Ex Parte Norris et alDownload PDFPatent Trial and Appeal BoardDec 17, 201312502727 (P.T.A.B. Dec. 17, 2013) Copy Citation UNITED STATES PATENT AND TRADEMARK OFFICE ____________________ BEFORE THE PATENT TRIAL AND APPEAL BOARD ____________________ Ex parte JAMES W. NORRIS and JAMES D. HILL ____________________ Appeal 2012-001703 Application 12/502,727 Technology Center 3700 ____________________ Before: CHARLES N. GREENHUT, MICHAEL L. HOELTER, and LYNNE H. BROWNE, Administrative Patent Judges. BROWNE, Administrative Patent Judge. DECISION ON APPEAL Appeal 2012-001703 Application 12/502,727 2 STATEMENT OF THE CASE James W. Norris and James D. Hill appeal under 35 U.S.C. § 134 from the rejection of claims 10-14, 16, 18, and 19. Claims 1 and 4-9 are allowed. Claims 15, 20, and 21 are objected to as being dependent on a rejected claim. Claims 2, 3, and 17 are canceled. We have jurisdiction under 35 U.S.C. § 6(b). We AFFIRM-IN-PART and designate our affirmance as A NEW GROUND OF REJECTION pursuant to our authority under 37 C.F.R. § 41.50(b). CLAIMED SUBJECT MATTER The claims are directed to a hybrid vapor and film cooled turbine engine component. Independent claims 10 and 16 are reproduced below: 10. A hybrid cooling system for cooling a gas turbine engine component having an airfoil portion and a root portion, the system comprising: a first cooling subsystem for cooling a region at or near a leading edge of the airfoil portion, wherein the first cooling subsystem utilizes vapor cooling; and a second cooling subsystem for cooling a region at or near a trailing edge of the airfoil portion, wherein the second cooling subsystem utilizes film cooling. 16. An improvement for a vapor cooled gas turbine engine component having a leading edge and a trailing edge, and further having a condenser section and a vaporization section, the improvement comprising: Appeal 2012-001703 Application 12/502,727 3 an auxiliary cooling system for cooling a region at or near the trailing edge of the gas turbine engine component using film cooling, wherein at least a portion of a fluid used to cool the condenser section is discharged out of a plurality of openings of the auxiliary cooling subsystem, such that the fluid used for film cooling includes thermal energy transferred from the condenser section. PRIOR ART Hough Cunha US 5,201,634 US 5,634,766 Apr. 13, 1993 Jun. 3, 1997 GROUND OF REJECTION Claims 10-14, 16, 18, and 19 stand rejected under 35 U.S.C. §103(a) as being unpatentable over Hough and Cunha. OPINION Claims 16, 18 and 19 The Examiner finds that Hough discloses every element of claim 16 except for: an auxiliary cooling system for cooling a region at or near the trailing edge of the gas turbine engine component using film cooling wherein at least a portion of a fluid used to cool the condenser section is discharged out of a plurality of openings of the auxiliary cooling subsystem, such that the fluid used for film cooling includes thermal energy transferred from the condenser section. Ans. 7. The Examiner further finds that Cunha teaches: Appeal 2012-001703 Application 12/502,727 4 an auxiliary cooling system for cooling a region at or near the trailing edge of the gas turbine engine component using film cooling wherein at least a portion of a fluid used to cool the condenser section is discharged out of a plurality of openings of the auxiliary cooling subsystem (col. 12, ll. 42-45), such that the fluid used for film cooling includes thermal energy transferred from the condenser section wherein a section of the vapor cooled gas turbine engine component is separated from the auxiliary cooling system by an internal wall (W, see Figure 4 as reproduced and annotated by the examiner below) and a flow deflector (passages 176) for redirecting a fluid used to cool a portion of a vapor cooling system of the vapor cooled gas turbine engine component to the auxiliary cooling subsystem. If modified by Cunha a portion of the air that passes into the film cooling system would pass over the condenser section and absorb the thermal heat. Id. (emphasis added). Based on these findings the Examiner concludes that it would have been obvious “to modify the blade of Hough by constructing it with the trailing edge film cooling apparatus, wall and deflector of Cunha for the purpose of film cooling the trailing edge with air.” Ans. 7-8 (emphasis added). As an initial matter we note that the Examiner has not identified nor do we discern any evidence in support of the finding that Cunha describes a system wherein “at least a portion of a fluid used to cool the condenser section is discharged . . . such that the fluid used for film cooling includes thermal energy transferred from the condenser section.” Ans. 7. Accordingly, this finding is in error and Appellants’ argument that “[t]he air used for film cooling by Cunha et al. has not absorbed any thermal energy from a condenser of a vapor cycle system, or even from the disclosed steam cooling circuit” (App. Br. 17) is persuasive. Further, the Examiner’s conclusory statement that “[i]f modified by Cunha a portion of the air that passes into the film cooling system would Appeal 2012-001703 Application 12/502,727 5 pass over the condenser section and absorb the thermal heat” (Ans. 7) is unsupported by evidence or persuasive reasoning. For these reasons, we do not sustain the Examiner’s rejection of claim 16, and claims 18 and 19 which depend therefrom. Claim 10 The Examiner’s rejection of independent claim 10 over the combined teachings of Hough and Cunha is similar to the rejection of independent claim 16 discussed supra. The Examiner similarly finds that Cunha teaches: A second cooling subsystem for cooling a region at or near a trailing edge