Umc Electronics Company v. The United States, Cross-Appellant

816 F.2d 647, 2 U.S.P.Q. 2d (BNA) 1465, 1987 U.S. App. LEXIS 237
CourtCourt of Appeals for the Federal Circuit
DecidedApril 15, 1987
DocketAppeal 86-522, 86-559
StatusPublished
Cited by140 cases

This text of 816 F.2d 647 (Umc Electronics Company v. The United States, Cross-Appellant) 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
Umc Electronics Company v. The United States, Cross-Appellant, 816 F.2d 647, 2 U.S.P.Q. 2d (BNA) 1465, 1987 U.S. App. LEXIS 237 (Fed. Cir. 1987).

Opinions

NIES, Circuit Judge.

UMC Electronics Company brought this action, pursuant to 28 U.S.C. § 1498(a), to recover compensation for use of its patented invention by the United States. UMC is the owner of Patent No. 3,643,513, issued February 22, 1972, by assignment from the inventor Preston Weaver. The United States Claims Court, 8 Cl.Ct. 604, 228 USPQ 396 (1985), upheld the validity of all claims (1-4) but dismissed the complaint on the ground of no infringement or, more accurately, no use of the patented invention by the United States. Both parties appeal. [649]*649We reverse the Claims Court’s holding that the patented invention was not on sale within the meaning of 35 U.S.C. § 102(b).1 Accordingly, we affirm the judgment in favor of the government, but on different grounds.

I

Background

The claimed invention is an aviation counting accelerometer (ACA), a device for sensing and for recording the number of times an aircraft has been subjected to predetermined levels of acceleration.2 The sensor component is mounted on the aircraft in a direction to measure acceleration loading and is connected electrically to the recorder component. Records produced by an ACA can indicate an aircraft’s remaining useful life and show the need for structural inspection, overhaul, or rotation to less demanding service.

The patent application which became the patent in this suit (’513) was filed on August 1, 1968. Under 35 U.S.C. § 102(b) the commercial exploitation and the state of development of the invention one year before the filing of the application for the subject invention are critical to resolution of the on-sale issue.

Prior to the late 1960’s when UMC first entered this field, the U.S. Navy had procured ACA’s from Maxson Electronics Company and from Giannini Controls Corporation. The Navy was dissatisfied with these ACA’s because they sometimes recorded data that defied common sense, failed to count accelerations, or counted accelerations that never occurred. In 1966 the Navy contacted Preston Weaver, an employee of UMC, told him of the problems with existing ACA’s and informed him of the Navy’s interest in buying improved devices. Weaver designed an accelerometer, model UMC-A, and in late 1966, UMC was awarded a contract to supply the Navy with approximately 1600 units.

In early 1967, UMC concluded that its model UMC-A would not meet the Navy’s performance specification required by its contract. Like the Maxson and Giannini ACA’s, the UMC-A accelerometer utilized, as part of its sensor, an electromechanical transducer to mechanically generate signals that indicate levels of acceleration.3 Like the Maxson and Giannini devices, the [650]*650UMC-A device sometimes counted and sometimes did not count the same acceleration load. The problem lay in the inherent frequency of the mass-spring system in the transducer. The devices could not distinguish between acceleration due to inflight maneuvers, which determines actual stress, and acceleration from other sources, e.g., windgusts or weapons release.

To prevent UMC from losing the ACA contract, Weaver began work to improve the sensor portion of an ACA and conceived his invention which uses an analog transducer in the sensor. An analog transducer electrically generates a varying signal (in contrast to the mechanically produced signal of prior devices) which can be filtered electronically to selectively remove the effects of superimposed vibrations. The Claims Court found that in April-May of 1967 Weaver built and tested an engineering prototype of his ACA containing a commercial analog transducer, a filter, a timing circuit and a voltage sensor that measured one load level. UMC sought to modify the existing contract for ACA’s to substitute an analog transducer for the electro-mechanical transducer specified in the contract, but was unsuccessful in negotiating a modification.

In late May, 1967, the Navy issued new specifications and in July, 1967, requested proposals from contractors to deliver ACA’s built to the new specification (Mil-A-22145B). Technically, the request for proposals called separately for a certain number of sensor components of an ACA system and a certain number of recorders, the two units being compatible in combination. UMC responded to the request on July 27, 1967, the final date for making a proposal, with an offer to supply $1,668,743 worth of its improved ACA (hereinafter model UMC-B). UMC represented as part of its proposal that the sensor portion “has been constructed and tested in conjunction with voltage sensing and time controlled circuitry.” In response to a Navy inquiry, on August 2, 1967, after the critical date, UMC submitted a technical proposal which described the model UMC-B in detail and included test results and schematic drawings. On August 9, 1967, UMC gave a demonstration of its device to the Navy at the UMC facility.

In early 1968 the Navy canceled the request to which the above submission of UMC was directed, and in July 1968, it issued another. The latter request eventually led to a contract with Systron-Don-ner Corporation, which company has been providing the Navy with ACA’s utilizing analog transducers since 1970.

In June, 1980, UMC filed the instant action against the United States seeking compensation (after attempting for a number of years to obtain compensation directly from the Navy) by reason of the Navy’s alleged use of its invention in the Systron-Donner ACA’s. The Claims Court upheld the validity of the patent claims, which were challenged by the government on a number of grounds, but found that the Systron-Donner ACA’s did not fall within the scope of the claims. Both parties appeal: UMC asking for reversal of the Claims Court’s finding of no infringement; the government seeking to have the claims in suit held invalid. Since we conclude that the Claims Court erred as a matter of law in holding that the claims of the ’513 patent were not invalid under section 102(b), we need discuss only that issue in detail.

II

The Claims Court Decision

The Claims Court analyzed the on-sale bar under the following three-part test set out in In re Corcoran, 640 F.2d 1331, 1333-34, 208 USPQ 867, 870 (CCPA 1981), taken from Timely Prods. Corp. v. Arron, 523 F.2d 288, 302, 187 USPQ 257, 267-68 (2d Cir.1975)4:

[651]*651(1) The complete invention claimed must have been embodied in or obvious in view of the thing offered for sale____ Complete readability of the claim on the thing offered is not required because whatever is published (or on sale) more than one year prior to the filing of a patent application becomes part of the prior art over which the claim must be patentable____
(2) The invention must have been tested sufficiently to verify that it is operable and commercially marketable.

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816 F.2d 647, 2 U.S.P.Q. 2d (BNA) 1465, 1987 U.S. App. LEXIS 237, Counsel Stack Legal Research, https://law.counselstack.com/opinion/umc-electronics-company-v-the-united-states-cross-appellant-cafc-1987.