Lombard v. Howard

213 F.2d 328, 41 C.C.P.A. 929, 102 U.S.P.Q. (BNA) 76, 1954 CCPA LEXIS 167
CourtCourt of Customs and Patent Appeals
DecidedMay 27, 1954
DocketPatent Appeal 6009
StatusPublished

This text of 213 F.2d 328 (Lombard v. Howard) 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
Lombard v. Howard, 213 F.2d 328, 41 C.C.P.A. 929, 102 U.S.P.Q. (BNA) 76, 1954 CCPA LEXIS 167 (ccpa 1954).

Opinion

WORLEY, Judge.

This is an appeal from the decision of the Board of Interference Examiners of the United States Patent Office awarding priority of invention of the subject matter embraced in two counts to appellee, the senior party herein.

The interference involves a patent to appellant, one Adrian Albert Lombard, assigned to Rolls Royce, Ltd., of England, Serial No. 2,494,821, dated January 17, 1950, on an application filed March 11, 1947 and an application of appellee, one Alan Howard, Serial No. 541,565, filed *329 June 22, 1944, assigned to the General Electric Corporation of Schenectady, New York.

The subject matter of the involved counts relates to certain supporting structures located in the after part of a turbo-jet engine. The structures are primarily designed to transmit the weight of the exhaust pipe and other parts of the engine to a forward area.

The invention is more clearly described by the counts themselves which Howard copied from two of the three claims in the Lombard patent:

“1. A gas-turbine engine comprising a compressor having a rotor and a stator casing enclosing the rotor, a turbine having a rotor coaxial with and axially-spaced from the compressor rotor and a stator casing enclosing the rotor, a driving shaft connecting the compressor rotor to the turbine rotor, a plurality of combustion chambers disposed in a ring around the said shaft to extend from the compressor toward the turbine, an exhaust unit supported from the turbine casing on the side thereof remote from the compressor, an intermediate casing surrounding the shaft within the ring of combustion chambers and secured to the compressor casing to extend towards the turbine, a ring-like casing member having formed therein a plurality of circumferentially-spaced apertures one for each combustion chamber to receive and support its outlet end, said ring-like easing member being connected to the intermediate casing and to the outer periphery of the turbine casing to transmit structural loads there between, and a plurality of nozzle-boxes one for each combustion chamber extending from the outlets of the combustion chambers to deliver the working fluid from the combustion chambers to the turbine, the walls of the nozzle-boxes being spaced from the ring-like casing member so that the latter is out of direct contact with the flow of working fluid through said nozzle boxes.
“2. A gas-turbine engine as claimed in count 1, wherein said turbine casing comprises a stationary shroud for the turbine rotor, an outer ring secured directly to said shroud, an inner ring located within and radially spaced from the outer ring, and a series of guide-blades supported between the inner and outer rings, and wherein the outer edge of said apertured ring-like casing member is connected to the outer ring by a first tubular member surrounding said nozzle-boxes and the inner edge of said apertured ringlike casing member is connected to the inner-ring by a second tubular member disposed radially inside the nozzle-boxes said apertured ring-like casing member and said first and second tubular members together forming a chamber enclosing the nozzle-boxes.”

In June 1940, 1 approximately four months after issuance of the Lombard patent and while Howard’s application was pending, the Patent Office granted Howard’s request for an interference with the patentee. Subsequently Lombard was ordered to show cause why judgment should not be rendered against him. In response Lombard moved to dissolve the interference on the ground that Howard could not make the counts. That motion was denied by the Primary Examiner. Lombard then petitioned for reconsideration. Upon reconsideration, the examiner adhered to his original views.

The Board of Interference Examiners likewise held that Howard could make the counts and in response to a petition for reconsideration, reaffirmed its holding.

In his brief here, Lombard correctly states that the sole question involved is whether the senior party Howard is entitled to make the claims which are the Counts of the interference. He relies on twelve of his original fifteen reasons of *330 appeal arid suinmárizés his' position as follows:

•' “1.- That Howard’s applicatión does not describe in writing the invention of these counts with the eer-' tainty and particularity required by-Section 4888 of the Revised Statutes, [now 35 U.S.C.A. §§ 111, 112, 162];
“2. That in Howard’s structure the apertures of his ring-like casing member-do not ‘receive’ the outlet ends of the combustion chambers; ánd
“3.' That, in any event, Howard fails to exhibit that ‘clear prior disclosure’ which is required of one who copies claims from an issued patent; and that the case presents such doubts whether these counts would be valid claims in a patent granted on the Howard application' as to require application of the rule that such doubts must be resolved' against him.”

In considering those arguments, we reproduce the pertinent portion of Howard's specification as originally filed and subsequently amended:

« * - * At its. discharge end, combustion chamber [wall] 2 casing 105 (see Fig. 8) is provided with a flange 124 which is clamped to a flange 125 by a Suitable split ring 126. Flange 125 is formed' integral with arid is carried by a combustor support ring 127 which in turn is welded to the circumference of [over] a round opening 128 in an annular plate 129. . Combustor support [Arinular] plate. 1,29 extends entirely around the áft frame [combustion ■ chamber]' structure and is provided with a circular [an] opening for each combustor support flarigé [combustion chamber wall] 127. At-its periphery, plate 129 [it] is bolted to a flange at the forward end of 'aft frame [turbine] casing 6 'as' is indicated at 130. At its inner edge, it fits around and is Welded to the end of wall 88. Or otherwise considered, there is welded to the forward end of wall 88, and the outer edges of ribs 83, a large combustion sup-r port collar 129 which’at its periphery is bolted to casing [wall] 6 at 130 and this large collar is provided with openings 128, one for each combustion chamber and over which opepings the combustor support flanges [flanged combustion chamber walls] 127 are welded. Thus cylinder [casing] 81, ribs 83 and. 83 a, nozzle diaphragm support walls 87, 88 [wall 87, wall 88,] annular plate or collar 129 and the several flanges [flanged walls] 127 form a welded [together] unitary aft frame structure.”

The application also contains detailed drawings illustrating the invention,,..

The tribunals of the Patent Office compared the Howard disclosures with the language of the counts and, in applying the well established principle of patent law that counts in an'interference should be given the broadest construction their language will support, held that Howard could make the counts. See Shultz v. Dunham, 67 F.2d 501, 21 C.C.P.A., Patents, 706.

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Bluebook (online)
213 F.2d 328, 41 C.C.P.A. 929, 102 U.S.P.Q. (BNA) 76, 1954 CCPA LEXIS 167, Counsel Stack Legal Research, https://law.counselstack.com/opinion/lombard-v-howard-ccpa-1954.