of the airfoil portion, wherein the second cooling subsystem utilizes film cooling (col. 12, ll. 43-45) wherein the fluid directed at the root portion to cool the condenser section is subsequently directed (passage 176) through the second cooling subsystem. The passage would connect to the already existing condenser cooling fluid and redirect a portion to the trailing edge. Ans. 5. The Examiner appears to have misconstrued the claim, as claim 10 does not require film cooling “wherein the fluid directed at the root portion to cool the condenser section is subsequently directed through the second cooling subsystem.” Id. Rather, claim 10 encompasses a hybrid cooling system comprising two self-contained subsystems. Thus, the Examiner interpreted the claim too narrowly by incorporating limitations which have no express basis in the claim. See In re Prater, 415 F.2d 1393, 1404-05 (CCPA 1969). Obvious must be judged in light of the objective reach of the claim. KSR v. Teleflex, 127 S. Ct. 1727, 1742 (2007). Claim 10 does not require the modification proposed by the Examiner. Upon review of the prior art relied upon to reject claim 10, we find that Cunha anticipates claim 10. Appeal 2012-001703 Application 12/502,727 6 Specifically, Cunha describes each and every limitation of claim 10 as follows with reference to Cunha’s Figure 4: 1. Cunha describes a hybrid cooling system (Abstract) for cooling a gas turbine engine component S. 2. Cunha’s gas turbine engine component S has an airfoil portion 54 and a root portion 73. 3. Cunha’s system includes a first cooling subsystem (col. 10, ll. 17- 34) for cooling a region at or near a leading edge 78 of the airfoil portion 54. 4. Cunha’s first cooling subsystem utilizes vapor (steam) cooling (col. 10, ll. 31-34). 5. Cunha’s system includes a second cooling subsystem (col. 12, ll. 1-2) for cooling a region at or near a trailing edge 80 of the airfoil portion 54. 6. In column12, lines 35-37 Cunha states that the second cooling subsystem utilizes air film cooling flow along the opposite side walls of the vane adjacent the trailing edge. Given that a disclosure that anticipates a claim under § 102 also renders the claim unpatentable under § 103, we sustain the Examiner’s rejection of claim 10. See Connell v. Sears, Roebuck, & Co., 722 F.2d 1542, 1548 (Fed. Cir. 1983) (citing In re Fracalossi, 681 F.2d 792 (CCPA 1982)) (for ‘anticipation is the epitome of obviousness.’). As our conclusion is based on findings of fact and reasoning that differs from that articulated by the Examiner, we designate our affirmance as a new ground of rejection under 37 C.F.R. § 41.50(b) to provide Appellants with a full and fair opportunity to respond to the rejection. Appeal 2012-001703 Application 12/502,727 7 Claims 11-14 Appellants argue that “[i]n contrast to having a condenser within a root, Hough explicitly teaches that heat exchanger 20 is “provided within the shank portion l3.” App. Br. 12 (citing Hough, col. 3, 11. 8-10; FIGS. 1 and 3); see also Reply Br. 3. In support of this contention, Appellants explain that: Hough distinguishes the shank from the root, and explicitly teaches away from the condenser being located in the root portion 12. Although it is acknowledged that usage of the term “root” sometimes is used very broadly, it is also well accepted in the relevant technical field to distinguish a “shank” from a more radially inward “root” that has a dovetail, fir tree, or other shape for retention purposes. (Cf. FIG. 1 of the present application). Id. In response to this argument, the Examiner notes that “Appellant states that the term root is broad and then argues that the root (12) and shank (13) are separate due to the ‘well accepted’ definition of shank in the art and the fact that a root has a fir tree section.” Ans. 11. The Examiner further notes that “Appellant has provided no documentation of this definition of shank.” Id. In the Reply Brief, Appellants proffer U.S. Pat. Nos. 5,846,054 and 6,932,570 as evidence that both “shank” and “dovetail” or “dovetail root” in a manner consistent with Appellants’ usage. We note that this use is also consistent with Hough. As the Examiner has not provided evidence to the contrary, Appellants’ argument is persuasive. In re Cortright, 165 F. 3d 1353, 1358 (Fed. Cir. 1999). “Prior art references may be ‘indicative of what all those skilled in the art generally believe a certain term means ... [and] can often help to demonstrate how a disputed term is used by those skilled in the art.’ Accordingly, the PTO's interpretation of claim terms Appeal 2012-001703 Application 12/502,727 8 should not be so broad that it conflicts with the meaning given to identical terms in other patents from analogous art.” Id. (Citations omitted). Accordingly, we do not sustain the Examiner’s rejection of claim 11, and claims 12-14 which depend therefrom. DECISION The Examiner’s rejection of claim 10 is AFFIRMED and designated as a NEW GROUND OF REJECTION under 37 C.F.R. § 41.50(b). The Examiner’s rejection of claims 11-14, 16, 18, and 19 is REVERSED. This decision contains a new ground of rejection pursuant to 37 C.F.R. § 41.50(b). 37 C.F.R. § 41.50(b) provides that “[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 that Appellants, 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 proceeding will be remanded to the Examiner. . . . (2) Request rehearing. Request that the proceeding be reheard under § 41.52 by the Board upon the same record. . . . No time period for taking any subsequent action in connection with this appeal may be extended under 37 C.F.R. § 1.136(a)(1)(iv) (2009). Appeal 2012-001703 Application 12/502,727 9 AFFIRMED-IN-PART tkl Copy with citationCopy as parenthetical citation