Application of Shao Wen Yuan

188 F.2d 377, 38 C.C.P.A. 967
CourtCourt of Customs and Patent Appeals
DecidedApril 3, 1951
DocketPatent Appeal 5776
StatusPublished
Cited by20 cases

This text of 188 F.2d 377 (Application of Shao Wen Yuan) 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 Shao Wen Yuan, 188 F.2d 377, 38 C.C.P.A. 967 (ccpa 1951).

Opinion

GARRETT, Chief Judge.

By this appeal reversal is sought of the decision of the Board of Appeals of the United States Patent Office affirming the rejection by the Primary Examiner, hereinafter referred to as the examiner, of the two claims, numbered respectively 8 and 9, remaining in the application after it, during a protracted prosecution in the Patent Office, had , been amended in various particulars, including the withdrawal of many claims. It appears that The Glenn L. Martin Company of Baltimore, Maryland, as assignee of the application, is the actual party in interest.

The application relates to alleged “new and useful improvements in Low Drag *378 Airfoil,” claim 8 being for the article and claim 9 for the method of making the article. The claims read:

“8. A high speed airfoil having low-drag characteristics at both high and low lift coefficients having a profile including a curve representing a substantial portion of the airfoil profile, which curve is obtained by computing the exact pressure distribution along the chord of the airfoil for said aerodynamic characteristics, which can be converted into velocity distribution along said chord, and from said pressure distribution and the airfoil attitude corresponding to a known optimum lift coefficient, computing the value of the rectangular coordinates on points of the curve from the equations:
“X = 2 cosh W cos 6
“Y = 2 sinh W cos 8 wherein 8 varies from it /16 to 1.94 it , the remainder of the curve in the area of the leading edge of the airfoil profile being completed by a sector of a circle tangent to the curves forming the upper and lower surfaces of the airfoil profile.
“9. A method of determining the exact airfoil profile for certain desired aerodynamic characteristics comprising computing the pressure distribution along the chord of the airfoil profile for the said aerodynamic characteristics, converting the pressure distribution along the chord into velocity distribution along the chord, from the pressure distribution, determining the airfoil attitude corresponding to the known optimum lift coefficient, and from said values of attitude and velocity distribution, determining values of necessary form parameters, converting said form parameters into the rectangular coordinates of a series of points from which substantial portions of the upper and lower curves of the airfoil profile can be obtained by means of the expression:
“X = 2 cosh W cos 8
“Y = 2 sinh W cos 8 wherein 8 varies from it/16 to 1.94 it, and completing the leading edge of the profile by a sector of a circle tangent to the curves for the upper and lower surfaces.”

The examiner rejected both claims on several distinct grounds, all of which were specifically approved by the Board of Appeals.

In the reasons of appeal accompanying-the appeal to us there are twenty-one allegations of error. Sixteen of these are-limited to allegations of error on the part of the examinee only. Three of the sixteen allege error with respect to a claim,, numbered 7, which is not before us, and' reference is made to a document which does not appear in the record. Three-others allege error on the part of the examiner in “failing to understand” appellant’s claimed invention, and one of these three says, in substance, that such failure was demonstrated by the rejection of claims 1 to 6, inclusive, in a paper wherein he discussed features not present in appellant’s application. Claims 1 to 6, inclusive, are not before us.

Of the five allegations of error on the part of the board at least two — Nos. 17 and 21 — are so general in character that they are virtually worthless as assignments of error, and that is true of many of the sixteen assignments relating to the decision of the examiner only.

We note that the brief for appellant states: “This Court is asked to find that the Board of Appeals erred in not fully considering the points of error on the part of Examiner, pointed out above, particularly the Examiner’s failure to understand the invention and his rejection of the claims.”

This appeal is from the decision of the Board of Appeals — not from that of the examiner — and there is no allegation that the board did not fully understand the application. It is noted from its decision that the allegation that the examiner did not understand the questions involved was' made before it and that the board expressed its view as follows: “ * * * Appellant states on page 7 of his brief that the-prosecution of this application clearly demonstrates that the Patent Office has not understood either the appellant’s concept or the claims thereto. From a study of appellant’s own description in the specification and the description thereof as set forth in the Examiner’s appeal .Statement,. *379 it seems to us that the Examiner has exhibited an adequate understanding of what it is that appellant is attempting to cover by his claims. In any event, if appellant believed that the Examiner’s description of the appealed subject matter was inadequate or erroneous, he should have pointed out the errors in his brief. This he has not done.”

From our study of the record in its entirety, and in the light of the brief for appellant, we are of opinion that the examiner demonstrated a comprehension of the subject matter as fully and completely as its nature admits and that the board did also.

Appellant’s difficulty, we think, is due to the character of the claims rather than to any lack of understanding on the part of the tribunals of the Patent Office concerning them. To state it differently, the claims seem to us to have been rejected because they were understood by the tribunals of the Patent Office, not because of any failure to comprehend them.

We take the following descriptive matter, which is a paraphrase of appellant’s own description, from the decision of the board:

“Appealed claim 9 relates to a method of determining an airfoil profile having certain desired aerodynamic characteristics by mathematical procedures. Claim 8 purports to be a claim to the airfoil as an article of manufacture, and the airfoil is defined in terms of the mathematical computations involved in determining the profile which will meet the specified requirements. Appellant points out that it has previously been the custom in designing airfoil profiles to select a known one having characteristics approaching those desired and to modify it in the light of experience to produce a trial profile. A model employing this trial profile is built and tested in a wind tunnel and further modified as indicated by the results of the test. This testing and modifying [referred to in appellant’s specification as ‘cut and try’ steps] may continue through several stages until a profile •sufficiently satisfactory to justify building an actual plane is obtained. After the actual plane is built and tested it may be further modified before the final profile is decided upon.

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188 F.2d 377, 38 C.C.P.A. 967, Counsel Stack Legal Research, https://law.counselstack.com/opinion/application-of-shao-wen-yuan-ccpa-1951.