Douglas Aircraft Co. v. Weeks

174 F. Supp. 442, 121 U.S.P.Q. (BNA) 559, 1959 U.S. Dist. LEXIS 3054
CourtDistrict Court, District of Columbia
DecidedJune 10, 1959
DocketCiv. A. No. 905-57
StatusPublished
Cited by2 cases

This text of 174 F. Supp. 442 (Douglas Aircraft Co. v. Weeks) is published on Counsel Stack Legal Research, covering District Court, District of Columbia primary law. Counsel Stack provides free access to over 12 million legal documents including statutes, case law, regulations, and constitutions.

Bluebook
Douglas Aircraft Co. v. Weeks, 174 F. Supp. 442, 121 U.S.P.Q. (BNA) 559, 1959 U.S. Dist. LEXIS 3054 (D.D.C. 1959).

Opinion

SIRICA, District Judge.

This is an action under 35 U.S.C.A. § 145 to obtain authorization from this Court for the Commissioner of Patents to issue to the plaintiffs letters patent on their application, Serial No. 316,325 filed October 22, 1952 and entitled “Phos-phonate Ester Hydraulic Fluid”. The claims deal with a composition of matter or a new and useful improvement thereof consisting of a hydraulic fluid designed to meet specifications for use in modern aircraft hydraulic systems and involving exposure to both high and very low temperatures. Both the Patent Office Examiner and the Patent Office Board of Appeals ruled that the plaintiffs’ claims were not patentable since their subject matter had been described in a patent granted to Watson, No. 2,636,862, on April 28, 1953 based on an application filed June 9, 1950.

Some of the important characteristics of an effective hydraulic fluid for use in aircraft should be mentioned. Viscosity should be reasonably high at high temperatures and, on the other hand, not too low at low temperatures. In addition, the rate of change of viscosity in relation to changes in temperature or “viscosity index” should also be low. Other desirable qualities are: a low pour point so that the fluid will flow at low temperatures ; low volatility within the range of temperatures usually met with to avoid evaporation; lubricity or capability of acting as a lubricant, as well as chemical stability, noninflammability (low autoge-nous ignition temperature) and inertness. As a means of meeting these specifications, plaintiffs claim the following (Cf. p. 34, plaintiffs’ Ex. 16):

“8. The composition consisting essentially of dibutyl phenyl phos-phonate and a sufficient proportion of a poly alkyl methacrylate the alkyl groups of which have from 4 to 6 carbon atoms and said poly alkyl methacrylate has an average molecular weight within the range of 2,000 to 12,000 and a molecular weight range of 1,500 to 14,000 to increase the viscosity of the composition at 210° F. above 3.0 centistokes and to increase the viscosity index of the composition above 150, said composition having a viscosity at -40° F. below 1000 centistokes and an au-togenous ignition temperature above 1000° F.
“3. The composition as defined in claim 8 in which said poly alkyl methacrylate is poly butyl methacry-late.
“4. The composition as defined in claim 8 in which said poly alkyl methacrylate is poly amyl methacry-late.
“5. The composition as defined in claim 8 in which said poly alkyl methacrylate is poly hexyl meth-acrylate.
“7. The composition as defined in claim 8 having from 0.2 to 10 per cent of said poly alkyl methacry-late.”

Thus, plaintiffs’ claims consist of one independent claim (8), and four limited, dependent claims (3, 4, 5 and 7).

The Watson patent is entitled “Lubricant and Hydraulic Fluid Compositions” and pertains, as it states in column 1:

“ * * * to compositions containing one or more organic phosphorus containing compounds, e. g., organic phosphates, phosphonates, phosphinates, etc., and a combination of additives which produce stable, non-corrosive compositions, such as improved fluids especially suitable for use as lubricants and in hydraulic mechanisms, particularly aircraft hydraulic apparatus.”

In column 3 of the Watson patent there is the following reference to a phosphorus-containing compound as part of a list of such compounds: “a mixed alkyl aryl phosphonate, for example an alkyl aromatic phosphonate such as dioc-[444]*444tyl styrene phosphonate”. These phosphorus-containing compounds form the principal ingredients of the fluids described by Watson. In order to improve viscosity characteristics, it is stated in Watson that several viscosity-index im-provers are usually added to the main ingredient.- Special reference is made in column 6 to “polymerized methaerylic acid esters” as being suitable additives to improve the viscosity-index of the phosphorus compounds.

Thus in the application of plaintiffs, the basic compound is “dibutyl phenyl phosphonate” and in'Watson there is reference to a “mixed alkyl aryl phospho-nate such as dioctyl styrene phospho-nate”. With reference to the viscosity-index improver, Watson mentions “polymerized methaerylic acid esters” with the preferable weight range of the molecules being from 5,000 to 15,000, whereas plaintiffs rely on a poly(merized) alkyl methacrylate (ester of methaerylic acid) with 4 to 6 carbon atoms in the alkyl groups and a molecular weight range from 1,500 to 14,000.

The position of the defendant, in essence, is that Watson teaches that phos-phonate compounds form a sound basic material in aircraft hydraulic fluids and that viscosity-index improving agents are usually added to them, such as polymerized esters of methaerylic acid. Within the scope of this teaching, defendant contends, lies the particular combination claimed by plaintiffs; namely, one particular phosphonate plus one particular polymerized methacrylate. As the Patent Office examiner stated in his ruling dated July 21, 1953:

“No invention resides in determining that specific compounds embraced within the genus have the property attributed to the genus by the prior art. In the absence of unusual and unexpected results, no invention is seen in applicants particular selection.”

In answer to this ruling, plaintiffs argued that Watson’s disclosures are so broad as to include thousands of possible compounds and that nowhere in Watson was the specific combination of dibutyll phenyl .phosphonate plus poly alkyl meth-acrylate disclosed. After reconsideration, the examiner stated in his communication of January 24, 1955, that his ruling did not mean that plaintiffs” claimed compounds lacked novelty but, that they did not constitute invention ia view of Watson’s references to the general classes of phosphonate and meth-acrylate compounds. It is the examiner’s ruling that the selection of particular compounds from these classes to accomplish a result contemplated by Watson would be obvious to one skilled in the art of hydraulic fluids. By means of affidavits, plaintiffs sought to bring to the-attention of the Board of Appeals of the-Patent Office the results of experiments that revealed that certain methacrylate-compounds other than those specified by plaintiff were not even soluble in dibutyi phenyl phosphonate, thus, indicating-that if one followed Watson’s suggestions, unfavorable results would follow rather than the success met with by plaintiff. In affirming the decision of the examiner the Board of Appeals stated on page 59 of plaintiffs’ Ex. 16:

“ * * * Moreover, while the affidavits may establish that certain selected poly alkyl methacrylates are incompatible with dibutyl phenyl phosphonate, they do not at the same time show what effect these meth- ■ acrylates have when added to the ‘ specific mixed alkyl aromatic phos-phonate disclosed by Watson, namely, dioctyl styrene phosphonate.” (Emphasis supplied.)

In order to satisfy this requirement,, plaintiffs made efforts to obtain a quantity of the above compound for testing. It was learned that by itself, as well as-in combination with a polymerized meth-aerylic acid ester, the suggested compound was in a solid state at -40° F.

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174 F. Supp. 442, 121 U.S.P.Q. (BNA) 559, 1959 U.S. Dist. LEXIS 3054, Counsel Stack Legal Research, https://law.counselstack.com/opinion/douglas-aircraft-co-v-weeks-dcd-1959.