Safe Flight Instrument Corp. v. Sundstrand Data Control, Inc.

706 F. Supp. 1146, 10 U.S.P.Q. 2d (BNA) 1733, 1989 U.S. Dist. LEXIS 1656, 1989 WL 15687
CourtDistrict Court, D. Delaware
DecidedFebruary 17, 1989
DocketCiv. A. 87-545 JRR
StatusPublished
Cited by3 cases

This text of 706 F. Supp. 1146 (Safe Flight Instrument Corp. v. Sundstrand Data Control, Inc.) is published on Counsel Stack Legal Research, covering District Court, D. Delaware primary law. Counsel Stack provides free access to over 12 million legal documents including statutes, case law, regulations, and constitutions.

Bluebook
Safe Flight Instrument Corp. v. Sundstrand Data Control, Inc., 706 F. Supp. 1146, 10 U.S.P.Q. 2d (BNA) 1733, 1989 U.S. Dist. LEXIS 1656, 1989 WL 15687 (D. Del. 1989).

Opinion

OPINION

ROTH, District Judge.

The plaintiff in this action, Safe Flight Instrument Corporation (“Safe Flight”), alleges that the defendant, Sundstrand Data Control, Inc. (“Sundstrand”), infringes its two patents, U.S. Patent Nos. 4,012,713 (the “’713 patent”) and 4,079,905 (the “ ’905 patent”), which cover avionic windsh-ear equipment. We denied the plaintiff’s motion for a preliminary injunction by Memorandum Opinion and Order dated August 30, 1988. The defendant has now moved for summary judgment of non-infringement of the plaintiff’s patents.

I. FACTS

Windshear, or more specifically micro-burst, describes an aviation hazard which occurs when a plane on takeoff or landing encounters violent, quick, and local shifts in wind direction. This can result in disaster if the pilot cannot compensate quickly and properly for the changing conditions. Equipment for warning of the presence of windshear can be located either on the ground or on board the aircraft.

The two Safe Flight patents in suit cover on-board systems of detecting windshear. Windshear is measured in these patents by comparing the rate of change of the instantaneous airspeed (the speed of an aircraft measured against the surrounding air) with the change in groundspeed (the speed of an aircraft measured against the earth; this change in speed is also termed “horizontal inertial acceleration”) and in the ’905 patent, by adding a downdraft angle. As the defendant explained in its Opening Brief and at oral argument, because the two patents are similarly written only claim 1 of the ’713 patent needs to be considered. If this claim is not infringed, then no claim of either patent is infringed. Defendant’s Opening Brief at 3 (D.I. 54); Transcript of January 30, 1989, Oral Argument at 12 [hereinafter Transcript] (D.I. 95). Claim 1 of the ’713 patent reads:

A system for generating a windshear signal representing the windshear condition encountered by an aircraft comprising:
*1148 means for generating a signal representing the rate of change of the instantaneous airspeed of the aircraft,
means for generating a signal representing the horizontal inertial acceleration of the aircraft,
means for subtracting the horizontal inertial acceleration signal from the rate of change of the instantaneous airspeed signal to provide a windshear signal representing windshear, and
means for processing said windshear signal to provide an indication representing the magnitude thereof.

Schematically, the Safe Flight patents generates a windshear signal according to the following basic diagram:

[[Image here]]

Affidavit of Philip A. Blythe [hereinafter Blythe Affidavit], Figure 2 (D.I. 81.2).

Sundstrand manufactures and sells several products known as Ground Proximity Warning Systems (“GPWS”). Sundstrand produces three types of GPWS that include a windshear warning capability: Part Numbers 965-0648 (“# 648”), 965-0676 (“#676”), and 965-0876 (“#876”) (collectively the “Sundstrand Parts”). Part # 648 uses one of The Boeing Company’s algorithms 1 to calculate windshear; Parts #676 and #876 use algorithms of Sundstrand's own design to calculate windshear. 2 The following basic diagram represents Sundst-rand’s commercially produced method for generating a windshear signal:

*1149 [[Image here]]

Blythe Affidavit, Figure 3 (D.I.81.2).

II. ANALYSIS

A. The Standard for Summary Judgment. Rule 56 of the Federal Rules of Civil Procedure provides the standard for summary judgment: Summary judgment should be granted when there are no genuine issues of material fact and the movant is entitled to judgment as a matter of law. Avia Group International, Inc. v. L.A. Gear California, Inc., 853 F.2d 1557, 1560 (Fed.Cir.1988) (citing Fed R.Civ.P. 56); Moeller v. Ionetics, Inc., 794 F.2d 653, 657 (Fed.Cir.1986) (same). Summary judgment is as appropriate in patent cases as in other cases. Avia Group, 853 F.2d at 1561 (citations omitted).

The burden of proving that there are no genuine issues of material fact rests on the moving party. Celotex Corp. v. Catrett, 477 U.S. 317, 323, 106 S.Ct. 2548, 2553, 91 L.Ed.2d 265 (1986). Summary judgment may be granted if there is “evidence that is merely colorable ... or [that] is not significantly probative.” Anderson v. Liberty Lobby, Inc., 477 U.S. 242, 249-50, 106 S.Ct. 2505, 2510-11, 91 L.Ed.2d 202 (1986) (citations omitted). “Factual disputes that are irrelevant or unnecessary will not be counted.” Id. at 248, 106 S.Ct. at 2510. Furthermore, reliance on mere assertions in the pleadings is not permissible. Id. There must be enough evidence to enable a reasonable jury to find for the nonmoving party on the issue for which summary judgment is sought. Id. at 249, 106 S.Ct. at 2510; Avia Group, 853 F.2d at 1560.

If the nonmoving party fails to make a sufficient showing of an essential element of the case for which that party has the burden of proof, the moving party is entitled to summary judgment as a matter of law. Liberty Lobby, 477 U.S. at 322, 106 S.Ct. at 2552. But the moving party need not “produce evidence showing the absence of a genuine issue of material fact”; it is sufficient for the moving party to demonstrate to the court that the nonmoving party’s case is not supported by the evidence. Avia Group, 853 F.2d at 1560 (quoting & citing Celotex, 477 U.S. at 325, 106 S.Ct. at 2554). Finally, it is well-settled law that in a motion for summary judgment the evidence should be viewed in a light most favorable to the nonmoving party, Adickes v. S.H. Kress & Co., 398 U.S. 144, 157, 90 S.Ct. 1598, 1608, 26 L.Ed.2d 142 (1970), and that this applies with equal force in patent actions. Avia Group, 853 F.2d at 1560; Moeller, 794 F.2d at 656 (citing SRI International v. Matsushita Electric Corp., 775 F.2d 1107, 1116 (Fed.Cir.1985) (en banc)).

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706 F. Supp. 1146, 10 U.S.P.Q. 2d (BNA) 1733, 1989 U.S. Dist. LEXIS 1656, 1989 WL 15687, Counsel Stack Legal Research, https://law.counselstack.com/opinion/safe-flight-instrument-corp-v-sundstrand-data-control-inc-ded-1989.