Rotor construction for high speed motors
View Patent ↗A rotor shaft for a high speed motor that has a coating that is secured to a shaft body. The coating and the shaft body are formed from dissimilar materials. More specifically, the coating may be an alloy material, such as, for example, a copper alloy, while the shaft body may be a steel material. According to certain embodiments, the alloy material of the coating may be secured to at least a portion of a rotor body blank in a solution treated condition via a low temperature welding procedure. Additionally, the coating may be hardened, such as for example, through the use of an age hardening process. The coating and the rotor body blank may be machined together to form the rotor shaft. According to certain embodiments, such machining may configure the rotor shaft for use with a turbo-compressor that is configured for air compression.
1. A method for manufacturing a rotor shaft for a high speed motor, the method comprising:
forming a rotor body blank from a steel material;
solution treating an alloy material, the alloy material and the steel material of the rotor body blank being different materials;
securing the solution treated alloy material to at least a portion of the rotor body blank to provide a coating;
heat treating the coating when the coating is secured to the rotor body blank; and
machining the rotor body blank and the coating to form the rotor shaft, the rotor shaft configured for operation in a high speed motor.
2. The method of claim 1 , wherein the alloy material is a copper alloy.
3. The method of claim 2 , wherein the step of securing the alloy material includes using a low temperature welding process.
4. The method of claim 3 , wherein the step of securing the alloy material includes using explosion welding to cover at least a portion of the rotor body blank with the alloy material.
5. The method of claim 3 , wherein the step of heat treating the coating includes age hardening the coating.
6. The method of claim 5 , further including the step of stress relieving the coating.
7. The method of claim 6 , wherein the rotor shaft is manufactured to operate at a tip speed greater than 300 meters/second.
8. The method of claim 6 , wherein the step of machining the rotor body blank and the coating includes forming the rotor shaft for use with a turbo-compressor that is configured for air compression.
9. The method of claim 8 , wherein the step of heat treating the coating includes enhancing the ductility of the coating.
10. The method of claim 8 , wherein the step of heat treating the coating includes enhancing the hardness of the coating.
11. The method of claim 8 , wherein the step of heat treating includes enhancing the temperature dependent creep resistance of the coating.
12. The method of claim 2 , wherein the solution treating is conducted at a temperature between 1450-1850 degrees Fahrenheit.
13. The method of claim 12 , wherein the solution treating is followed by water quenching.
14. The method of claim 12 , wherein the step of heat treating the coating includes enhancing the ductility of the coating.
15. A method for manufacturing a rotor shaft for a high speed motor, the method comprising:
providing a rotor body blank from a steel material;
providing an alloy material which has been solution heat treated, the alloy material and the steel material of the rotor body blank being different materials;
securing the alloy material which has been solution heat treated to at least a portion of the rotor body blank to provide a coating;
heat treating the coating when the coating is secured to the rotor body blank; and
machining the rotor body blank and the coating to form the rotor shaft, the rotor shaft configured for operation in a high speed motor.
16. The method of claim 15 , wherein the alloy material is a copper alloy.
17. The method of claim 16 , wherein the step of securing the alloy material includes using an explosion welding process.
18. The method of claim 17 , wherein the step of heat treating the coating includes age hardening the coating.
19. The method of claim 18 , wherein the age hardening includes subjecting the coating to a temperature between 795-935 degrees Fahrenheit for between two to four hours.
20. The method of claim 19 , wherein the rotor shaft is manufactured to operate at a tip speed greater than 300 meters/second.
21. The method of claim 19 , wherein the copper alloy is a copper chromium alloy, and which further includes precipitating out the chromium during the age hardening.