Ware v. Pratt & Whitney Aircraft Co.

20 F. Supp. 168, 1937 U.S. Dist. LEXIS 1565
CourtDistrict Court, D. Delaware
DecidedJuly 10, 1937
DocketNo. 1052
StatusPublished
Cited by1 cases

This text of 20 F. Supp. 168 (Ware v. Pratt & Whitney Aircraft Co.) 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
Ware v. Pratt & Whitney Aircraft Co., 20 F. Supp. 168, 1937 U.S. Dist. LEXIS 1565 (D. Del. 1937).

Opinion

NIELDS, District Judge.

This is a patent infringement suit by Raymond Ware, patentee and owner of the patent, against the Pratt & Whitney Aircraft Company and United Aircraft Manufacturing Corporation, defendants. The bill of complaint charges defendants with infringing claims 1, 3, and S of the Ware patent No. 1,864,384 granted June 21, 1932. The defenses are noninfringement and invalidity.

The Wright Aeronautical Corporation of Paterson, N. J., and Pratt & Whitney Aircraft Company, the latter now merged into and forming a division of United Aircraft Manufacturing Corporation, divide the business in this country in the larger sizes of aviation engines. In May, 1930, the Wright Company had an epidemic of scuffing or seizures of its pistons causing failures running as high as 1 and 4 engines and resulting in a shutdown. The problem was assigned to the company’s engineers who tried various piston designs, clearances, materials, etc. Finally, engineers Chilton and Gagg tried out a tapered part at a very slight angle to each end of the skirt of the piston. When such tapering was. adopted, 100 engines were run through without a failure and since then the scuffing and scoring of the Wright pistons and cylinders has ceased. As a result of the Chilton work, the angle of the taper adopted by the Wright Corporation at each end of the piston was one-half degree with relation to the piston side wall. That angularity has been retained ever since and is applied now to all Wright’s pistons in current production. Chilton and Gagg filed an application for patent and were called upon to file a statement of their conception date. Since their conception date was not as early as the filing date of the Ware application, no interference was declared. The Ware patent issued in June, 1932, and the application of Chilton and Gagg was rejected and abandoned. Thereafter on December 31, 1932, the Wright Company acquired a license under the Ware patent. Prior to the adoption of the taper, the practice of the Wright Company was to form a juncture of the wall surface of the piston and the end either square or by a coarse chamfer or a bevel of substantial angle all of which were ineffective for en-training oil.

Before considering what the Ware patent covers, it may be well to consider what it does not cover. What is the scope and meaning of the Ware patent? The brief and argument on behalf of plaintiff distort the patent by reading into the patent certain limitations not found there. Those limitations are:

(1) That the Ware patent has to do only with pistons for airplane engines or other “internal combustion engines of high output.”

(2) That the tapers of the Ware patent “initiate” a film of oil on which the pis[169]*169ton rides or “planes” and also “initiate” planing.

(3) That an essential feature of the taper of the Ware patent is “tangency” at the point where the taper meets the cylindrical bearing surface.

These three points are fundamental in plaintiffs argument respecting the Ware patent and may be further elaborated.

(1) We are not dealing with Chilton’s problem of aircraft engines but with the Ware patent. The title of the Ware patent is merely “Piston.” The drawings show a piston which might be any usual piston with rings at the head end and a skirt portion tapered at the top and bottom. The specification begins: “This invention relates to pistons and more particularly to the pistons of internal combustion engines of high output, although it will be apparent that the principles involved are applicable to all other mechanisms using pistons, such as reciprocating pumps and air compressors.” The patent is applicable to all kinds of pistons in all kinds of engines. The patentee says: “The object of my invention is to overcome the inherent defects of the conventional piston.” Further on he says: “The piston of Fig. 1 may be assumed to be an aluminum type automobile piston.” References to automobiles negative any limitation to airplanes. Each claim of the patent calls merely for “A piston” without specifying the material of which it is to be made or whether it is to be used in an air compressor, reciprocating pump, automobile, airplane, or other internal combustion engine.

(2) Plaintiff’s requested finding of fact No. 23 is that defendant’s pistons “initiate” planing. As to that, plaintiff’s expert testifies :

“Q. 167. With tapers of the order of magnitude about which you have testified in those charts, what would you say is the effect of such tapers in the operation of the engines containing such pistons? A. That such tapers would have an effect upon the film conditions between the piston and the cylinder surface.
“Q. 168. What effect? A. The effect of changing what you might call the hydraulic set-up or the velocity diagram.
“Q. 169. What would they do in operation, in your opinion ? A. They would tend to thicken the film, and that I think would be the greatest effect that they would have and reduce the chances of metallic contact.
“Q. 170. How would they function m comparison with the character of the taper disclosed in the Ware patent? A. Do you mean as far as the piston bearing itself is concerned ? They would have somewhat the same effect.
“Q. 171. What effect would that be? A. The effect I have just explained, an improvement in the film conditions between piston and cylinder wall.
“Q. 172. As a practical matter, what in your opinion is the difference as far as concerns the character of lubrication in providing tapers of that order and providing tapers of the order disclosed in the Ware patent? A. It would be simply one of degree.
“Q. 173. What difference in operation would it make in the functioning of the piston? A. I think the difference is of the same order of the differences that occur between different engines.
“Q. 174. What effect on the initiation of planing is had by providing a taper angularly disposed to the side wall of the piston rather than one which merges tangentially? A. I think it would be one of degree.
“Q. 175. What would be the effect in those particular pistons, 8, 9 and 10, as far as concerns the initiation of planing, in your opinion? A. They would reduce the time that the piston took to form a bearing film and generally assist at the initiation of such film.”

That a change in degree only, and not in kind, does not rise to the dignity of invention, has been decided by the courts many times. Plaintiff’s expert again emphasized on redirect examination that the Ware patent merely increased the oil film, as does the prior art, and does not initiate. He testified: “The basic objective of the Ware patent is the improvement of the film-bearing conditions between piston and cylinder.”

(3) The idea of tangency was expressly given up in the proceedings in the patent office leading to the grant of a patent and plaintiff is attempting to construe the claims to cover something which not only is not there but which was expressly given up in the prosecution of the patent. On pages 6 and 7 of the file wrapper and contents of the patent in suit are found claims which the patentee projected but which were all rejected by the patent office on patents which were cited. .We can take projected claim 1 as an example"

[170]*170“1.

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Related

Ware v. Pratt & Whitney Aircraft Co.
103 F.2d 364 (Third Circuit, 1939)

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Bluebook (online)
20 F. Supp. 168, 1937 U.S. Dist. LEXIS 1565, Counsel Stack Legal Research, https://law.counselstack.com/opinion/ware-v-pratt-whitney-aircraft-co-ded-1937.