Fike Corp. v. United States

41 Fed. Cl. 776, 1998 U.S. Claims LEXIS 223, 1998 WL 599137
CourtUnited States Court of Federal Claims
DecidedSeptember 8, 1998
DocketNo. 95-58C
StatusPublished
Cited by2 cases

This text of 41 Fed. Cl. 776 (Fike Corp. v. United States) is published on Counsel Stack Legal Research, covering United States Court of Federal Claims primary law. Counsel Stack provides free access to over 12 million legal documents including statutes, case law, regulations, and constitutions.

Bluebook
Fike Corp. v. United States, 41 Fed. Cl. 776, 1998 U.S. Claims LEXIS 223, 1998 WL 599137 (uscfc 1998).

Opinion

OPINION

FUTEY, Judge.

This patent case is presently before the court following a trial on the merits. Plaintiff seeks compensation from defendant for the unauthorized use of plaintiffs invention, entitled “High Reverse Pressure Resistant Low Forward Burst Pressure Rupture Disc Assembly” (rupture disc assembly).1 The rupture disc assembly at issue in this case has been used in the propulsion system of the United States Army’s Javelin missile. Defendant concedes that plaintiffs patent covers the accused device,2 but maintains that plaintiffs patent is invalid because: (1) it is both anticipated and obvious in light of prior art; and (2) plaintiff failed to disclose the best mode for constructing its patent.

Factual Background

In the late 1970’s, defendant began to seek a replacement for the Dragon missile, which by that time period, had become ineffective against the then-current tanks of the Soviet Union.3 In particular, defendant wanted to replace the Dragon with a missile that: (1) had forget and fire capabilities; (2) had a soft launch capability; and (3) would be lethal against enemy tanks.

Specifically, the forget and fire capabilities would allow an infantryman to press the firing mechanism of the launch unit and immediately take cover, thus minimizing the infantryman’s exposure to hostile fire. The soft launch capability of the missile would allow the weapon to be fired out of a fox hole, or from a covered fighting position, without injuring the infantryman. In addition, defendant desired a missile that possessed a high lethality, having the ability to climb quickly, and then dive on top of the tank where the armor is generally thinnest.

During the early 1980’s, Allegheny Ballistics Laboratory, the Aerospace Division of Hercules, Inc. (Hercules), worked with Texas Instruments on a proof of principle (POP) program where Hercules was responsible for the missile motor and Texas Instruments was responsible for the guidance and warhead portion of the missile.4 In order to [779]*779sufficiently suppress noise during firing, and at the same time provide adequate flight range for the missile, Hercules determined that the missile motor would need two separate launch and flight stages, with the launch stage having different propellant properties than the flight stage. Hercules proposed to use a rupture disc to separate the two propulsion stages while allowing propulsion gases to be discharged through a single discharge nozzle at the rear of the motor.

Hercules met with plaintiffs sales engineer regarding its need for a rupture disc to separate the flight and motor stages of the missile motor under development by Hercules. Hercules advised plaintiff that the rupture disc was required to withstand a high back pressure on the launch-side of 4500 pounds per square inch (psi), and a significantly lower burst pressure on the flight-side of approximately 1000 psi. The required withstand pressure was later increased to 7000 psi and the burst pressure reduced to 300 psi.

Plaintiff prepared a number of sketches regarding Hercules’ requirements. Among them, Sketch (SK) 747-2, sought to utilize an unsupported single-bulge disc,5 and SK 747-3, which included a single-bulged rupture disc that had a backup for the single dome surface of the disc.6 SK 747-3 disclosed four openings in the backup member to allow combustion gases to flow through the openings toward the discharge nozzle of the motor upon rupture of the disc. Plaintiff determined that these designs did not satisfy the specifications required by Hercules. In December 1982, however, James Hinrichs, plaintiffs development engineer responsible for new products, formulated a multi-bulged supported rupture disc assembly that, indeed, could withstand the demand requirements specified by Hercules.

On May 14, 1983, Mr. Hinrichs assigned his interest in the rupture disc assembly to plaintiff.7 Subsequent to this assignment, plaintiff filed an application with the Patent and Trademark Office (PTO) for a patent on the subject rupture disc assembly. On March 19, 1985, the PTO allowed all the claims as filed, and issued U.S. Patent No. 4,505,180 (the ’180 patent) to plaintiff. A copy of the ’180 patent is located in Appendix A to the court’s opinion.

The patent describes the invention as “broadly concerned with a rupture disc assembly having the characteristics of resistence to high burst pressure in one direction, while permitting rupturing under the influence of relatively low burst pressure in the opposite direction.”8 Further, the patent states that “[t]he assembly [finds] particular utility in projectiles fired from hand held weapons in order to permit staged ignition of the propellant in the projectile, so that [the] weapon can be used without fear of injuring the user.”9 The patent cautions, however, that “the disc assembly of the invention can be used in many other contexts where it is desirable to provide resistence to high burst pressure in one direction, while permitting bursting under the influence of relatively low pressures in the opposite direction.”10

Specifically, the claims of the ’180 patent include, in pertinent part:

1. A rupture disc assembly, comprising: a frangible disc presenting a low pressure face, an opposed high pressure face, and scoring on said high pressure face disposed at least partially about a rupture region for the disc; and a backing member adjacent said low pressure face, including:
web means in substantial alignment with said scoring and in close proximity to said low pressure face for preventing rupturing of said disc under the influence of relatively high burst pressures directed against said high pressure face; and structure defining an opening through said backing member for exposing an area on said low pressure face corresponding to said rupture region to burst pressures, and for rupturing of said disc along said scoring under the influence of relatively low burst [780]*780pressures directed against said low pressure face.
4. The assembly of claim 1, there being a plurality of burst regions on said disc, said backing member having an opening there-through, for each burst region.
5. The assembly of claim 4, each of said burst regions having a concavo-convex face of each portion extending into the corresponding backing member opening.

Figure 4 of the patent shows a sectional view of the rupture disc assembly:

[[Image here]]

The preferred embodiment of plaintiffs patent discloses a rupture disc assembly 22 comprising a frangible disc 26 having a low pressure face, an opposed and scored high pressure face 32, and a backing member 28 adjacent to the low pressure face. This rupture disc assembly 22 is positioned within a projectile between an initial propellant charge and a secondary propellant charge. During firing of the initial propellant charge, a relatively high burst pressure is developed in the initial charge zone, which exerts pressure against the high pressure side of the disc 32, but yet does not burst the disc 26.

The disc contains a plurality of burst regions defined by the score lines 36,38.

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

Related

Chemical Separation Technology, Inc. v. United States
51 Fed. Cl. 771 (Federal Claims, 2002)
In Re Parametric Technology Corp. Securities Litigation
300 F. Supp. 2d 206 (D. Massachusetts, 2001)

Cite This Page — Counsel Stack

Bluebook (online)
41 Fed. Cl. 776, 1998 U.S. Claims LEXIS 223, 1998 WL 599137, Counsel Stack Legal Research, https://law.counselstack.com/opinion/fike-corp-v-united-states-uscfc-1998.