Kennametal, Inc. v. American Cutting Alloys, Inc.

77 F. Supp. 136, 77 U.S.P.Q. (BNA) 78, 1948 U.S. Dist. LEXIS 2634
CourtDistrict Court, D. Delaware
DecidedApril 2, 1948
DocketCiv. 606
StatusPublished
Cited by5 cases

This text of 77 F. Supp. 136 (Kennametal, Inc. v. American Cutting Alloys, Inc.) is published on Counsel Stack Legal Research, covering District Court, D. Delaware primary law. Counsel Stack provides free access to over 12 million legal documents including statutes, case law, regulations, and constitutions.

Bluebook
Kennametal, Inc. v. American Cutting Alloys, Inc., 77 F. Supp. 136, 77 U.S.P.Q. (BNA) 78, 1948 U.S. Dist. LEXIS 2634 (D. Del. 1948).

Opinion

LEAHY, District Judge.

Defendant’s patents in suit 1 cover the manufacture of sintered hard carbide compositions. Plaintiff manufactures hard carbide compositions for cutting tools. Controversy arose as to whether plaintiff was and is an infringer. The action is one for declaratory judgment. 28 U.S. C.A. § 400.

In its answer and opening statement defendant admitted that certain of the patents and claims are not infringed by plaintiff’s product and processes and moved to dismiss as to the same. The ruling on this motion becomes unnecessary in view of the decision to be made here.

It appears to be the case that defendant considers its patents cover broadfy all multi-carbide cutting compositions; but I think its patents are limited to certain methods claimed to be of high efficiency for making such compositions. Upon this basis the findings of infringement will be made. 2

Re. 22,207

1. Claim 1 analyzed into its elements reads:

“1. In a method of producing a hard metal composition, particularly for tool elements, containing hard and refractory carbide crystal structures of at least two different elements other than carbon selected from the (third,) fourth, fifth and sixth group of the periodic system and considerably lower melting auxiliary metal substantially of the iron group in amounts from about 3 to 22%, the steps of
“(1) preforming said structures substantially in solid solution (a) in a first cycle including a heat treatment at a temperature of about 1600° to about 2000° C. and
“(2) consolidating in a subsequent cycle the mass so obtained with the auxiliary metal admixed in powdery state (a) by heat treatment at elevated temperature up to about 1400° to about 1600° C.”

2. Claim 2, so analyzed, reads: “2. In a method of producing a hard metal composition, particularly for tool elements, containing hard and refractory carbide crystal structures of at least two different elements other than carbon selected from the (third), fourth,' fifth, and sixth group of the periodic system and considerably lower melting auxiliary metal substantially of the iron group in amounts from 3 to 22%, the steps of

“(1) forming substantially solid solutions of said structures (a) by mixing them and (b) heat-treating the mixture at a temperature of about 1600° to 2000° C„

“(2) intimately mixing the mass so obtained with the auxiliary metal in powdery state and

“(3) sintering this mixture at elevated temperature up to about 1400° to 1600° C.”

3. Claim 3 reads:

“3. In a method of producing a hard metal composition, particularly for tools or tool elements, containing in substantial amounts hard and refractory carbide crystal structures of at least two different elements other than carbon selected from the (third,) fourth, fifth and sixth group of the periodic system and considerably lower melting auxiliary metal substantially of the iron group in amounts from about 3 to 22%, the steps of
“(1) forming solid solutions of said structures (a) by mixing them and (b) heat-treating the mixture at a temperature of about 1600° to about 2000° C.,
“(2) finely powdering and intimately mixing the mass so obtained with powdered auxiliary metal,
“(3) and subsequently sintering this mixture at elevated temperature up to about 1400 to about 1600° C.”

*138 4. Qaim 4 reads:

“4. In a method of producing a hard metal composition, particularly for tool elements, the steps of
“(1) forming by heat treatment hard and refractory carbide crystal structures of carbon and at least two different elements other than carbon selected from the (third) fourth through sixth group of the periodic system (a) so that substantially carbide crystal structures are obtained homogeneously containing atoms of at least two different elements selected from said groups in addition to carbon atoms required to form carbide therewith, (b) said heat treatment extended for this purpose to a temperature of about 1600° to about 2000° C.,
“(2) comminuting and intimately admixing the carbide substance so obtained with considerably lower melting 'powdery auxiliary metal essentially of the iron group (a) in an amount of about 3 to about 22%,
“(3) and heat treating said mixture at a temperature elevated up to about 1400 to about 1600° C., (a) so that on cooling a substantially dense and tough body results.”
5. Claims 5 and 6 are similar to claim 4.
6. Claim 7 reads:
“7. In a method of producing a hard metal composition, particularly for tool elements, substantially composed of hard and refractory carbide crystal structures of at least two different elements other than carbon selected from the (third) fourth through sixth group of the periodic system and always of titanium, and considerably lower melting auxiliary metal substantially of the iron group in amounts from about 3% to 22%, the steps of
"(1) preforming by heat treatment hard and refractory carbide crystal structures of titanium carbon and at least one other element, other than carbon, selected from said groups (a) so that substantially carbide crystal structures are obtained homogeneously containing atoms of titanium and said other selected element or elements in addition to carbon atoms required to form carbide therewith, (b) said heat treatment extended for this purpose to a temperature of about 1600° to about 2000° C.,
“(2) comminuting and intimately admixing the carbide substances so obtained with powdery auxiliary metal substantially of the iron group (a) in an amount of about 3% to 22%,
“(3) shaping under pressure and
“(4) finally sintering by heat treatment said mixture at a temperature elevated up to about 1400° to 1600° C., (a) so that on cooling a substantially dense and tough body results.”
7. Claim 8 reads:
“8. In the manufacture of hard metal compositions, particularly for tool elements, by finely comminuting and admixing hard and refractory carbide crystal structures with powdery auxiliary metal essentially of the iron group in an amount of about 3% to 22%, shaping under pressure and sintering the mixture by heat treatment at a temperature elevated up to about 1400° to 1600° C.: the step of

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Bluebook (online)
77 F. Supp. 136, 77 U.S.P.Q. (BNA) 78, 1948 U.S. Dist. LEXIS 2634, Counsel Stack Legal Research, https://law.counselstack.com/opinion/kennametal-inc-v-american-cutting-alloys-inc-ded-1948.