Application of Marvin C. Van Wanderham, Warren W. Worthley and Carl R. Comolli

378 F.2d 981, 54 C.C.P.A. 1487, 154 U.S.P.Q. (BNA) 20, 1967 CCPA LEXIS 291
CourtCourt of Customs and Patent Appeals
DecidedJune 15, 1967
DocketPatent Appeal 7781
StatusPublished
Cited by6 cases

This text of 378 F.2d 981 (Application of Marvin C. Van Wanderham, Warren W. Worthley and Carl R. Comolli) 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
Application of Marvin C. Van Wanderham, Warren W. Worthley and Carl R. Comolli, 378 F.2d 981, 54 C.C.P.A. 1487, 154 U.S.P.Q. (BNA) 20, 1967 CCPA LEXIS 291 (ccpa 1967).

Opinion

SMITH, Judge.

The issue presented is whether, in view of the facts of record, appellants’ invention relating to cryogenic liquid systems, is obvious within the meaning of 35 U.S.C. § 103. The real party in interest, by virtue of an assignment, is the National Aeronautics and Space Administration.

All three of the appealed claims were considered together. Appealed claim 22 describes a cryogenic liquid system as follows:

22. In a rocket propelled missile booster cryogenic liquid propellant flow system for uniformly supplying a cryogenic liquid propellant from a propellant storage tank to the combustion chamber in said rocket engine with minimal delay and waste of said fluid in stabilizing said uniform flow, the combination comprising:
1. conduit means for containing and directing the flow of said cryogenic liquid propellant from said tank to said rocket engine combustion chamber;
2. a thin substantially uniform layer of thermal insulating plastic material on the internal surfaces of said conduit means in contact with said cryogenic liquid propellant flowing therethrough;
3. means for producing and maintaining the flow of said cryogenic liquid propellant from said tank to said combustion chamber of said rocket engine;
4. whereby, the flow of said cryogenic liquid propellant from said tanks to said rocket engine combustion chamber is stabilized.

At the onset there is a dispute between the parties as to what precisely is appellants’ invention. For reasons developed more fully hereafter, the Patent Office terms the invention as “means to accelerate cooling of a metal by a liquid” while appellants argue it is a “cryogenic liquid propellant flow system” for missiles. No objection was made by the Patent Office as to the form of the claims or that they fail to meet the requirements of 35 U.S.C. § 112 in particularly pointing out and distinctly claiming the subject matter which *983 appellants regard as their invention. There is, therefore, no issue here as to whether the appealed claims define appellants’ invention, in accordance with section 112. Accordingly, appellants’ invention is the subject matter set forth in the appealed claims.

A second dispute arises between the parties as to what teachings were “prior art” at the time appellants made their invention. The Patent Office, in discharging its burden to show that the invention is obvious within the meaning of section 103, argues the prior art includes certain alleged admissions by appellants in their specification and the following article:

Sato, On the Effect of “Facing” on the Cooling Velocity of a Specimen During Quenching, 295th Report of the Research Institute for Iron, Steel and Other Metals, 21 Science Reports 565-74 (No. 4 1932).

We will first consider the disclosure in Sato. This article states:

A method of quenching, which has been the practice of Japanese cutlery makers for a long time, is to face the surface of the specimen to be hardened with a mixture of “tonoko” i. e. the very fine powder of a razor whetstone and water, and to dry the specimen prior to the quenching operation. This process is said to be absolutely indispensable to obtain a perfect hardening. Since “tonoko” is powdered clay slate and a bad conductor of heat, a coating of this material even though a very thin layer, may at first be thought to have the effect of preventing the quick cooling of the specimen. * * * it was confirmed [by tests] that the velocity of cooling is much greater in the case of a faced than in that of an unfaeed specimen, and that the slow cooling in the latter case is caused by the vapour film which forms on the surface of the specimen during the first period of immersion in the cooling liquid.

Sato discloses quenching specimens, the surface of which is roughened “to obtain a firm adhesion for the facing material.” This is referred to “as the standard surface condition, whether faced or unfaced, for quenching.” Sato concludes:

The present investigation may be summarized as follows:
(1) By comparing cooling curves during quenching * * * it was ascertained that a more drastic and uniform quenching may be effected in the case of specimens with facing than in the case of those without facing.
(2) An unfaced specimen heated to a high temperature, is, when quenched, at once covered with a vapour envelope given off by the cooling medium, and as the vapour is a bad conductor of heat, the cooling of the specimen is thereby greatly retarded, until the envelope begins to break and a direct contact of the specimen with the cooling medium takes place; then an abrupt increase in the cooling velocity which is indicated by a break in the temperature-time curve results.
(3) Faced specimens are never enveloped by vapour film and, therefore, their cooling is very rapid and uniform throughout the specimen. Thus, the old technique of quenching steel specimens with facing is very useful; it gives them an intense and uniform hardening.

In addition to the teachings of Sato, the examiner relied on statements in appellants’ specification as establishing facts which were known to those of ordinary skill in the art at the time the invention was made. Appellants stated:

In a cryogenic, that is extremely low temperature, liquid containing and flow system such as the rocket fuel supply system shown in Fig. 1, it is essential to cool down or lower the temperature of the cryogenic liquid containing and flow defining walls as rapidly as possible so as to stabilize the flow of cryogenic liquid to such apparatus as rocket thrust chambers and thereby stabilize the operation of such apparatus as rapidly as possible.
*984 In the past, efforts have been made to accelerate this wall cool-down time including the proper selection of cryogenic fluid and wall metal, providing heat conducting layers therebetween and so forth but none have been acceptable. * * *

Appellants discuss in the specification their invention as follows:

* * * applicants * * * have found that a marked improvement is obtained in cryogenic fluid chamber wall cool-down when an insulating layer is applied to the inner surface of the walls and that optimum efficiency is obtained when the insulating layer covers the entire wall inner surface. It has been found that the film boiling which was present in the past between the wall metal and the cryogenic liquid is prevented from becoming established by the use of this insulating layer and that a nucleate boiling is established in its place. This nucleate boiling allowed better heat transfer than the insulating film boiling between the cryogenic liquid and the walls which occurred when insulation was not used. This film seriously impeded the absorption of heat from the metal walls by the cryogenic liquid.

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378 F.2d 981, 54 C.C.P.A. 1487, 154 U.S.P.Q. (BNA) 20, 1967 CCPA LEXIS 291, Counsel Stack Legal Research, https://law.counselstack.com/opinion/application-of-marvin-c-van-wanderham-warren-w-worthley-and-carl-r-ccpa-1967.