1:23—38. Figure 2 represents six modified cross-sections of the turbine blade. Id. at 1:91—93. In embodiment f, the convex surface of the blade includes a straight taper. Id. at 2:3 4. We note that, like Appellant’s blade, the convex 13 Appeal 2016-004278 Application 13/066,827 side of Ghizawi’s blade is the suction surface. See Ghizawi 5:13—31, Fig. 2; Spec. 133, Fig. 2. Therefore, we agree with the Examiner that Parsons teaches a cropped comer on only the suction surface of a blade. Appellant’s conclusory argument fails to apprise us otherwise. Appellant presents a new argument in the Reply Brief that was not made in the Appeal Brief. See Reply Br. 6 (regarding the use of Parson’s blade in Ghizawi’s turbine). This argument is untimely and will not be considered, as Appellant fails to show good cause as to why the argument could not have been timely presented in the Appeal Brief. See 37 C.F.R. § 41.41(b)(2). We further note that the absence of any opportunity for the Examiner to respond to this untimely argument precludes meaningful appellate review. Accordingly, for the foregoing reasons, we sustain the rejection of claim 18 and its dependent claims 19—24, which are not argued separately, as being unpatentable over Ghizawi and Parsons. Rejection II With respect to the rejection of claims 11—13, Appellant relies on the argument presented above in regard to the rejection of claim 18. Appeal Br. 15. Accordingly, for the same reasons as discussed above, we also sustain the rejection of claims 11—13 as being unpatentable over Ghizawi, Burton, and Parsons. Rejection VI With respect to the rejection of claim 17, Appellant relies on the arguments presented above in regard to the rejection of claim 18. Appeal 14 Appeal 2016-004278 Application 13/066,827 Br. 19. Accordingly, for the same reasons as discussed above, we also sustain the rejection of claim 17 as being unpatentable over Ghizawi, Burton, Hausammann, Jansen, and Parsons. Rejection VIII With respect to the rejection of claim 25, Appellant relies on the arguments presented above in regard to the rejection of claim 18. Appeal Br. 20. Accordingly, for the same reasons as discussed above, we also sustain the rejection of claim 25 as being unpatentable over Ghizawi, Parsons, and Jansen. Rejection X With respect to the rejection of claim 27, Appellant relies on the arguments presented above in regard to the rejections of claims 18 and 26. Appeal Br. 24. Accordingly, for the same reasons as discussed above, we also sustain the rejection of claim 27 as being unpatentable over Ghizawi, Parsons, Hausammann, and Jansen. DECISION The Examiner’s decision to reject claims 1—5 and 7—10 as being unpatentable over Ghizawi and Burton is affirmed as to claims 1 and 7—10 and reversed as to claims 2—5. The Examiner’s decision to reject claims 11—13 as being unpatentable over Ghizawi, Burton, and Parsons is affirmed. The Examiner’s decision to reject claim 14 as being unpatentable over Ghizawi, Burton, and Jansen is affirmed. 15 Appeal 2016-004278 Application 13/066,827 The Examiner’s decision to reject claim 15 as being unpatentable over Ghizawi, Burton, and Hausammann is affirmed. The Examiner’s decision to reject claim 16 as being unpatentable over Ghizawi, Burton, Hausammann, and Jansen is affirmed. The Examiner’s decision to reject claim 17 as being unpatentable over Ghizawi, Burton, Hausammann, Jansen, and Parsons is affirmed. The Examiner’s decision to reject claims 18—24 as being unpatentable over Ghizawi and Parsons is affirmed. The Examiner’s decision to reject claim 25 as being unpatentable over Ghizawi, Parsons, and Jansen is affirmed. The Examiner’s decision to reject claim 26 as being unpatentable over Ghizawi, Parsons, and Hausammann is affirmed. The Examiner’s decision to reject claim 27 as being unpatentable over Ghizawi, Parsons, Hausammann, and Jansen 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)(l)(iv). AFFIRMED-IN-PART 16 Copy with citationCopy as parenthetical citation