Walter C. Alexander, Leo Nordwald and Robert P. Wanger v. Howard J. Williams, Francis R. Rogers and Basil J. Ryder

342 F.2d 466, 52 C.C.P.A. 1155
CourtCourt of Customs and Patent Appeals
DecidedMay 6, 1965
DocketPatent Appeal 7270
StatusPublished
Cited by2 cases

This text of 342 F.2d 466 (Walter C. Alexander, Leo Nordwald and Robert P. Wanger v. Howard J. Williams, Francis R. Rogers and Basil J. Ryder) is published on Counsel Stack Legal Research, covering Court of Customs and Patent Appeals primary law. Counsel Stack provides free access to over 12 million legal documents including statutes, case law, regulations, and constitutions.

Bluebook
Walter C. Alexander, Leo Nordwald and Robert P. Wanger v. Howard J. Williams, Francis R. Rogers and Basil J. Ryder, 342 F.2d 466, 52 C.C.P.A. 1155 (ccpa 1965).

Opinion

ALMOND, Judge.

This appeal by the junior party, Alexander et al., is from. a decision of the Board of Patent Interferences awarding priority of invention of the single count in issue to the senior party, Williams et al. Appellees’ application 1 was filed on April 5, 1955. Appellants’ application, 2 filed May 24, 1955, became a patent 3 on April 5, 1960. The Williams et al. application is assigned to The Bendix Corporation and the Alexander et al. patent is assigned to General Electric.

The invention involved in this interference is a system for controlling fuel flow and stator angle in a jet engine. The sole count is reproduced below.

“For use in a variable stator turbojet engine having a main fuel supply system and a rotor speed governor, a control system for controlling the main fuel supply and for positioning the compressor stator blades including: a compressor inlet temperature sensor; compressor discharge pressure sensor; fuel control means including a first cam mounted on a cam shaft, said control means being connected to said sensors and adapted to be connected to said governor and said supply system for controlling the flow of fuel to the engine as a function of compressor inlet temperature, compressor discharge pressure and rotor speed; and a variable stator blade control including a second cam mounted on said cam shaft, said variable stator control being adapted to be connected to the compressor stator blades for *467 varying the setting thereof as a funetion of rotor speed and compressor inlet temperature.”

The elements of the count are shown in the following drawing from the Alexander et al. patent:

*468 Fuel flow to the engine is governed by valve 41. The setting of valve 41 is a function of 3 variables: rotor speed, compressor inlet temperature, and compressor discharge pressure. Rotor speed causes rotation of cam shaft 51 by means of governor 17, rack 54 and spur gear 53. Compressor inlet temperature actuates bellows 52 causing axial movement of the cam shaft. Because both cams 49 and 66 are three dimensional cams, both rotation and axial movement of the cams cause movement of the cam followers. Rod 47 thus operates the fuel valve as a function of both temperature and speed. Bellows 45 further controls the valve setting as a result of compressor pressure. Cam 66 which is also positioned as a function of rotor speed and compressor inlet temperature governs the setting of variable stator blades 76.

The facts out of which this interference arose are shrouded by a heavy veil which time has drawn across the memory of the primary witnesses. One undisputed fact of great significance, we think, is that the General Electric inventors were the first to conceive the invention defined by the count. The conception occurred sometime in the latter part of 1952 as is evidenced by drawings (Alexander Exhibit 6) dated November 1952. The fuel control of the drawing was apparently necessitated by the concurrent development of the J-79 turbojet engine with variable stator blades. The J-79 differed from past models primarily by the fact that the stator blades of the compressor were movable rather than stationary. The fuel controller conceived by Alexander was designed to control both fuel flow to the engine and the angle of the variable stator blades.

General Electric apparently decided to buy the control from an experienced fuel control manufacturer rather than produce the units itself. Thus, General Electric planned to develop and produce the J-79 engine while a fuel control manufacturer was independently producing the controller.

In order to select a control supplier, General Electric met with several suppliers including Bendix in January 1953. In February 1953 Bendix made drawings of a controller supporting the count which L alleges represent an independent conception of the invention. In March Bendix was awarded the contract to supply General Electric with fuel controllers. There followed a development period of over two years during which General Electric and Bendix worked closely on the development of a controller for the J-79. During most of this time General Electric and Bendix engineers held bi-weekly meetings. This joint effort extended through 1958. The controller was apparently produced in operational form sometime during 1955. Both parties filed patent applications covering the controller in the spring of 1955.

The junior party contends that it is entitled to an award of priority on three grounds. First, General Electric claims that Williams was not an independent inventor but rather that the invention of the count was disclosed to Bendix prior to any claimed conception date by Williams. Second, it is claimed that Alexander reduced the controller to practice prior to the Bendix inventors’ filing date. Third, General Electric claims that Alexander was diligent from just prior to the entry of the Bendix inventors into the field until the filing of the Alexander application.

We will first consider the question of derivation, since it presents issues which must be resolved before the reduction to practice and diligence questions can be properly determined. In order to understand General Electric’s contentions, it is necessary to study carefully the meeting between General Electric and Bendix personnel held on January 19, 1953. The purpose of the meeting with Bendix was the same as that of the meetings held with other fuel control manufacturers, to select a supplier of the J-79 controller. The evidence establishes that General Electric did not hand Bendix a drawing of the controller it had conceived and ask them to manufacture it. Rather, General Electric attempted to take advantage of Bendix’s experience. On this point, Mr. *469 Strock, a General Electric representative at the meeting, testified:

“XQ128. Wasn’t it a fact that you intended not to influence the thinking of the vendors so that you could get as many different approaches as possible and select perhaps the best from among many different types? A. It was our intent to call out requirements that control system suppliers could not possibly know, such as the parameters that would be used and the degree of sophistication of control that was required.
“Within these boundaries it was our intention indeed not to limit the proposals because we wanted to keep an open mind relative to the various ways of accomplishing the important things that we had in mind as requirements.”

In addition to stating requirements at the meeting General Electric supplied Bendix with a document (Alexander Exhibit 1) entitled “General Objectives for Advanced Engine.” This document listed the design specifications for the controller. The fuel control is specified as a function of rotor speed, N, and compressor inlet temperature, @. It is suggested that the control should be based upon corrected speed, N //©. Compressor pressure is also specified as a means of correcting acceleration fuel flow. The inlet guide vane position is specified as a function of corrected engine speed N /\¡Q-

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Bluebook (online)
342 F.2d 466, 52 C.C.P.A. 1155, Counsel Stack Legal Research, https://law.counselstack.com/opinion/walter-c-alexander-leo-nordwald-and-robert-p-wanger-v-howard-j-ccpa-1965.