Method for manufacturing magnetostrictive torque sensor shaft
US-2018195142-A1 · Jul 12, 2018 · US
US11866798B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11866798-B2 |
| Application number | US-201715854102-A |
| Country | US |
| Kind code | B2 |
| Filing date | Dec 26, 2017 |
| Priority date | Jan 11, 2017 |
| Publication date | Jan 9, 2024 |
| Grant date | Jan 9, 2024 |
A practical reading order for non-experts. Skip the full description unless you need deep technical detail.
What the patent document calls the invention.
A short plain-language summary of the technical disclosure.
Who owns or filed the patent and who is credited as inventor.
Filing, priority, publication, and grant dates set the timeline.
The legal scope of protection — read this for what is actually claimed.
Technology tags used to group this patent with similar filings.
Prior art links and similar publications in this corpus.
Official abstract text for this publication.
Provided is a method for manufacturing a magnetostrictive torque sensor shaft mounting a sensor portion of a magnetostrictive torque sensor. The method includes conducting heat treatment on a shaft material including chrome steel or chrome-molybdenum steel by carburizing, quenching and tempering, and conducting shot peening on the shaft material after the heat treatment at least on a position where the sensor portion is to be mounted. The shot peening is conducted by firing shot with a particle size of not less than 0.6 mm and a Rockwell hardness of not less than 60 at a jet pressure of not less than 0.4 MPa for a jet exposure time of not less than 2 minutes.
Opening claim text (preview).
What is claimed is: 1. A method for manufacturing a magnetostrictive torque sensor shaft mounting a sensor portion of a magnetostrictive torque sensor, the method consisting of: conducting heat treatment on a shaft material comprising chrome steel or chrome-molybdenum steel by carburizing for one time, quenching, and tempering for plural times such that the surface of the shaft material includes both austenite and martensite; and conducting shot peening on the shaft material after the heat treatment at least on a continuous surface where the sensor portion is to be mounted, wherein the shot peening is conducted by firing shot with a particle size of not less than 0.6 mm and not more than 0.8 mm and a Rockwell hardness of not less than 60 at a jet pressure of not less than 0.4 MPa and not more than 0.6 MPa for a jet exposure time of not less than 2 minutes only once such that further martensitic transformation occurs on the shaft material, such that peak values of martensite in the shaft material having a Miller index of 200 and martensite having a Miller index of 211, respectively, are not less than 1.15 times peak values of martensite in the shaft material with a Miller index of 200 and martensite having a Miller index of 211, respectively, before conducting shot peening, such that sensitivity of the resulting magnetostrictive torque sensor is not less than 4 mV/Nm, wherein hysteresis error of the magnetostrictive torque sensor is not more than 3% FS in a range of not less than −40° C. and not more than 150° C., and wherein the hardness of the shaft material after the heat treatment step is an HRC of not less than 59 and not more than 62, and wherein the shaft surface after the shot peening step has a surface roughness Ra of not more than 0.2 μm. 2. The method according to claim 1 , wherein the shaft material includes an Ni content that is no more than 0.25% by mass. 3. The method according to claim 1 , wherein the shot peening is conducted at a jet pressure of not less than 0.4 MPa and less than 0.55 MPa for a jet exposure time of not less than 5 minutes, or is conducted at a jet pressure of not less than 0.55 MPa for a jet exposure time of not less than 2 minutes. 4. The method according to claim 3 , wherein the shaft material comprises chrome steel. 5. The method according to claim 1 , wherein the shot peening is conducted at a jet pressure of not less than 0.4 MPa and less than 0.55 MPa for a jet exposure time of not less than 10 minutes, or is conducted at a jet pressure of not less than 0.55 MPa for a jet exposure time of about 2 minutes. 6. The method according to claim 1 , wherein the shot peening is conducted at a jet pressure of not less than 0.55 MPa for a jet exposure time of about 2 minutes. 7. The method according to claim 1 , wherein the heat treatment is conducted so that the shaft material after the heat treatment has a Rockwell hardness of not less than 58. 8. The method according to claim 1 , wherein the quenching of the shaft material is marquenching, and wherein in the heat treatment of the shaft material, all of the plural tempering occurs after all marquenching of the shaft material has occurred. 