United Technologies Corp. v. Chromalloy Gas Turbine Corp.

105 F. Supp. 2d 346, 2000 U.S. Dist. LEXIS 9288, 2000 WL 875259
CourtDistrict Court, D. Delaware
DecidedJune 29, 2000
DocketCiv.A. 95-444-RRM
StatusPublished
Cited by2 cases

This text of 105 F. Supp. 2d 346 (United Technologies Corp. v. Chromalloy Gas Turbine Corp.) 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
United Technologies Corp. v. Chromalloy Gas Turbine Corp., 105 F. Supp. 2d 346, 2000 U.S. Dist. LEXIS 9288, 2000 WL 875259 (D. Del. 2000).

Opinion

OPINION

McKELVIE, District Judge.

This is a commercial dispute. Plaintiff United Technologies Corporation manufactures gas turbine engines for commercial aircraft. Defendant Chromalloy Gas Turbine Corporation repairs engines manufactured by United. In 1975, United began licensing its patented technology to Chro-malloy for use in repairing engines manufactured by United.

On July 11, 1995, United filed a complaint against Chromalloy in this court for breach of contract, patent infringement, and unfair competition and trade practices. On August 29, 1995, before answering the complaint, Chromalloy filed an action against United in Texas state court, alleging that United violated Texas antitrust law. The next day, Chromalloy filed an answer and counterclaim in this court, in which it denied United’s allegation of infringement, asserted affirmative defenses of invalidity and unenforceability, and sought a declaratory judgment of invalidi *347 ty, unenforceability and non-infringement. Chromalloy subsequently amended its pleading in this court to assert two additional counterclaims for breach of contract and one for recovery of royalty overpay-ments. The breach of contract claims in the third and fourth counterclaims are the subject of this opinion. 1

In November 1996, following a three-month trial, a Texas jury found that United had attempted to engage in monopolistic conduct in violation of Texas antitrust law. However, the Texas jury found that Chromalloy was not entitled to damages. On May 19, 1997, the Texas court denied Chromalloy’s post-trial motion for injunc-tive and declaratory relief.

On November 3, 1997, United moved for summary judgment in this court, alleging that Chromalloy’s third and fourth counterclaims for breach of a 1985 Repair Process Agreement and a 1988 Ceramic Coating Agreement were barred by claim preclusion following the Texas antitrust action. On December 10, 1997, the court denied United’s motion for summary judgment, finding that the claims and relief sought differed in the two cases.

In December 1997, the court held a seven-day bench trial on Chromalloy’s third counterclaim that United breached the Repair Process Agreement by failing to grant repair approvals and failing to provide technical data relating to the repairs. On August 14, 1998, the court issued its opinion on the third counterclaim, finding that United had breached the Repair Agreement and ordering United to perform its obligations under the agreement.

In July 1998, the court held a five-day bench trial on Chromalloy’s fourth counterclaim that United breached the Ceramic Coating Agreement by changing a product designation to avoid its obligations under the agreement. The court has not issued its decision on the fourth counterclaim.

On September 14, 1998, the court entered final judgment on the third counterclaim pursuant to Fed.R.Civ.P. 54(b), finding that its August 14,1998 order was final and immediately appealable insofar as it ordered specific performance. On the same day, United filed its notice of appeal with the U.S. Court of Appeals for the Federal Circuit. Both the Rule 54(b) judgment and the notice of appeal were limited to the repair approval portion of the third counterclaim. 2 On August 25, 1999, the Federal Circuit reversed this court’s denial of United’s motion for summary judgment and found that claim preclusion barred Chromalloy from litigating its third counterclaim in Delaware. United Techs. Corp. v. Chromalloy Gas Turbine Corp., 189 F.3d 1338, 1346 (Fed.Cir.1999).

Following the decision by the Federal Circuit, the parties filed three motions. First, United moves for post-appeal restitution in the form of a court order directing Chromalloy to return the proprietary information that United provided pursuant to the court’s August 14, 1998 order. Second, United renews its motion for a summary judgment that the fourth counterclaim and a part of the third counterclaim that was not subject to the Federal Circuit’s decision are barred by claim preclusion. Third, Chromalloy moves for findings of fact to determine which of Chromalloy’s repair approval claims in the third counterclaim are barred by claim preclusion following the Federal Circuit’s decision.

This is the court’s decision on the motions.

1. FACTUAL AND PROCEDURAL BACKGROUND

The court draws the following facts from the record of the proceedings in this mat *348 ter and from the affidavits, documents and deposition transcripts submitted by the parties.

A. The Parties

1. Plaintiff United Technologies Corporation

United is a Delaware corporation with its principal place of business in East Hartford, Connecticut. Through its Pratt & Whitney division, United manufactures gas turbine engines for commercial aircraft. United owns U.S.Patent No. 4,008,-844, which is directed to a method of repairing surface defects using metallic filler material. United also owns U.S.Patent No. 4,585,481 and Reissue No. 32,121, which are directed to overlay coatings for super-alloys.

2. Defendant Chromalloy Gas Turbine Corporation

Chromalloy is a Delaware corporation with its principal place of business in Orangeburg, New York. Through its Chro-malloy New York division, Chromalloy repairs gas turbine engines manufactured by United. Chromalloy New York was formerly known as Chromalloy Research and Technology (“CRT”).

B. Gas Turbine Engines

Gas turbine engines generate power by mixing compressed air with jet fuel, burning the resulting air-fuel mixture and expelling the burned mixture as a high temperature, high pressure gas. A gas turbine engine has several different sections, one of which is known as the high pressure turbine (“HPT”) section. The HPT section consists of two sets of “blades” and “vanes” arranged in rings or airfoils. Vanes are curved surfaces of metal that are fixed in place, and direct airflow through the engine. The airflow turns the rings of blades, which then drive other portions of the engine. Blades and vanes in the first airfoil are referred to as “first stage,” and those in the second airfoil are referred to as “second stage.”

Turbine blades are often exposed to temperatures near the melting point of the metal alloys from which the blades are manufactured. As a result, turbine blades and other parts in the HPT section tend to deteriorate quickly. In order to extend the life-span of these parts, manufacturers apply a thermal barrier coating to engine parts in the HPT section. This multi-layer coating generally includes a corrosion resistant metallic bond coat and a ceramic top coat.

Any repair of an engine part in the HPT section must comply with regulations established by the Federal Aviation Administration (“FAA”).

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105 F. Supp. 2d 346, 2000 U.S. Dist. LEXIS 9288, 2000 WL 875259, Counsel Stack Legal Research, https://law.counselstack.com/opinion/united-technologies-corp-v-chromalloy-gas-turbine-corp-ded-2000.