Honeywell International, Inc. v. United States

596 F.3d 800, 93 U.S.P.Q. 2d (BNA) 1740, 2010 U.S. App. LEXIS 3199, 2010 WL 547908
CourtCourt of Appeals for the Federal Circuit
DecidedFebruary 18, 2010
Docket2008-5181
StatusPublished
Cited by6 cases

This text of 596 F.3d 800 (Honeywell International, Inc. v. United States) is published on Counsel Stack Legal Research, covering Court of Appeals for the Federal Circuit primary law. Counsel Stack provides free access to over 12 million legal documents including statutes, case law, regulations, and constitutions.

Bluebook
Honeywell International, Inc. v. United States, 596 F.3d 800, 93 U.S.P.Q. 2d (BNA) 1740, 2010 U.S. App. LEXIS 3199, 2010 WL 547908 (Fed. Cir. 2010).

Opinions

[803]*803Opinion for the court filed by Circuit Judge MOORE. Opinion dissenting-in-part filed by Circuit Judge MAYER.

MOORE, Circuit Judge.

Honeywell International, Inc. and Honeywell Intellectual Properties, Inc. (collectively, Honeywell) appeal from a final judgment of the U.S. Court of Federal Claims. The Court of Federal Claims held that the government infringed independent claim 2 of the patent-in-suit but that this claim is invalid. The Court of Federal Claims also held that Honeywell lacks standing on its claim for just compensation under the Invention Secrecy Act and that the first sale doctrine precludes Honeywell from recovering damages for one particular infringing system. For the reasons set forth below, we reverse and remand for a determination of damages.

BACKGROUND

The patent-in-suit is U.S. Patent No. 6,467,914 B1 (the '914 patent), and it relates to passive night vision goggles (NVGs) that are compatible with a full color display when both are used in an aircraft cockpit. See '914 patent eol.1 11.19-21, eol.2 11.1-5. NVGs operate by amplifying available light, specifically light having a relatively long wavelength (e.g., red and infrared light). See id. col.l 11.36— 38. Thus cockpit displays that emit this light, specifically red warning lights, can overwhelm NVG sensor elements and lead to disruption of vision through the NVGs. Id. col.l 11.38-41. Still, “[i]t is important that the display indicators remain illuminated, not only for the benefit of the crewmen who are not wearing [NVGs], but also because those using the goggles will typically view the instruments by looking under the goggles.” Id. col.l 11.42-46.

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Prior art solutions involved eliminating and/or dimming red and infrared light from cockpit displays. But filtration used to eliminate this light “must be very efficient because small amounts of light within the active frequency range of the [NVGs] will overwhelm the [NVGs].” Id. col.l 11.51-54. In addition, “[t]he selective filtration of light according to wavelength generally prevents the use of full color displays ... because frequencies at the lower end of the visible spectrum overlap with those frequencies which are received by the [NVGs].” Id. col.l 11.63-57. This second problem is particularly significant because it prevents the use of red warning lights, which are at the lower end of the visible spectrum, in cockpit displays. Furthermore, with respect to dimming light that is capable of overwhelming NVG sensor elements, the light must be dimmed to such a degree that it is no longer visible by crewman not wearing NVGs and by persons looking under the NVGs.

[804]*804In the 1980s, the government developed a standard governing interior cockpit lighting that also addressed the problem of NVG compatibility in cockpits having full color displays. As witnesses testified at trial, it was important for the government to retain red light in cockpits, particularly for use as warning lights. For example, Dr. Harry Lee Task, a member of the committee developing the military’s corresponding specification, testified that because red indicates warning “if at all possible the MIL spec which was in consideration should be such that it would retain red and yellow in the cockpit.” J.A. 501730 (explaining that “warning is associated with red and amber is associated with caution”). And Col. William S. Lawrence, Honeywell’s expert, testified that “red has always been perceived as the color that denotes danger and we find, as pilots and test pilots, red to be extraordinarily valuable in that role. The immediate perception of danger is crucial to survival and we want red in the cockpit.” J.A. 622806. Nevertheless, in January 1986, the government issued a military specification (MILL-85762) that prohibited the use of red light in NVG-compatible cockpits.

On October 10, 1985, Allied Corporation filed Patent Application No. 06/786,269 (the '269 application), which taught a way to continue to have red light in NVG-compatible cockpits. Pursuant to the Invention Secrecy Act, David McLure, a Naval Air Systems Command engineer, reviewed this application in March 1986 and concluded that a secrecy order should be imposed. Notably, Mr. McClure served on and eventually chaired the government committee charged with revising MIL-L-85762. After Mr. McClure reviewed the '269 application, the government revised its military specification to permit the use of red light in NVG-compatible cockpits. The PTO imposed secrecy orders on the '269 application, which prevented the patent from issuing, every year until 2000. By this time, Allied Corporation had become AlliedSignal Inc., which then merged with Honeywell Inc. to form Honeywell International, Inc. This latter entity amended the '269 application, which then issued as the '914 patent.

The invention claimed in the '914 patent permits the use of NVGs in cockpits having full color displays (including red light) without the aforementioned problems associated with the prior art. In the claimed invention, a local color display emits blue, red, and green light. A combination of filters prevents the red light from disrupting vision through the NVGs. Specifically, one filter passes only a narrowband (i.e., a narrow range of frequencies) of red light from the display; another filter at the NVG blocks that narrowband of red light and passes all other ambient red light. See '914 patent col.4 11.54-57, eol.5 11.4-8, col.5 11.13-15. Thus the narrowband of red light passed from the display does not reach (and overwhelm) the NVG sensor elements. Figure 3 of the '914 patent illustrates this combination of filters.

[805]*805[[Image here]]

Accordingly, red warning lights inside the cockpit do not disrupt vision through the NVGs, pilots can look under NVGs to view the warning lights, and crew members not wearing NVGs can see these lights as well.

In 2002, about two months after the '914 patent issued, Honeywell filed a complaint against the United States. Honeywell’s Amended Complaint seeks compensation under the Invention Secrecy Act for pre-issuance use of the invention and under 28 U.S.C. § 1498(a) for post-issuance infringement of at least independent claims 1 and 2. Relevant to this appeal, the Court of Federal Claims construed disputed claim terms, see Honeywell Int’l, Inc. v. United States, 66 Fed.Cl. 400 (2005) (Claim Construction Order), and held a trial on the issue of infringement by three accused systems: (1) the Color Multifunction Display (CMFD) and NVGs in the F-16 aircraft, (2) the Radar Display Unit (RDU) and NVGs in the C-130H aircraft, and (3) the Color Multifunction Display Unit (CMDU) and NVGs in the C-130J aircraft.1 The court determined that all three accused systems infringed claim 2— literally and under the doctrine of equivalents — but that claim 1 and claim 3, which depends from claim 2, were not infringed. See Honeywell Int’l, Inc. v. United States, 70 Fed.Cl. 424 (2006) (Infringement Order ). The Court of Federal Claims then held separate trials on Honeywell’s claim under the Invention Secrecy Act, on the government’s infringement defenses, and on damages. Ultimately, the court concluded that claim 2 is invalid under 35 U.S.C. § 103

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596 F.3d 800, 93 U.S.P.Q. 2d (BNA) 1740, 2010 U.S. App. LEXIS 3199, 2010 WL 547908, Counsel Stack Legal Research, https://law.counselstack.com/opinion/honeywell-international-inc-v-united-states-cafc-2010.