Picard v. United Aircraft Corporation

128 F.2d 632, 53 U.S.P.Q. (BNA) 563, 1942 U.S. App. LEXIS 3661, 1942 WL 37407
CourtCourt of Appeals for the Second Circuit
DecidedMay 28, 1942
Docket244
StatusPublished
Cited by135 cases

This text of 128 F.2d 632 (Picard v. United Aircraft Corporation) is published on Counsel Stack Legal Research, covering Court of Appeals for the Second Circuit primary law. Counsel Stack provides free access to over 12 million legal documents including statutes, case law, regulations, and constitutions.

Bluebook
Picard v. United Aircraft Corporation, 128 F.2d 632, 53 U.S.P.Q. (BNA) 563, 1942 U.S. App. LEXIS 3661, 1942 WL 37407 (2d Cir. 1942).

Opinions

L. PIAND, Circuit Judge.

Both parties appeal from a judgment in an action to enjoin infringement of claims 2, 3, 4, 5, 11, 14, 15, 16, 17, 18, 19 and 20 of Reissue Patent No. 21,031, originally issued on July 21, 1931, to Martin J. Schenk (No. 1,815,868)', the reissue being granted on March 34, 1939. The district judge held claims 4 and 14 — original claims— valid and infringed; he held claims 2, .3, 5, 11, 15 and 16 — likewise original claims —not infringed; and he held claims 17, 18, 19 and 20 — reissue claims — invalid because broadened over the original claims, and also .because of laches in the application. Each side appealed from so much of the judgment as went against sit. In the view we take, it will not.be necessary, to pass upon the plaintiff’s appeal, because we [634]*634think that the claims in suit are all invalid for lack of invention.

The patent was for a luhricatjng and cooling system for “radial” air-cooled combustion engines, and was primarily; -nor exclusively, intended for aeroplanes. “Radial” engines are like ordinary combustion engines except for location of the cylinders as to the driving shaft, which in ordinary engines are either set “in line” or in a V— two parallel lines, inclined to each other. In a “radial” engine the cylinders xu'e set around the driving shaft like the ,,,/okcs of a wheel — ordinarily nine in nui ’ ■ and it follows that some of then c a,re vertical — heading up or down; — some «zúlirie upwards, some are horizontal and soffi,e incline downwards. The train of elements in the patent-in-suit which operate;, the poppet valves in each cylinder starts with a cam in the crank case which engages a “cam follower” (divided into two parts), or “valve tappet.” The upper surface of the “cam follower” holds the end of. a hollow push rod — enclosed in a case- — and the upper end of the push rod abuts ‘ upon one end of a rocker-arm. The rocker-arm is journalled in a housing Oi ..box which completely .encases it; its other e>nd abuts upon the stem of the poppet valv.e, depressing it against a spring tó dislodge it from its seat in the cylinder head. Thus, by means of this train the cam in the, crank case alternately seats and unseats fife valve. All this was old in the art. r;

Oil is pumped by a standard pressure pump through passages in the “cam follower” not necessary to describe, whence it flows through the inside of the hollow push rod, oiling the joint between it and the “cam follower” as it passes. It emerges from the upper end of the push rod and enters a passage in the rocker-arm, oiling the joint between them; thence it passes through the bearing of the rocker-arm and through a passage out of its other end and into the stem of the poppet valve, oiling the joint between these. It is not necessary to describe the further course of the oil during which it cools the valve, because concededly the defendant does not use it. It is enough to say that after passing through certain'passages and a chamber in, the valve, the oil spills into the rocker-arm box. In the infringement the oil, having lubricated the joint between the end of the rocker-arm and the stem of the valve, similarly spills into the rocker-arm box. Schenk disposes of the oil so spilled by tapping into each • rocker-arm box at its lowest part a pipe which leads to a circular manifold. Since the boxes dra by gravity the manifold has to run below each, and this is accomplished by passing it between the crank case and the boxr-o h? the case of all boxes which are aboco tho level of the crank case, and below the boxes in the case of all that are below that level. The manifold drains into a sump from which a scavenging pump sucks it bacjc-to the main oil reservoir.

There was nothing new^n the train .which leads from the oiil pump to the jofet between valve stpin and the rocker-armj, That had been ,/áhown for a “radial” engiine in Scott’s Patent No. 1,321,338 in 1919,' although the /'oil did not pass beyond the' .,uc ,- the f rocker-arm. Obviously no inv ■ - '• sary to pass it to the joxt^t bci.. "i <1 iv> rocker-arm and the end of Vjhe valve s. l . Moreover, if any had.beer-i, Simes fully disclosed it for an “in line” engine in . Figure 2 of his British Patent Nq. 223,393 of 1924. However, in these disclosures the rocker-arm and its joints were exposed to the air so that the joints could, and did, gather dirt; but in the Pratt & Whitney “radial” engine the rocker-arm and its joints were housed exactly as in Schenk’s disclosure, and indeed he copied this feature from the Pratt & Whitney design.' In that engine the bearing of the rocker-arm and its joints with the ■push rod and the valve stem, were lubricated by a grease gun which had to be used periodically at intervals of from ten to ^fifteen hours of flight, and which could not -,be used during flight without difficulty and clanger. Schenk’s invention, so far as the defendant borrowed from it, can therefore be fairly stated as substituting the automatic oil feed of Scott or Simes in the Pratt & Whitney engine, and making the necessary adjustments to drain back the oiHj to the reservoir. It is in the drainage of the rocker-arm boxes that the invention, if awy, must lie.

There had never been any complete anticipation of Schenk’s method of oil disposal vn the prior art; the nearest was the Curtías R-14S4 engine about which the evidence has very largely centered. The plaintiff challenges its relevancy, first, because she denies that it is properly a part of the prior art at all; and-second, because even though it is, the step between it and Schenk’s disclosure required invention. She wishes us to disregard it because it [635]*635was only an “abandoned experiment.” The district judge thought otherwise, and so do we. Three of these engines were made under a contract with the United States Army and completed in 1925 or 1926 at a cost of over $50,000. They were to be put to a fifty hour endurance test — greater than would be demanded in service — and one of them was. The same one was later installed in a plane, though it does not definitely appear that it was ever used in flight; and in any event it was never exploited, but was taken out and placed in a museum where it was at the time of the trial, accessible to visitors- and open for examination. All three of these engines were certainly “experimental”; all three were "abandoned” if by that is meant that the model never went into production and became an historical exhibit. But that is by no means conclusive on the issue of novelty. It is true that the designer, Heron, said that the engine was not successful and that he was surprised that it “worked at all,” but he was not speaking of the lubricating system; the defects he referred to were in the crank case, crank shaft and connecting rod; these were the cause of any abandonment, and they were' remedied in the Pratt & Whitney engine. In that, however, the lubrication remained what it had been before — manual greasing —automatic oil lubrication being deferred until 1934 when “the customers squawked” for it. It is true that the plaintiff’s expert Woeltjen testified that the Curtiss engine would foul the cylinders because the suction was so arranged as not to empty the rocker-arm boxes, and perhaps that was true, though the judge made no finding on the matter. Be that as it may, the testimony does not show that the defect — if it was one — made the engine inoperative.

On this showing the engine must be considered a part of the prior art. To be patentable, an invention cannot have been “known or used by others” in this country before the inventor “invented or discovered” it. § 31,. Title 35, U.S.C.A.

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128 F.2d 632, 53 U.S.P.Q. (BNA) 563, 1942 U.S. App. LEXIS 3661, 1942 WL 37407, Counsel Stack Legal Research, https://law.counselstack.com/opinion/picard-v-united-aircraft-corporation-ca2-1942.