Chandler v. Mock

150 F.2d 563, 32 C.C.P.A. 1183, 66 U.S.P.Q. (BNA) 209, 1945 CCPA LEXIS 465
CourtCourt of Customs and Patent Appeals
DecidedJune 22, 1945
DocketPatent Appeal 5000
StatusPublished
Cited by10 cases

This text of 150 F.2d 563 (Chandler v. Mock) is published on Counsel Stack Legal Research, covering Court of Customs and Patent Appeals primary law. Counsel Stack provides free access to over 12 million legal documents including statutes, case law, regulations, and constitutions.

Bluebook
Chandler v. Mock, 150 F.2d 563, 32 C.C.P.A. 1183, 66 U.S.P.Q. (BNA) 209, 1945 CCPA LEXIS 465 (ccpa 1945).

Opinion

O’CONNELL, Associate Judge.

This is an appeal by Chandler from an award of priority of invention to Mock in a decision of the Board of Interference Examiners of the United States Patent Office.

The interference involves appellant Chandler’s patent No. 2,228,000, granted January 7, 1941, on his application filed May 2, 1938, and appellee Mock’s application, Serial No. 362,572, filed October 24, 1940, as a continuation of his application, Serial No. 118,718, filed January 2, 1937.

The subject matter of the invention pertains to a carburetor and is sufficiently described in the sole count in issue, which reads:

“Fuel supply means for a throttle controlled carburetor having an air entrance *564 and a m’isture outlet connected to a super charger comprising, a source of fuel supply under pressure, pressure reducing means therefor, automatic means responsive to the absolute pressure at the discharge side of the supercharger for controlling the pressure reducing means, and automatic means responsive to the drop in pressure from the air entrance to the mixture outlet created by the throttle for controlling the pressure reducing means whereby the pressure on the fuel at the low pressure side of the pressure reducing means is responsive to the drop in pressure due to the throttle and also to the absolute pressure created by the supercharger.”

Before the Board of Interference Examiners, appellant, the junior party, sought to establish priority of conception and reduction to practice by the testimony of the witnesses Chandler, Wiegand, and Hunt relative to certain engine and “air box” tests of the device described in the issue together with records alleged to have been made contemporaneously with the running of such tests during the latter part of August and the earlier part of September, 1936. Appellee, the senior party, submitted no testimony and for conception and reduction to practice relied on the date of his original application filed on January 2, 1937.

The ’board held that while the construction of appellant’s device satisfied the requirement of the count, nevertheless his device was not only insufficiently tested to effect its reduction to practice, but also that his conduct during the critical period was lacking in diligence.

The crux of the question to be here decided is the sufficiency of the tests of the involved device. Appellant urges that its reduction to practice was amply established and offers the following citations to the record in support of his position:

“In September, 1936, Chandler’s invention was subjected to extensive tests on an engine, by F. J. Wiegand, test engineer of the Wright Aeronautical Company, at Paterson, New Jersey (R 252 — 4, Qs. 4-22). Chandler, who was present for some of the tests (R. 238 — 9, Qs. 61, 64 — 68; R. 241 — 2, Qs. 86-90), testified to the satisfactory operation of the apparatus and produced a record which he made, showing data compiled during certain of the tests (R. 239, Qs. 64-68). Wiegand testified that the apparatus operated successfully and performed the function for which it was intended (R. 254, Qs. 23 and 24). He accompanied his testimony by detailed test records which he made contemporaneously with the running of the tests (R. 255, Qs. 33-39).”

Appellant further contends that since the limitations of the count do not include an engine, reduction to practice was established also by his evidence relative to “air box” tests made at Detroit and Dayton.

It appears from the evidence introduced by appellant that the carburetor of a small aircraft engine which operates in the right side up position at low altitudes is a simple device. But as aircraft engines have increased in power and the art of flying has advanced, a multiplicity of new elements have been required to enable an aircraft engine to operate at high altitudes under all weather conditions and in an inverted position.

The preliminary statement made by Chandler and verified by him under oath in the interference proceeding discloses that he had been working in connection with airplane carburetors for aviation engines and had been experiencing certain difficulties with the performance of the engines which he thought were due to carburetion difficulties. This was the problem that confronted Chandler and according to the respective specifications of the two devices here submitted by him, Chandler sought to solve the problem of the advanced art of aviation carburetion by the invention of the device described in the count.

In his testimony, Chandler identified Exhibit 1 as a carburetor which was developed by his organization prior to the date of the invention here in issue. In the original carburetor, Exhibit 1, described as an airplane carburetor in the application of Milton J. Kittler, Serial No. 107,386, filed October 24, 1936, the fuel flow was varied under the control of supercharger pressure, but it lacked what is called “load compensation.” To improve that feature of the original carburetor, the invention here in issue, described in appellant’s application also as an airplane carburetor, was developed by Chandler to supplement the original carburetor by adding a channel suction control to the supercharger control.

The parts of the respective carburetors, Chandler testified, were structurally different, but it is noted that the carburetor here in issue was designed to function with a supercharger and the supercharger is one *565 of the elements defined in the count of the interference.

Appellee Mock urged before the Board of Interference Examiners that since the device in issue was designed to function in an airplane engine, appellant was obliged to put the carburetor to a test on an engine in an airplane. The board overruled Mock’s argument and held that the structure claimed by appellant could be applied to other engines because the count of the interference was not limited to an airplane engine. As hereinbefore stated, appellant here urges further that the count was not limited to an engine and he was therefore not required to use an engine in testing the device in order to establish its reduction to practice.

To constitute reduction to piactice of a complex mechanical device as the basis for awarding priority of invention, the law requires a preponderance of evidence in an interference proceeding to the effect that the device was subjected to a test under actual working conditions which demonstrated not that the device might work, but that it actually did work. See Jacke v. Long (Jacke v. Goldsborough), 111 F.2d 184, 27 C.C.P.A., Patents, 1147; Payne v. Hurley, 71 F.2d 208, 21 C.C.A.P.A., Patents, 1144.

The engine tests relied upon by appellant were conducted by the witness Wiegand in the plant of the Wright Aeronautical Corporation at Paterson, New Jersey. Six carburetors embodying the channel ■suction control in combination with the supercharger pressure control were constructed by Chandler’s organization and employed in making the tests. In the interference proceeding, Chandler testified that he was then unable either to locate or produce any one of the six carburetors •complete upon which the tests were run.

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150 F.2d 563, 32 C.C.P.A. 1183, 66 U.S.P.Q. (BNA) 209, 1945 CCPA LEXIS 465, Counsel Stack Legal Research, https://law.counselstack.com/opinion/chandler-v-mock-ccpa-1945.