9. The method according to claim 8 , wherein in the heat treatment of the shaft material, all of the plural tempering is performed at about 180° C. or less. 10. The method according to claim 1 , wherein the shot peening is conducted by firing shot with a particle size of about 0.8 mm. 11. A method for manufacturing a magnetostrictive torque sensor shaft mounting a sensor portion of a magnetostrictive torque sensor, the method consisting of: conducting heat treatment on a shaft material comprising chrome steel or chrome-molybdenum steel by carburizing for one time, quenching, and tempering for plural times such that the surface of the shaft material includes both austenite and martensite; and conducting shot peening on the shaft material after the heat treatment at least on a continuous surface where the sensor portion is to be mounted, wherein the shot peening is conducted by firing shot with a particle size of not less than 0.6 mm and not more than 0.8 mm and a Rockwell hardness of not less than 60 at a jet pressure of not less than 0.4 MPa and not more than 0.6 MPa for a jet exposure time of not less than 2 minutes only once such that further martensitic transformation occurs on the shaft material, wherein the shot peening is conducted until a peak value of martensite in the shaft material with a Miller index of (200) is greater than a peak value of austenite in the shaft material with a Miller index of (200), wherein before the shot peening is conducted, the peak value of martensite in the shaft material with a Miller index of (200) is smaller than the peak value of austenite in the shaft material with a Miller index of (200), wherein peak values of martensite in the shaft material with a Miller index of (200) after conducting shot peening and martensite in the shaft material with a Miller index of (211) after conducting shot peening are not less than 1.15 times peak values of martensite in the shaft material with a Miller index of (200) and martensite in the shaft material with a Miller index of (211) before conducting shot peening, such that sensitivity of the resulting magnetostrictive torque sensor is not less than 4 mV/Nm, wherein hysteresis error of the magnetostrictive torque sensor is not more than 3% FS in a range of not less than −40° C. and not more than 150° C., wherein the hardness of the shaft material after the heat treatment step is an HRC of not less than 59 and not more than 62, and wherein the shaft surface after the shot peening step has a surface roughness Ra of not more than 0.2 μm. 12. The method according to claim 11 , wherein the shaft material includes an Ni content that is no more than 0.25% by mass. 13. The method according to claim 11 , wherein the shot peening is conducted at a jet pressure of not less than 0.4 MPa and less than 0.55 MPa for a jet exposure time of not less than 5 minutes, or is conducted at a jet pressure of not less than 0.55 MPa for a jet exposure time of not less than 2 minutes. 14. The method according to claim 13 , wherein the shaft material comprises chrome steel. 15. The method according to claim 11 , wherein the shot peening is conducted at a jet pressure of not less than 0.4 MPa and less than 0.55 MPa for a jet exposure time of not less than 10 minutes, or is conducted at a jet pressure of not less than 0.55 MPa for a jet exposure time of about 2 minutes. 16. The method according to claim 11 , wherein the shot peening is conducted at a jet pressure of not less than 0.55 MPa for a jet exposure time of about 2 minutes. 17. The method according to claim 11 , wherein the heat treatment is conducted so that the shaft material after the heat treatment has a Rockwell hardness of not less than 58. 18. The method according to claim 11 , wherein the quenching of the shaft material is marquenching, and wherein in the heat treatment of the shaft material, all of the plural tempering occurs after all marquenching of the shaft material has occurred. 19. The method according to claim 18 , wherein in the heat treatment of the shaft material, all of the plural tempering is performed at about 180° C. or less. 20. The method according to claim 11 , wherein the shot peening is conducted by firing shot with a particle size of about 0.8 mm.
during manufacturing of rods or wires · CPC title
for rods of limited length (of unlimited length C21D9/52) · CPC title
for compacting surfaces, e.g. shot-peening (for deforming sheet metal, tubes or profiles B21D31/06; as a metallurgical treatment C21D7/00, C22F1/00) · CPC title
containing Cr and Ni · CPC title
by shot-peening or the like · CPC title
Related publications grouped by family.
Answers are generated from the same data shown on this page.