Surgical implant and alloy for use in making an implant

Claim 2

Implant for bone, joint or dental surgery consisting essentially of a worked and heat-treated alloy composition having full tissue compatibility and a tensile strength of not less than about 100 kg/mm 2 and fatigue strength of at least about 40 kg/mm 2 , said alloy composition consisting essentially of: i. a first component constituting about 3% to about 30% by weight of said alloy composition, said first component consisting essentially of not less than one member selected from the group consisting of niobium, tantalum, chromium, molybdenum, aluminum; and the balance ii. a second component of said alloy composition consisting essentially of not less than one member selected from the group consisting of titanium and zirconium; wherein the sum of the weights of chromium, molybdenum, and aluminum in said alloy composition amounts to at least 20% by weight of said alloy composition, and the weight of zirconium therein amounts to not more than 75% by weight of said alloy composition; said alloy composition being free from copper, cobalt, nickel, vanadium and tin, apart from the usual impurities.

Claim 3

Implant according to claim 1, wherein said implant is a device for internal fixation.

Claim 4

Implant according to claim 2, wherein said device comprises a plate for securing bone fragments together.

Claim 5

Implant according to claim 3, wherein said plate has at least one opening therethrough for a securement device.

Claim 6

Implant according to claim 2, wherein said device comprises a screw.

Claim 7

Implant according to claim 2, wherein said device comprises a nail or pin.

Claim 8

Implant according to claim 6, wherein said device has at least one opening therethrough for a securement devive.

Claim 9

Method of using a durable, workable, non-toxic alloy as an implant for bone, joint or dental surgery which comprises providing an implant of a worked and heat-treated alloy composition consisting essentially of i. a first component constituting from about 3% to about 30% by weight of said alloy composition and consisting essentially of not less than one member selected from the group consisting of niobium, tantalum, chromium, molybdenum, and aluminum; and the balance ii. a second component consisting of not less than one member selected from the group consisting of titanium, and zirconium wherein the sum of the weights of chromium, molybdenum, and aluminum in said alloy composition amounts to not more than 20% by weight of said alloy composition, and the weight of zirconium in said alloy composition amounts to not more than 75% by weight of said alloy composition; said alloy composition being free from copper, cobalt, nickel, vanadium, and tin, apart from the usual impurities, said alloy composition having a tensile strength of at least about 100 kg/mm 2 and fatigue strength of at least about 40 kg/mm 2 , and positioning said implant in a living subject undergoing bone joint or dental surgery for internal fixation or repair of a fractured bone, joint or tooth.

Claim 10

Method of using a durable, workable, non-toxic alloy as an implant for bone, joint or dental surgery which comprises providing an implant of a worked and heat-treated alloy composition consisting essentially of i. a first component constituting from about 3% to about 30% by weight of said alloy composition and consisting essentially of not less than one member selected from the group consisting of niobium, tantalum, chromium, molybdenum, and aluminum; and the balance ii. a second component consisting of not less than one member selected from the group consisting of titanium, and zirconium wherein the sum of the weights of chromium, molybdenum, and aluminum in said alloy composition amounts to not more than 20% by weight of said alloy composition, and the weight of zirconium in said alloy composition amounts to not more than 75% by weight of said alloy composition; said alloy composition being free from copper, cobalt, nickel, vanadium, and tin, apart from the usual impurities, said alloy composition having a tensile strength of at least about 100 kg/mm 2 and fatigue strength of at least about 40 kg/mm 2 , and positioning said implant in a living subject undergoing bone joint or dental surgery for internal fixation or repair of a fractured bone, joint or tooth.

Claim 11

The method of claim 8, wherein up to about 1% by weight of said alloy composition is dissolved gas.

Claim 12

The method of claim 9, wherein said gas is a member selected from the group consisting of oxygen, nitrogen, hydrogen and a carbon containing gas.

Claim 13

The method of claim 8, wherein said first component contains about 3% by weight niobium and about 6% by weight aluminum based on said alloy, and said second component consists essentially of titanium.

Claim 14

The method of claim 8, wherein said first component contains from about 8% to about 9% by weight niobium, about 11% by weight chromium and about 3% by weight aluminum based on said alloy, and said second component consists essentially of titanium.

Claim 15

The method of claim 8, wherein said first component contains about 4% by weight molybdenum and about 48% by weight zirconium based on said alloy, and said second component consists essentially of titanium.

Claim 16

Method of making an implant for bone, joint or dental surgery, which comprises: a. providing a worked and heat-treated alloy composition having full tissue compatibility, said alloy composition consisting essentially of: i. a first component of said alloy composition constituting about 3% to about 30% by weight thereof, and consisting essentially of not less than one member selected from the group consisting of niobium, tantalum, chromium, molybdenum, and aluminum; and the balance ii. a second component of said alloy composition consisting essentially of not less than one member selected from the group consisting of titanium, and zirconium, wherein the sum of the weights of chromium, molybdenum and aluminum in said alloy composition about to not more than 20% by weight of said alloy, and the weight of zirconium therein amounts to at most 75% by weight of said alloy composition; said alloy composition being free from copper, cobalt, nickel, vanadium and tin, apart from the usual impurities; b. shaping the alloy composition to the desired form of implant; and c. subjecting the so-shaped alloy composition to heat treatment, whereby an implant is obtained composed of alloy having a tensile strength at least about 100 kg/mm 2 and fatigue strength of at least about 40 kg/mm 2 .

Claim 17

Method of making an implant for bone, joint or dental surgery, which comprises: a. providing a worked and heat-treated alloy composition having full tissue compatibility, said alloy composition consisting essentially of: i. a first component of said alloy composition constituting about 3% to about 30% by weight thereof, and consisting essentially of not less than one member selected from the group consisting of niobium, tantalum, chromium, molybdenum, and aluminum; and the balance ii. a second component of said alloy composition consisting essentially of not less than one member selected from the group consisting of titanium, and zirconium, wherein the sum of the weights of chromium, molybdenum and aluminum in said alloy composition about to not more than 20% by weight of said alloy, and the weight of zirconium therein amounts to at most 75% by weight of said alloy composition; said alloy composition being free from copper, cobalt, nickel, vanadium and tin, apart from the usual impurities; b. shaping the alloy composition to the desired form of implant; and c. subjecting the so-shaped alloy composition to heat treatment, whereby an implant is obtained composed of alloy having a tensile strength at least about 100 kg/mm 2 and fatigue strength of at least about 40 kg/mm 2 .

Claim 18

The method as claimed in claim 14, wherein a dissolved gas, constituting at most 1% by weight of said alloy is added to the alloy.

Claim 19

The method as claimed in claim 14, wherein said first component consists essentially of 3% by weight of niobium and 6% by weight of aluminum, all based on said alloy and wherein said second component consists essentially of titanium.

Claim 20

The method as claimed in claim 14, wherein said first component consists essentially of from about 8% to about 9% by weight of niobium, about 11% by weight of chromium and about 3% by weight of aluminum, all based on said alloy, and wherein said second component consists essentially of titanium.

Claim 21

The method as claimed in claim 14, wherein said first component consists essentially of about 4% by weight of molybdenum and about 48% by weight of zirconium, based on said alloy, and wherein said second component consists essentially of titanium.