Morse v. United States

25 F. Supp. 580, 86 Ct. Cl. 649, 1938 U.S. Ct. Cl. LEXIS 202, 1938 WL 3994
CourtUnited States Court of Claims
DecidedApril 4, 1938
DocketNo. 43055
StatusPublished

This text of 25 F. Supp. 580 (Morse v. United States) is published on Counsel Stack Legal Research, covering United States Court of Claims primary law. Counsel Stack provides free access to over 12 million legal documents including statutes, case law, regulations, and constitutions.

Bluebook
Morse v. United States, 25 F. Supp. 580, 86 Ct. Cl. 649, 1938 U.S. Ct. Cl. LEXIS 202, 1938 WL 3994 (cc 1938).

Opinion

Booth, Chief Justice,

delivered the opinion of the court:

This patent case is to be determined upon the issue of the validity or invalidity of plaintiff’s patent. If the patent is [657]*657valid, infringement is admitted. April 12,1921, the plaintiff obtained the grant of patent #1374314. Following proceedings with respect to plaintiff’s original application, the Patent Office finally allowed two of plaintiff’s five claims and upon these the plaintiff relies to establish infringement.

The two claims read as follows:

1. The method of dropping bombs from aircraft, which consists in pointing the aircraft downward when substantially over the target and in dropping a bomb while the aircraft is diving rapidly downward, whereby the bomb is dropped with a high initial velocity downward and a comparatively small velocity component in a horizontal direction.
2. The improvement in the art of dropping bombs from aircraft which consists in carrying a bomb attached to an aircraft until it is substantially over a target, then causing the aircraft to dive substantially vertically toward the target, and then detaching the bomb while the aircraft is pointed at the target, whereby the horizontal component of the bomb trajectory is substantially eliminated and the bomb is hurled with a high initial vertical velocity toward the target.

It is manifest from the above claims that the patent is a “method one.” No mechanism of any character is involved. The novelty said to reside in the method claimed consists wholly in a claimed change from the old method of approach employed in aircraft bombing toward the target intended to be hit.

The patent specifications describe in detail and at considerable length the inherent difficulties and imperfections in utilizing horizontal flights of airplanes in the process of dropping bombs intended to explode at a certain point. An airplane in horizontal flight can not drop a bomb so the latter will instantly go straight downward. The speed of the airplane naturally imparts to the bomb the moment it is released a component of velocity “approximating that of the horizontal velocity of the airplane.”

Obviously the trajectory of the bomb released as above noted will approximate a parabolic one, and will be influenced more or less in its descent by wind and other atmospheric conditions. The altitude of the airplane and its speed at the moment of release of the bomb are vital factors in as[658]*658certaining the results attendant upon effective bomb-dropping.

The aviator in order to ascertain the precise moment to release a bomb’ in horizontal flying has available what is termed a “bomb sight,” a delicate scientific instrument which may be adjusted with the speed and altitude of the airplane, and thus determines for him the moment when he should release the bomb in order to strike the target intended to be hit. The necessity for accuracy and precision in determining when to release the bomb is apparent from the fact that at no moment of release is the aviator exactly above the target to be hit.

If the bomb is released too soon it will strike ahead of the target; if too late, behind it. What we mean is diagrammatically illustrated in Fig. 1, finding 3. We need only say that aiming at a target and successfully striking it are more difficult when the instrumentality employed to discharge the bomb is in a horizontal rather than a vertical position, notwithstanding both instrumentalities are under great speed.

The plaintiff’s patent, intended to eliminate the difficulties and imperfections of releasing bombs from an airplane in horizontal flight, depends so far as invention is concerned upon a single change in the angle of flight of the airplane, i. e., from a horizontal to a vertical one, before the bomb is released by the aviator.

The specifications and claims of the patent in suit disclose that the novelty of plaintiff’s method is restricted to “pointing the aircraft downward when substantially over the target,” — in other words, converting a horizontal flight into a vertical flight before releasing the bomb. This it is claimed imparts to the bomb a minimum of velocity component in a horizontal direction and a very high degree of velocity to the bomb itself, accomplishing by this method precision in results.

Additional advantages are claimed in the elimination of instruments employed in horizontal bomb dropping, as well as the availability of the method at high altitudes out of the range of anti-aircraft guns. In fact, it is asserted that the higher the altitude of the plane the greater the velocity [659]*659imparted to the bomb, and its destructive effect is accelerated. An airplane traveling in a vertical position at great speed releases a bomb; naturally the horizontal component of velocity is eliminated, and the vertical component increased ; the time of descent is shortened and the factors of atmospheric disturbances greatly reduced.

The patent does not disclose the discovery of any new scientific principles. It was not new or novel to change the flying angle of airplanes. The plaintiff availed himself of what had long been known, and takes existing mechanisms, alters their course through the air, and insists that by so doing he has pointed out a method original in conception and novel in operativeness. While these facts do not of themselves negative invention, they are essential factors in determining whether it exists.

The plaintiff’s application contained five claims. Claim 1 was as follows:

The method of dropping bombs from aircraft, which consists in causing the aircraft to dive downward toward a target, and in dropping a bomb while the aircraft is so diving, whereby the bomb is given a high initial velocity in a downward direction.

A British patent to von Willisch in 1911 and an additional British one to Coanda in 1913 were cited by the Patent Office as anticipatory, and all five claims were rejected. Claims 1 and 3 were rejected for lack of invention. Claims 4 and 5 were directed to a combination of an airplane and a mechanism to discharge a bomb from the plane. They were rejected and not involved in this suit. The plaintiff did not cancel his claims, but insisted upon their validity, and added to his application what is now claim 1 in suit.

The application was finally rejected by the Primary Examiner, and the plaintiff appealed to what is now the Board of Appeals of the Patent Office. The Board allowed what are now claims 1 and 2 and rejected the others, deciding that inasmuch as these two claims are limited to pointing the airplane downward when substantially over the target and substantially vertical toward the same they are allowable.

The limitation placed upon the claims narrows them to such an extent that it is difficult to ascertain with any degree [660]*660of definiteness when and under what circumstances the method involved applies. Again referring to Fig. 1, finding 3, it is apparent that the airplane is in horizontal flight during the process of ascertaining its position “substantially over the target.” This portion of flight is excluded from the patent.

The patented method does not begin to function until the airplane descends vertically as far at least as is shown by fig. 7.

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Bluebook (online)
25 F. Supp. 580, 86 Ct. Cl. 649, 1938 U.S. Ct. Cl. LEXIS 202, 1938 WL 3994, Counsel Stack Legal Research, https://law.counselstack.com/opinion/morse-v-united-states-cc-1938.