Wright Co. v. Herring-Curtiss Co.

177 F. 257, 1910 U.S. App. LEXIS 5302
CourtDistrict Court, W.D. New York
DecidedJanuary 3, 1910
DocketNo. 400
StatusPublished
Cited by8 cases

This text of 177 F. 257 (Wright Co. v. Herring-Curtiss Co.) is published on Counsel Stack Legal Research, covering District Court, W.D. New York primary law. Counsel Stack provides free access to over 12 million legal documents including statutes, case law, regulations, and constitutions.

Bluebook
Wright Co. v. Herring-Curtiss Co., 177 F. 257, 1910 U.S. App. LEXIS 5302 (W.D.N.Y. 1910).

Opinion

HAZEL, District Judge.

A preliminary injunction is sought herein against the defendants, the Herring-Curtiss Company and Glenn H. Curtiss, for infringement of United, States letters patent No. 821,393, granted May 22, 190(5, on application filed March 23, 1903, for improvements in a flying machine to Orville Wright and Wilbur Wright, of Dayton, Ohio, and subsequently assigned to the complainant corporation. The title to the patent is not in controversy. The bill of complaint alleges that the patentees were the first inventors of what is commonly known as a heavier than air flying machine. Such machines are sustained in their aerial movements by either one or two planes or surfaces which travel through the air in a forward ascending or descending course at an angle of incidence, and may be driven or propelled by mechanical power or force of gravity. The objects of [258]*258the inventors were to provide means for maintaining or restoring the equilibrium or lateral balance of the apparatus, to remove or repress aerial forces which tended to divert the course of the apparatus, and to provide means for guiding the machine both vertically and horizontally. The claims relied upon are the seventh, fourteenth, and fifteenth. It is sufficient to' here set forth the seventh claim, which in broad terms includes both the monoplane and biplane types of apparatus.

“(7) In a flying machine, the combination with an aeroplane, and means for simultaneously moving the lateral portions thereof into different angular relations to the normal plane of the body of the aeroplane and to each other, so as to present to the atmosphere different angles of incidence of a vertical rudder, and means whereby said rudder is caused to present to the wind that side thereof nearest the side of the aeroplane having the smaller angle of incidence and offering the least resistance to the atmosphere, substantially as described,”

The essential elements of such claims are an aeroplane or supporting surface, the lateral portions of which are capable of adjustment to attain different angles of incidence and a vertical rudder in the rear of the machine. Claims 14 and 15 include as elements a horizontal rudder which is positioned forward of the machine and means for raising and lowering it so as to present its upper or under side to the pressure of the wind. The questions of the scope of said claims, infringement, and the propriety of granting an injunction herein are contested by the defendants.

In a flying machine of the biplane type, with which we are here concerned, the aeroplanes are connected together by upright stanchions extending lengthwise on the extreme front and, rear portions thereof, and are fastened on top and bottom of the planes by universal joints so as to permit the planes or surfaces to yield to pressure and incline upward or downward at their lateral edges or marginal extremities when the cord or rope fastened to the cradle is manipulated by the aviator. This lateral yielding, warping, or distorting of. the aeroplane is the essential feature by which the equilibrium is secured. Its importance cannot be overestimated, as it is shown that long before the Wright invention a method was sought by which equilibrium in mechanical flying could be secured and maintained. Not only the conception of the idea of securing and maintaining equilibrium in the air, but the appliances — the dynamic cause to achieve the result — originated in the minds of the patentees, and took shape and form in the evidently simple method of slightly turning up and down the lateral ends or margins of the planes, thus securing different angles of incidence. The unsurmountable obstacle with which prior inventors in this art strug-gled for years was the precipitate unbalancing or upsetting of the apparatus and such prior flying machines were therefore incapable of flights with any appreciable degree of success. The affidavits indicate that the patentees did not use the means or identities of prior flying machines, but solved the problem of maintaining equilibrium or lateral and front and rear balance by the introduction of new and practical elements and became pioneers in the field of flying machines’of the so-called heavier than air type. True, some of the ele[259]*259merits of the claims were old and are shown in the prior gliding machines, but such machines without the combination which included a method of maintaining equilibrium or lateral balance were utter failures. Hence the prior patents and publications apparently do not anticipate the Wright patent, and the claims in controversy are entitled to a broad and liberal construction.

The Wright patent is unadjudicated, but such fact will not deprive the complainant of its right to enjoin infringement save where the prior art shows sufficient ground to doubt the validity of the patent. Palmer v. Wilcox Mfg. Co. (C. C.) 141 Fed. 378. But in the present case public acquiescence is claimed. It appears that machines embodying the invention in suit have made notably successful flights in France, Germany, and the United States. The first aerial flight to which the attention of the public was attracted was had at Kitty Hawk, N. C., in December, 190:5, when the Wright machine using a 12 horse power motor weighing 200 pounds demonstrated its ability to maintain its balance and readily turn to the right or left and ascend or descend. The newspapers of the country heralded as marvelous the success of the patentees, and published wide that human flight had been made possible and that the patentees were the first in the annals of the world to achieve success with a heavier than air flying machine. Public recognition of tlieir success was subsequently made by scientific institutes and academies of high repute in this country and abroad. Medals were presented to the inventors by Congress, by the republic of France and by various areonautical societies of Europe and America. Such testimonials are entitled to weight in support of the presumption of validity and the practical utility. National Co. v. New York Co. (C. C.) 46 Fed. 114; Thompson Co. v. Two Rivers (C. C.) 63 Fed. 120. Moreover, in this connection it may he instanced as bearing upon the novelty and utility of complainant’s machine that the defendant Curtiss and the affiant Herring, both officers of the defendant corporation, obtained detailed information prior to the construction of the defendant’s machine, as to experiments and pressure of wind on curved and flat planes and mode of maintaining equilibrium in flights, the former through correspondence passing between the patentees and the late Uieut. Selfridge in January, 1908, and the latter from personal observation and investigation while at the camp of the patentees at Kitty Hawk, N. C., where the earlier Wright experimental flights were conducted, and subsequently both Curtiss and Herring practically admitted that in complainant’s machine the problem of equilibrium appeared to have been solved. But in the answering affidavit Herring asserts that he had considered that the Wright invention was limited to the lateral warping of the planes, and not that it covered broadly the feature of lateral balancing. This brings me to the question of whether defendants’ machine infringes that of complainant.

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177 F. 257, 1910 U.S. App. LEXIS 5302, Counsel Stack Legal Research, https://law.counselstack.com/opinion/wright-co-v-herring-curtiss-co-nywd-1910.