Honeywell International Inc. v. Universal Avionics Systems Corp.

347 F. Supp. 2d 114, 2004 U.S. Dist. LEXIS 24246, 2004 WL 2757577
District Court, D. Delaware·Decided November 30, 2004·No. C.A.03-242-MPT·Published·Cited by 1 cases

Opinion

MEMORANDUM ORDER

THYNGE, United States Magistrate Judge.

This, isi a patent infringement case. Pending before the court is Universal Avionics Systems Corp.’s (“Universal”) Motion In Limine seeking to preclude plaintiffs Honeywell International Inc. and Honeywell Intellectual Properties Inc. (collectively “Honeywell”) from introducing expert testimony regarding alleged infringement under the doctrine of equivalents. Specifically, Universal’s motion recites: “Honeywell should be precluded from introducing any evidence of alleged infringement under the doctrine of equivalents because John Hansman, Honeywell’s technical witness, provided conclusory opinions unsupported by any analysis in his report with respect to this issue.” 1

In Graver Tank & Mfg. Co., Inc. v. Linde Air Products Co., the United States Supreme Court stated that “a patentee may invoke [the] doctrine [of equivalents] to proceed against the producer of [an allegedly infringing] device if it performs substantially the same function in substan *116 tially the same way to obtain the same result.” 2 The Federal Circuit has since “recognized the function, way, result test applied in Graver Tank.” 3 Moreover, “substantial identity must be proven with regard to all three elements of the doctrine specified in Graver Tank: function performed, means by which function is performed, and result achieved.” 4

“[T]he evidentiary requirements necessary to prove infringement under the doctrine of equivalents [include] ... the need to prove equivalency on a limitation-by-limitation basis ... [and] requirfes] equivalency to be proven with particularized testimony and linking argument.” 5 The purpose of “[t]hese evidentiary requirements [is to] assure that the fact-finder does not, under the guise of applying the doctrine of equivalents, erase a plethora of meaningful structural and functional limitations of the claim on which the public is entitled to rely in avoiding infringement.” 6 Therefore, “[i]n order to prevent the doctrine from expanding a patent’s protection beyond the scope of its claims, the Federal Circuit has warned that the application of the doctrine of equivalents should be ‘the exception ... [and] not the rule’ in patent infringement actions.” 7 The Federal Circuit has summarized the burden of establishing infringement under the doctrine of equivalents, stating that:

[A] patentee must ... provide particularized testimony and linking argument as to the “insubstantiality of the differences” between the claimed invention and the accused device or process, or with respect to the function, way, result test when such evidence is presented to support a finding of infringement under the doctrine of equivalents. Such evidence must be presented on a limitation-by-limitation basis. Generalized testimony as to the overall similarity between the claims and the accused in-fringer’s product or process will not suffice. 8

A plaintiff asserting infringement under the doctrine of equivalents “must present evidence and argument concerning the doctrine and each of its elements .... The evidence and argument on the doctrine of equivalents cannot merely be subsumed in plaintiffs case of literal infringement. ... Accordingly, the fact there was evidence and argument on literal infringement, that may also bear on equivalence,” is insufficient to demonstrate infringement under the doctrine of equivalents. 9

According to Universal, the expert reports submitted by Honeywell’s expert, *117 Dr. John Hansman, Jr., fail to meet these requirements for establishing infringement under the doctrine of equivalents.

The only claim which remains at issue in this litigation is claim 1 of U.S. Patent No. 4,914,436 (“the ’436 patent”). 10 Claim 1 contains five elements and reads as follows:

1. A system for use in an aircraft for providing an enabling envelope for a ground proximity warning system for an aircraft comprising:
[1] a first source of signals representative of the longitude and latitude of an airport;
[2] a second source of signals representative of the current longitude and latitude of said aircraft;
[3] means responsive to said first source of signals representative of the longitude and latitude of said airport and said second source of signals representative of the current longitude and latitude of said aircraft for computing the distance of said aircraft from said airport and providing an enabling envelope for enabling the warning system as a function of said distance of the aircraft with respect to said airport;
[4] a source of signals representative of the relative angular position of a particular runway with respect to the heading of the aircraft; and
[5] means responsive to said first and second sources of signals for providing a signal representative of the alignment of the aircraft with the runway by determining the angle between the runway and the heading of the aircraft.

Attached as Exhibit 2 to the Opening Expert Report of Robert John Hansman, Jr. Regarding Defendant Universal 11 is a chart detailing Hansman’s conclusions supporting his opinion that the accused Universal product infringes the ’436 patent. Hansman’s report details evidence purportedly supporting his opinion of literal infringement of Universal’s Terrain Awareness Warning System (“TAWS”) for each of the elements of claim 1 of the ’436 patent. That report makes no argument for infringement under the doctrine of equivalents with regard to the first and second limitations of the ’436 patent. 12 Hansman’s report purports to provide evidence of infringement under the doctrine of equivalents for the third, forth, and fifth elements of claim 1.

The third element of claim 1 reads:

means responsive to said first source of signals representative of the longitude and latitude of said airport and said second source of signals representative of the current longitude and latitude of said aircraft for computing the distance of said aircraft from said airport and providing an enabling envelope for enabling the warning system as a function of said distance of the aircraft with respect to said airport. 13

Free access — add to your briefcase to read the full text and ask questions with AI

Honeywell International Inc. v. Universal Avionics Systems Corp., 347 F. Supp. 2d 114, 2004 U.S. Dist. LEXIS 24246, 2004 WL 2757577 (D. Del. 2004).

347 F. Supp. 2d 114 (Honeywell International Inc. v. Universal Avionics Systems Corp.) — published by Counsel Stack Legal Research, free access to 12M+ legal documents.

Related