Endodontic instruments and methods of manufacturing thereof

Patent metadata

Field	Value
Publication number	US-10351934-B2
Application number	US-201414541872-A
Country	US
Kind code	B2
Filing date	Nov 14, 2014
Priority date	May 10, 2010
Publication date	Jul 16, 2019
Grant date	Jul 16, 2019

Abstract

A method for manufacturing a nonlinear superelastic file comprising the steps of: providing a superelastic file having a shaft and a file axis; providing a fixture including a file groove being defined by one or more displacement members, the file groove configured for receiving the shaft; inserting at least a portion of the shaft into the fixture along the file groove, the portion of the shaft including a first portion of the shaft; contacting the first portion of the shaft with a first displacement member of the one or more displacement members such that the first portion of the shaft is displaced from the file axis thereby forming a first offset portion of the shaft; heating the portion of the shaft while inserted in the fixture to a temperature of at least about 300° C. for a time period of at least about 1 minute to shape-set the portion of the shaft thereby forming a shape-set nonlinear file.

First claim

What is claimed:

1. A method for manufacturing a nonlinear superelastic file comprising the steps of:
providing a superelastic file having a shaft and a file axis;
providing a fixture including a file groove being defined by one or more displacement members, the file groove configured for receiving the shaft;
inserting at least a portion of the shaft into the fixture along the file groove, the portion of the shaft including a first portion of the shaft;
contacting the first portion of the shaft with a first displacement member of the one or more displacement members such that the first portion of the shaft is displaced from the file axis thereby forming a first offset portion of the shaft;
heating the portion of the shaft while inserted in the fixture to a temperature of at least about 300° C. for a time period of at least about 1 minute to shape-set the portion of the shaft thereby forming a shape-set nonlinear file; and
wherein the file groove defines a first predetermined nonlinear file path and at least one of the one or more displacement members are movable relative to the file axis so that the file groove is a variable file groove configured to define the first predetermined nonlinear file path or a second predetermined nonlinear file path that is different from the first predetermined nonlinear file path.

2. The method of claim 1 , wherein the heating step, the portion of the shaft is heated to a temperature from about 300° C. to about 650° C. for a time period from about 1 minute to about 45 minute to shape-set the portion of the shaft thereby forming the shape-set nonlinear file.

3. The method of claim 1 , wherein the heating step, the portion of the shaft is heated to a temperature from about 350° C. to about 600° C. for a time period from about 3 minutes to about 30 minutes to shape-set the portion of the shaft thereby forming the shape-set nonlinear file.

4. The method of claim 1 , wherein the heating step, the portion of the shaft is heated to a temperature from about 450° C. to about 550° C. for a time period from about 5 minutes to about 20 minutes to shape-set the portion of the shaft thereby forming the shape-set nonlinear file.

5. The method of claim 1 , wherein the one or more displacement members includes at least two displacement member that are movable either independently or simultaneously relative to the file axis so that the file groove is a variable file groove configured to define the first predetermined nonlinear file path or a second predetermined nonlinear file path that is different from the first predetermined nonlinear file path.

6. The method of claim 1 , wherein the non-superelastic file is formed of a material that includes a shape memory alloy.

7. The method of claim 6 , wherein the shape memory alloy includes nickel and titanium.

8. The method of claim 7 , wherein the shape memory alloy is a nickel-titanium based ternary alloy.

9. The method of claim 8 , wherein the nickel-titanium based ternary alloy of the formula Ni—Ti—X wherein X is Co, Cr, Fe, or Nb.

10. The method of claim 6 , wherein the shape memory alloy is a nickel-titanium based binary alloy.

11. The method of claim 6 , wherein the shape memory alloy includes a copper based alloy, an iron based alloy or a combination of both.

12. The method of claim 11 , wherein the shape memory alloy is the copper based alloy includes CuZnAl or CuAlNi.

13. The method of claim 11 , wherein the shape memory alloy is the iron based alloy includes FeNiAl, FeNiCo, FeMnSiCrNi or FeNiCoAlTaB.

14. The method of claim 1 further comprising the steps of:
providing the shape-set nonlinear file having an austenite finish temperature; and
heating at least a portion of the shape-set nonlinear file to a temperature from about 300° C. to about 600° C. for a period of time from about 5 minutes to about 120 minutes to alter the austenite finish temperature thereby forming a shape-set non-linear non-superelastic file;
wherein the altered austenite finish temperature of the shape-set non-linear non-superelastic file is from about 20° C. to about 40° C.

15. The method of claim 14 , wherein heating the step, the temperature is from about 300° C. to about 600° C. for a period of time from about 5 minutes to about 120 minutes to alter the austenite finish temperature thereby forming the shape-set non-linear non-superelastic file, and wherein the altered austenite finish temperature of the shape-set non-linear non-superelastic file is from about 20° C. to about 38° C.

16. The method of claim 14 , wherein the heating step, the temperature is from about 400° C. to about 500° C. for a period of time from about 40 minutes to about 70 minutes to alter the austenite finish temperature thereby forming the non-superelastic file, and wherein the altered austenite finish temperature of the non-superelastic file is from about 20° C. to about 35° C.

17. The method of claim 14 , further comprising the step of cooling the portion of the non-superelastic file and heating at least a portion of the cooled non-superelastic file to a temperature from about 300° C. to about 650° C. for a time period from about 1 minute to about 45 minute to shape-set the portion of the shaft thereby forming a shape-set non-superelastic nonlinear file.

18. The method of claim 14 , further comprising the step of cooling the portion of the non-superelastic file and heating at least a portion of the cooled non-superelastic file to a temperature from about 350° C. to about 600° C. for a time period from about 3 minutes to about 30 minutes to shape-set the portion of the shaft thereby forming a shape-set non-superelastic nonlinear file.

19. The method of claim 14 , wherein the shape-set non-linear non-superelastic file is formed of a material that includes a shape memory alloy.

20. The method of claim 19 , wherein the shape memory alloy includes nickel and titanium.

21. The method of claim 19 , wherein the shape memory alloy is a nickel-titanium based binary alloy.

22. The method of claim 19 , wherein the shape memory alloy is a nickel-titanium based ternary alloy.

23. The method of claim 22 , wherein the nickel-titanium based ternary alloy of the formula Ni—Ti—X wherein X is Co, Cr, Fe, or Nb.

24. The method of claim 19 , wherein the shape memory alloy includes a copper based alloy, an iron based alloy or a combination of both.

25. The method of claim 24 , wherein the shape memory alloy is the copper based alloy includes CuZnAl or CuAlNi.

26. The method of claim 24 , wherein the shape memory alloy is the iron based alloy includes FeNiAl, FeNiCo, FeMnSiCrNi or FeNiCoAlTaB.

Assignees

• Dentsply Sirona Inc

Inventors

• Ammon Dan
• Shotton Vincent
• Gao Yong
• Maxwell Randall

Classifications

• C22C18/02 Primary

  with copper as the next major constituent · CPC title

• C21D6/008

  containing Si · CPC title

• C22F1/10

  of nickel or cobalt or alloys based thereon · CPC title

• C22C30/00

  Alloys containing less than 50% by weight of each constituent · CPC title

• C21D9/0068

  for particular articles not mentioned below · CPC title