Hardened titanium structure for transmission gear applications

Patent metadata

Field	Value
Publication number	US-10179940-B2
Application number	US-201514942997-A
Country	US
Kind code	B2
Filing date	Nov 16, 2015
Priority date	Feb 11, 2009
Publication date	Jan 15, 2019
Grant date	Jan 15, 2019

Abstract

A method and apparatus are present for manufacturing a part. The part is comprised of a metal alloy and is positioned to form a positioned part. An electromagnetic field is generated that heats the positioned part. A surface of the positioned part is exposed to an inert gas, while the electromagnetic field is generated to create an inverse thermal gradient between an exterior of the positioned part and an interior section of the positioned part to form a heat treated part.

First claim

What is claimed is:

1. An apparatus comprising:
a chamber configured to hold a spur gear comprising a cylindrical portion and teeth radially extending from the cylindrical portion;
an induction coil configured to generate an electromagnetic field located in the chamber; and
a gas delivery system with a cooling ring manifold comprising a plurality of jets arranged radially around a central axis of the spur gear and directed at the teeth and dedendum circle of the spur gear, the gas delivery system configured to continuously deliver an inert gas from the chamber onto the teeth and a dedendum circle of the spur gear to cool the teeth of the spur gear, wherein the cylindrical portion of the spur gear within a root diameter of the spur gear is allowed to heat via induction heating created by the electromagnetic field thereby establishing an inverse thermal gradient through the spur gear.

2. The apparatus of claim 1 further comprising:
a power unit configured to generate a current that causes the induction coil to generate the electromagnetic field at a frequency configured to create eddy currents an interior section of the spur gear.

3. The apparatus of claim 1 , wherein the chamber comprises a circular chamber.

4. The apparatus of claim 3 , wherein the chamber further comprises a part holder configured to hold the spur gear.

5. The apparatus of claim 1 , wherein the induction coil is configured to generate different eddy currents in the spur gear.

6. The apparatus of claim 1 further comprising:
a forge configured to forge a plate of metal into the spur gear.

7. The apparatus of claim 6 , wherein the forge is further configured to forge the plate in a beta phase region.

8. The apparatus of claim 7 , wherein the forge is further configured to forge the plate into an alpha plus beta phase region after forging the spur gear in the beta phase region.

9. The apparatus of claim 8 further comprising:
a solution heat treatment device configured to solution heat treat the spur gear in the beta phase after forging the spur gear.

10. The apparatus of claim 1 further comprising:
a cooling station configured to quench the spur gear after forging rapidly enough to prevent alpha precipitation from occurring.

11. The apparatus of claim 10 wherein the cooling station is an air cooling station.

12. The apparatus of claim 10 wherein the cooling station is a water cooling station.

13. The apparatus of claim 1 further comprising:
a machining station configured to machine the spur gear.

14. The apparatus of claim 1 further comprising:
a grinding station configured to grind the spur gear after heat treatment.

15. The apparatus of claim 1 further comprising:
a compression station configured to place the spur gear into compressive stress after heat treatment.

16. The apparatus of claim 1 further comprising:
a peening station configured to perform laser shock peening on a surface of the spur gear.

17. The apparatus of claim 1 further comprising:
a coating station configured to deposit a coating on a surface of the spur gear.

18. The apparatus of claim 17 , wherein the coating comprises a material selected from one of physical vapor deposition titanium nitride, plated nickel carbide, and high velocity oxygen fuel deposited tungsten carbide—cobalt.

19. The apparatus of claim 17 further comprising:
a polishing station configured to polish a surface of the spur gear with the coating.

20. The apparatus of claim 1 , wherein establishing an inverse thermal gradient through the spur gear comprises creating an inverse thermal gradient between an exterior of the spur gear and an interior section of the spur gear to form a heat treated gear.

21. The apparatus of claim 1 , wherein inverse thermal gradient comprises an increasing temperature farther into an interior of the spur gear as compared to a surface of the spur gear.

22. The apparatus of claim 21 , wherein a temperature of the interior of the spur gear is between around 1,000 degrees Fahrenheit and around 1,100 degrees Fahrenheit and wherein a temperature of the surface of the spur gear is between around 800 degrees Fahrenheit and around 900 degrees Fahrenheit.

Assignees

• Boeing Co

Inventors

• Kirkwood Brad L
• Matsen Marc R
• Shen Tony
• Crow Wesley B

Classifications

• C22F1/10

  of nickel or cobalt or alloys based thereon · CPC title

• C21D1/74

  Methods of treatment in inert gas, controlled atmosphere, vacuum or pulverulent material · CPC title

• C21D1/62

  Quenching devices · CPC title

• C21D1/10

  by electric induction · CPC title

• C21D2211/004

  Dispersions; Precipitations · CPC title