Turbocare Division of Demag Delaval Turbomachinery Corp. v. General Electric Co.

214 F. Supp. 2d 170, 2002 U.S. Dist. LEXIS 15274, 2002 WL 1837995
CourtDistrict Court, D. Massachusetts
DecidedAugust 9, 2002
DocketCIV.A. 95-30069-MAP
StatusPublished

This text of 214 F. Supp. 2d 170 (Turbocare Division of Demag Delaval Turbomachinery Corp. v. General Electric Co.) is published on Counsel Stack Legal Research, covering District Court, D. Massachusetts primary law. Counsel Stack provides free access to over 12 million legal documents including statutes, case law, regulations, and constitutions.

Bluebook
Turbocare Division of Demag Delaval Turbomachinery Corp. v. General Electric Co., 214 F. Supp. 2d 170, 2002 U.S. Dist. LEXIS 15274, 2002 WL 1837995 (D. Mass. 2002).

Opinion

MEMORANDUM REGARDING DEFENDANT’S MOTION FOR SUMMARY JUDGMENT OF NON-INFRINGEMENT AND INVALIDITY (Docket No. 226)

PONSOR, District Judge.

I. INTRODUCTION

The plaintiff, Turbocare Division of De-mag Delaval Turbomachinery Corp. (“plaintiff’), has brought suit against General Electric Co. (“defendant”), for the alleged infringement of U.S. Patent No. 4,436,311 (“the ’311 patent”), which is directed to a shaft sealing system for fluid turbines. Defendant has moved for summary judgment of noninfringment and invalidity. The motion will be denied. Disputed issues of material fact prevent the court from concluding, as a matter of law, that defendant has not infringed the ’311 patent under the doctrine of equivalents, or that claims 1, 5, 6, and 7 of the ’311 patent are invalid.

II. STANDARD OF REVIEW

Summary judgment is proper when “the pleadings, depositions, answers to interrogatories, and admissions on file, together with affidavits, if any, show that there is no genuine issue as to any material fact and that the moving party is entitled to judgment as a matter of law.” Fed. R.Civ.P. 56(c). A “genuine” issue is one that reasonably could be resolved in favor of either party, and a “material” fact is one that affects the outcome of the suit under governing law. Anderson v. Liberty Lobby, Inc., 477 U.S. 242, 248-250, 106 S.Ct. 2505, 91 L.Ed.2d 202 (1986). “[T]he district court must view ‘the facts in the light most favorable to the non-moving party, drawing all reasonable inferences in that party’s favor.’ ” Bienkowski v. Northeastern University, 285 F.3d 138, 140 (1st Cir.2002), quoting Barbour v. Dynamics Research Corp., 63 F.3d 32, 36 (1st Cir. 1995).

The Federal Circuit has made it clear that “a district court properly may grant summary judgment on obviousness or anticipation only when the underlying factual inquiries present no lingering genuine issues.” Beckson Marine, Inc. v. NFM, Inc., 292 F.3d 718, 723 (Fed.Cir.2002) (citations omitted). Similarly, “[ijnfringement ... is a question of fact that a court is not to resolve on summary judgment unless no genuine factual issue remains.” Id. at 722. *172 “On summary judgment, the question is not the ‘weight’ of the evidence, but instead the presence of a genuine issue of material fact concerning infringement.” Contessa Food Products, Inc. v. Conagra, Inc., 282 F.3d 1370, 1376 (Fed.Cir.2002).

III. FACTUAL AND PROCEDURAL BACKGROUND

The facts in this case have been set forth at length in two related opinions by this court, see TurboCare Div. of Demag Delaval v. General Elec., 938 F.Supp. 83 (D.Mass.1996), and Turbocare Div. of Demag Delaval v. General Elec., 45 F.Supp.2d 110 (D.Mass.1999), and one opinion by the Federal Circuit. Turbo-Care Div. of Demag Delaval v. General Elec., 264 F.3d 1111 (Fed.Cir.2001). The following summary of the facts and procedural background is tailored to the ’311 patent and the issues currently before the court. Additional descriptions of the surrounding issues in the case may be found in the above cited decisions.

A. The Problem of Rubbing

The ’311 patent allegedly solved a problem that had confounded manufacturers of steam turbines since at least 1927: the problem of the turbine shaft rubbing against and damaging the shaft seal. (Docket 231 at 4). In 1927, a GE employee wrote the following in a patent application:

In connection with the operation of elastic fluid turbines, it is known that when a turbine is operating at full load, it runs more smoothly and is less likely to vibrate than when running at light load. This is because a turbine when running at full load is evenly heated and is subjected to little if any temperature and pressure changes. On the other hand, when a turbine is running at light load or is being started up, it may be subjected to changes in temperature and pressure of considerable magnitude and at such times is much more likely to operate unevenly or to vibrate.

(Docket 236, Exhibit G). As this early patent application describes, the vibration, or uneven running, that occurs when running a turbine at start-up or at light load can cause substantial damage to the shaft seal. The purpose of the shaft seal is to prevent steam leakage so that as much steam as possible is directed towards turning the rotor, and generating power. (Docket 238 at 2). When the teeth of the seal shaft become damaged by rubbing from the turbine shaft, an excessive clearance results between the shaft seal and the rotor. This affects the efficiency of the turbine because, put simply, too much clearance allows for too much steam leakage. Id. Unfortunately, the 1927 GE patent did not solve the problem of the turbine rotor rubbing against the shaft seal. Indeed, plaintiff claims, the problem went unsolved until the invention of the ’311 patent. (Docket 231 at 4-5).

The ’311 patent creator was Ronald Brandon (“Brandon”), who was a former GE employee. At first, Brandon attempted several unsuccessful solutions aimed at the problem of rubbing. However, he eventually,

thought of the idea of making the shaft seal movable so that it would move away from the rotor to a large clearance at start up and under low turbine loads, when damage by rubbing occurs, and to a small clearance position when the turbine reaches operating speeds, so that the efficiency of the turbine is maximized under normal operating conditions.

(Docket 238 at 3). The ’311 patent arose out of this simple concept.

B. The ’811 Patent

Brandon’s preferred embodiment uses S-shaped compressed springs to apply a *173 circumferential force which biases the seal ring segments towards the large clearance position. These springs maintain a large clearance position when the turbine is running at start-up, or during low load conditions, in order to save the seal rings from becoming damaged. (Docket 227, Exhibit 2).

When the turbine accelerates, the steam pressure on the seal ring segments increases. This pressure overcomes the bias of the springs towards the large clearance position, and the seal ring segments move radially inward towards the small clearance position. Thus, when the turbine is operating at a normal operating speed, the seal becomes fixed at the low clearance position. This shift reduces the amount of steam leakage during normal operating conditions and increases the passage of steam through the nozzle.

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