Sarazin v. Wright Aeronautical Corp.

54 F. Supp. 244, 60 U.S.P.Q. (BNA) 320, 1944 U.S. Dist. LEXIS 2568
CourtDistrict Court, S.D. New York
DecidedJanuary 12, 1944
StatusPublished
Cited by4 cases

This text of 54 F. Supp. 244 (Sarazin v. Wright Aeronautical Corp.) is published on Counsel Stack Legal Research, covering District Court, S.D. New York primary law. Counsel Stack provides free access to over 12 million legal documents including statutes, case law, regulations, and constitutions.

Bluebook
Sarazin v. Wright Aeronautical Corp., 54 F. Supp. 244, 60 U.S.P.Q. (BNA) 320, 1944 U.S. Dist. LEXIS 2568 (S.D.N.Y. 1944).

Opinion

BRIGHT, District Judge.

This action is brought by the patentee Sarazin and the exclusive licensee Hispano-Suiza, to enjoin an alleged infringement of two patents for “Means adapted to reduce the torsional oscillations of crank shafts”» The first (referred to during the trial as the link type), is No. 2,079,227, was applied for on July 30, 1931, and issued on May 4, 1937. The second is Reissue No. 20,773, and was originally applied for with the first. The Patent Office required a division, the application was renewed on February 29, 1936, and granted May 4, 1937, the patent issuing as No. 2,079,226. The Reissue was applied for on December 9, 1937, and granted June 28, 1938. Plaintiffs also seek an accounting and that damages be trebled, because of the alleged wanton nature of the infringement. As the basis for the latter, it is alleged that the licensee and defendant had maintained a business practice and confidential relationship which the defendant violated by its opposition in the Patent Office to the application for the reissue patent, and by entering into a contract with a concern known as APIC which restricted it in its dealings with the licensee

The claims alleged to be infringed are 11 to 16, inclusive, of the ’227 patent, and 5, 6, 8, 9, 10, 12, 13, 14, 15 and 16 of the Reissue. The claimed infringing mechanism is that used by the defendant, known as the Chilton or Wright damper, made under United States patent No. 2,112,984, granted to Roland Chilton on April 8, 1938, pursuant to his application of February 21, 1935.

The two patents in suit are directed •to the problem of reducing torsional oscillations of crank shafts. It is said to be well known that crank shafts of motors of Diessel engines, internal combustion motors and the like, having a variable speed and torque in their revolution, display in any sequence of distribution along their length inertias and resiliencies giving rise at certain velocities of revolution to torsional resonance speeds due to the harmonics of the driving torque and to the inertia of the pistons and connecting rods. The crank shaft of an engine has frequency at which it will vibrate in response to impulses delivered to it by the firing pistons. If these impulses, or torsional vibrations, become of a frequency m resonance with the natural frequency of the crank shaft, serious damage to the engine may ensue. The problem of damping, neutralizing or overcoming such vibrations in internal combustion engines of variable speeds is claimed to have been solved by Sarazin and Chilton.

It is not disputed that the solution of such damping or neutralizing as relates to machines running at fixed speeds was accomplished some time before either of the patents mentioned. The problem involved in this case relates to an engine running at variable speeds. It seems to be conceded that a damping device for a fixed speed will become ineffective and probably make the vibrations worse at speeds different than that to which it is tuned. For engines that change speeds during operation, such as those used for automobiles, airplanes, boats, etc., a problem of vibration is created that becomes more acute as the engine speed increases.

All three patents are of centrifugal pendulum devices affixed firmly to the crank shaft, to which devices are attached, or in which are contained, masses which oscillate as they revolve with the shaft, and are designed to oppose by counter vibrations the vibrations of the shaft.

Plaintiffs contend that their two patents make six important and new contributions to the art—

1. The use of a centrifugal pendulum with small friction as a vibration damper which will neutralize one order of vibration at all speeds. They define “order of vibration” as the number of vibrations per revolution, as distinquished from “frequency of vibrations”, used to indicate the number of vibrations per minute or other fixed period.

2. The use of a free bifilar pendulum so that large masses may be used and will neutralize a high order of vibration at all speeds.

3. Provide a centrifugal pendulum designed according to a specified formula, that will neutralize a pre-determined order of frequency at all speeds.

4. Provide a system which is balanced at every instant of motion so that secondary vibrations of the engine are not produced by the action of the damper.

5. Provide certain embodiments which are not influenced by gravity, and do not affect the frequency of the pendulum.

[246]*2466. Provide in the reissue patent for a roller as a friction reducing means and as means for obtaining a short radius of action.

We are concerned, thus, with an inj vention (1) of a free centrifugal bifilar pendulum damper, (2) with small friction (3) designed by formula so that it will neutralize a predetermined order of vibration at all speeds, (4) in which reduction of friction and a shorter pendulum may be obtained by the use of rollers. We are not concerned with points 4 and S. They are not urged as having been infringed, and were not.

Eight patents preceding Sarazin are cited —Frahm United States patent 989,958, April 18, 1911; Siemens-Schuckert German patent 272,575, May 21, 1911; SiemensSchuckert Austrian patent 72,077, February 1, 1916; Lanchester British patent No. 262,174, December 1, 1926; Salmson German patent 487,753, August 4, 1927; Chenard French patent 632,017, December 30, 1927; Griswold United States patent 1,874,040, applied for October 26, 1928 and issued August 30, 1932; and Carter British patent 337,466, November 3, 1930.

A reference to those patents will assist in the solution of the problem by contracting the field into which the patents in suit were born. Neutralization of vibrations is not a new thought. Application of its principle was made long before the time now under discussion. The familiar illustration of the command to marching men to break step while crossing a bridge comes readily to mind. The general principles of vibrations in bodies and their neutralization was discussed and applied by Frahm in 1911. He and many others following him, attempted to solve it by the use of springs and friction in varying degrees. His invention taught the damping or avoidance of disturbing vibrations by means of an auxiliary body, within or on the main body whose vibrations are to be damped, whose vibrations, caused by those of the main body, have as nearly as possible the same period as the main body. Thus the resonance vibration of the main body is annulled by those of the smaller auxiliary body. The fundamental principle of that invention is a pendulum to which is attached a smaller pendulum reacting 180 degrees out of phase against the primary disturbance. It is clear that pendulum neutralization, as well as the problem of tuning such neutralizer to the vibrations to be neutral-. ized, was then within the knowledge of the art. He was the first to teach the use of a mass pendulum tuned to, a fixed frequency of neutralized resonance vibrations which arise in bodies subject to periodic impacts. And his remedy was. friction.

-The Siemens-Schuckert patents are both of the same device, and in my opinion,, teach the use of a centrifugal bifilar pendulum mass which will rotate with the shaft-U-shaped tubes of liquid form a supplemental flywheel which are to be tuned “by-means of suitable dimensioning” in such a. way that precise resonance with the number of driving cycles prevails.

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Bluebook (online)
54 F. Supp. 244, 60 U.S.P.Q. (BNA) 320, 1944 U.S. Dist. LEXIS 2568, Counsel Stack Legal Research, https://law.counselstack.com/opinion/sarazin-v-wright-aeronautical-corp-nysd-1944.