Fatigue Fracture Technology v. Navistar, Inc.

Court of Appeals for the Federal Circuit·Decided December 28, 2020·No. 20-1094·Unpublished

Opinion

NOTE: This disposition is nonprecedential.

United States Court of Appeals for the Federal Circuit

FATIGUE FRACTURE TECHNOLOGY, LLC, Appellant

v.

NAVISTAR, INC.,

Appellee

2020-1094

Appeal from the United States Patent and Trademark Office, Patent Trial and Appeal Board in No. IPR2018- 00853.

Decided: December 28, 2020

MEREDITH MARTIN ADDY, AddyHart P.C., Atlanta, GA, argued for appellant. Also represented by ROBERT PATRICK HART, Chicago, IL.

CRAIG D. LEAVELL, Barnes & Thornburg LLP, Chicago, IL, argued for appellee.

Before WALLACH, TARANTO, and CHEN, Circuit Judges.

2 FATIGUE FRACTURE TECHNOLOGY v. NAVISTAR, INC.

TARANTO, Circuit Judge.

Fatigue Fracture Technology, LLC (FFT) owns U.S.

Patent No. 7,143,915, which concerns processes for fracturing connecting rods. In March 2018, Navistar, Inc. sought an inter partes review of claims 1, 7, 9, and 10 of the ’915 patent. The Patent Trial and Appeal Board instituted the requested review and determined that the four claims are unpatentable on four grounds, each ground applicable to all four claims: anticipation by the Brovold patent, obviousness based on the Cavallo patent combined with the Brovold patent, obviousness based on the Cavallo patent combined with the Bayliss patent, and obviousness based on the Cavallo patent combined with the Brovold and Bayliss patents. See Navistar, Inc. v. Fatigue Fracture Tech., LLC, IPR2018-00853, 2019 WL 4126205 (P.T.A.B. Aug. 29, 2019) (Final Written Decision). On appeal, we affirm the Board’s determination of unpatentability based on Cavallo and Bayliss. We do not reach (or, therefore, either question or approve) the Board’s other unpatentability determinations .

I

A

The ’915 patent concerns connecting rods that connect the crankshaft to the piston in internal-combustion engines . A connecting rod shown in the patent and prior art has the shape of a soap-bubble wand or an unstrung tennis racket—with a linear portion and a ring-shaped head, the hollow of the ring (the bore) to hold the crankshaft. A common method for manufacturing such a connecting rod is to produce it initially in one piece, then to fracture it across the bore to form two pieces (cap and rod) that may be assembled together around the crankshaft. See J.A. 1823. An objective when designing or choosing a process for the fracturing step is to minimize plastic deformation at the split, because such deformation can make it difficult to fit the two parts back together smoothly. Id. When the parts

FATIGUE FRACTURE TECHNOLOGY v. NAVISTAR, INC. 3

do not fit back together smoothly, the result can be a defective fit between the connecting rod and crankshaft, which can cause friction-generating movement that degrades components over time or creates sparks during engine operation . See J.A. 372.

Titled “Process to Fracture Connecting Rods and the Like with Resonance-Fatigue,” the ’915 patent describes purported improvements in the fracturing process. The patent observes that many of the known methods for fracturing connecting rods rely on applying an “outward pressure” to the bore until “the generated stresses are high enough to fracture the connecting rod.” ’915 patent, col. 1, lines 30–33. The patent then notes a challenge: Because “connecting rods are made of high strength materials, the fracturing force is required to be of big magnitude,” id., col. 1, lines 39–40, but larger forces tend to produce more plastic deformation, with its undesirable results, id., col. 1, lines 41–50.

The patent proposes a solution based on applying small magnitude forces repeatedly rather than applying a large fracturing force once. Id., col. 3, lines 1–14. Specifically, the patent teaches using a cyclic force to fatigue the connecting rod, thereby creating cracks and micro-cracks, and only then fracturing the rod into two pieces by applying a dynamic force. Id., Abstract; id., col. 3, lines 16–24; id., col. 4, lines 35–43; id., col. 7, lines 20–36. Independent claim 1 is representative. It recites:

1. A process for the fracture separation of a part having a cylindrical bore passing therethrough into a first portion and a second portion, the cylindrical bore having a central axis, the part having two opposed sides proximate to the intersection of a predetermined fracture plane passing through the cylindrical bore and the part, the process including the steps of:

4 FATIGUE FRACTURE TECHNOLOGY v. NAVISTAR, INC.

a) optionally applying at least one pre-stressing force to at least one of the first portion, the second portion and said sides of said part, said at least one pre-stressing force selected from the group compr[]ising:

i) a longitudinal pre-stressing force applied to one of the first portion and the second portion relative to the other of the portion and the second portion, said longitudinal pre-stressing force being applied in a direction substantially perpendicular to said predetermined fracture plane, and ii) a lateral pre-stressing force applied to each of the opposed sides of the part, each of said lateral pre-stressing forces being applied along substantially straight line that is substantially parallel to the predetermined fracture plane and substantially perpendicular to the central axis, where at any time instant, each of the lateral pre- stressing forces being substantially equal in magnitude and acting opposite in direction to one another;

b) applying at least one fatigue force to at least one of the first portion and the second portion, said at least one fatigue force being selected from the group comprising:

i) a longitudinal cyclic force applied to one of the first portion and the second portion relative to the other of the first portion and the second portion, said longitudinal cyclic force being applied in a direction substantially perpendicular to said predetermined fracture plane, and

FATIGUE FRACTURE TECHNOLOGY v. NAVISTAR, INC. 5

ii) a lateral cyclic force applied to each of the opposed sides of the part, each of the said lateral cyclic forces being applied along a substantially straight line that is substantially parallel to the predetermined fracture plane and substantially perpendicular to the central axis, where at any time instant, each of said lateral cyclic forces being substantially equal in magnitude and acting opposite in direction to one another;

c) applying at least one dynamic force to one of the first portion and the second portion relative to the other of the first portion and the second portion, said at least one dynamic force being applied in a direction substantially perpendicular to said predetermined fracture plane, said dynamic force being applied to fracture the part into the first portion and the second portion so as to separate the first portion from the second portion substantially along said predetermined plane.

Id., col. 6, line 61, through col. 7, line 45. Claims 7, 9, and 10 depend on claim 1 and therefore incorporate all of claim 1’s limitations. FFT has not made any argument on appeal that distinguishes the dependent claims from claim 1.

B

In March 2018, Navistar filed a petition for an inter partes review of claims 1, 7, 9, and 10 of the ’915 patent. J.A. 1358–59. In its petition, Navistar challenged claim 1 on eight grounds. J.A. 1345–46. Navistar relied on three key prior-art references: U.S. Patent No. 4,754,906 (Brovold ); U.S. Patent No. 5,699,947 (Cavallo); and U.S. Patent No. 3,155,300 (Bayliss).

Brovold describes and claims a system for manufacturing a connecting rod that includes breaking it into two parts. See Brovold, col. 1, lines 6–11. Brovold discloses a 6 FATIGUE FRACTURE TECHNOLOGY v. NAVISTAR, INC.

fracturing tool that is “adaptable for either brittle fractures using one load cycle or for cycling the members to cause fatigue breaks, generally under a low number of cycles.” Id., col. 2, lines 26–33.

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