Chemical vapor deposition of wear resistant coatings onto piston ring running face, side face, and inner diameter in one coating run

Patent metadata

Field	Value
Publication number	US-9909210-B2
Application number	US-201314051696-A
Country	US
Kind code	B2
Filing date	Oct 11, 2013
Priority date	Oct 11, 2012
Publication date	Mar 6, 2018
Grant date	Mar 6, 2018

Abstract

A method of coating all surfaces of a plurality of piston rings in a single run by a chemical vapor deposition (CVD) process is provided. The method can include providing a coil formed of an iron-based material; heating the coil; and depositing a coating on all surfaces of the coil during a single continuous period of time, without having to move the coil during the CVD process. The coil is maintained in a fixed position during the depositing step. The method next includes splitting the coil into a plurality of separate coated piston rings. Alternatively, the method can include providing a plurality of stacked keystone piston ring bodies; and disposing a cylinder around the stack to maintain the keystone piston ring bodies in position while depositing the CVD coating on all surfaces of the keystone piston ring bodies during the single coating run.

First claim

The invention claimed is:

1. A method of forming a plurality of coated piston rings, comprising the steps of:
providing a coil formed of a first metal material and including a plurality of windings, each winding including an inner diameter surface, an outer diameter surface, and side surfaces extending from the inner diameter surface to the outer diameter surface;
applying a coating to the coil during a single period of time by a chemical vapor deposition (CVD) process, wherein the windings of the coil are spaced from one another while applying the coating so that all of the surfaces of the coil are coated during the single period of time; and
splitting the coated coil into a plurality of coated piston rings.

2. The method of claim 1 , wherein the windings extend continuously along and circumferentially around a center axis; and including the step of maintaining the coil in a fixed position with each winding spaced from an adjacent winding by not greater than 1 μm while applying the coating.

3. The method of claim 1 , wherein the windings extend continuously along and circumferentially around a center axis; and including the steps of disposing a tube with a plurality of orifices along the center axis; and supplying gas including the composition of the coating through the orifices of the tube during the CVD process.

4. The method of claim 1 , wherein the composition of the coating includes at least one of nitrogen and carbon, and at least one of titanium, chromium, and hafnium.

5. The method of claim 4 , wherein the coating includes a plurality of layers, wherein each layer includes at least one of TiN, CrN, HfN, TiCN, TiC, CrC, and Al 2 O 3 .

6. The method of claim 5 , wherein the plurality of layers includes a base layer formed of TiC, a middle layer formed of Al 2 O 3 , and a top layer formed of TiN.

7. The method of claim 1 , wherein the CVD process includes heating the coil in a reaction chamber; supplying a gas including the composition of the coating to the reaction chamber; and depositing the composition on all surfaces of the heated coil.

8. The method of claim 7 , wherein the composition of the coating includes at least one of TiN, CrN, HfN, TiCN, TiC, CrC, and Al 2 O 3 .

9. The method of claim 1 , wherein the CVD process is conducted at atmospheric pressure.

10. The method of claim 1 , wherein the CVD process is conducted at a temperature not greater than 500° C.

11. The method of claim 1 , wherein the CVD process is conducted at a temperature of 700 to 1050° C.

12. The method of claim 1 including providing a wire of the first metal material; forming the wire into the coil; and at least one of the following steps: forming a groove along an outer diameter surface of the wire; and embedding a second metal material distinct from the first metal material in an outer diameter surface of the wire.

13. The method of claim 1 , wherein the surfaces extend circumferentially around a center axis.

14. A method of forming a plurality of coated keystone piston rings, comprising the steps of:
providing a stack of keystone piston ring bodies each formed of a first metal material, each keystone piston ring body includes an inner diameter surface, an outer diameter surface, and a pair of side surfaces extending from the inner surface to the outer diameter surface, the side surfaces extend inwardly toward one another at an angle from the outer diameter surface to the inner diameter surface, the outer diameter surface is convex, and the inner diameter surface is concave; and
applying a coating to all surfaces of the keystone piston ring bodies during a single period of time by a chemical vapor deposition (CVD) process.

15. The method of claim 14 , wherein the surfaces extend circumferentially around a center axis.

16. The method of claim 14 , including maintaining each keystone piston ring body in a fixed position relative to the adjacent keystone piston ring body while applying the coating.

17. The method of claim 16 , including disposing a cylinder around the stack of keystone piston ring bodies to maintain the keystone piston ring bodies in the fixed position.

18. The method of claim 14 , wherein each keystone piston ring body extends circumferentially around a center axis; and including disposing a tube with a plurality of orifices along the center axis; and supplying gas including the composition of the coating through the orifices of the tube during the CVD process.

19. The method of claim 1 , wherein each keystone piston ring body in the stack is spaced from an adjacent keystone piston ring body by not greater than 1 μm while applying the coating.

20. A method of forming a plurality of a coated piston rings, comprising the steps of:
providing a wire formed of an iron-based material;
winding the wire around a center axis to form a coil with a plurality of windings extending continuously along and circumferentially around a center axis, each winding including an inner diameter surface, an outer diameter surface, and side surfaces extending from the inner diameter surface to the outer diameter surface;
disposing the coil in a reaction chamber; heating the coil in the reaction chamber;
supplying a gas to the reaction chamber, wherein the gas includes at least one of the following compositions: TiN, CrN, HfN, TiCN, TiC, CrC, and Al 2 O 3 ;
depositing a coating formed of the at least one composition on all of the surfaces of the coil during a single continuous period of time, wherein the windings of the coil are spaced from one another while depositing the coating so that all of the surfaces of the coil are coated during the single period of time;
maintaining the coil in a fixed position with each winding spaced from an adjacent winding by not greater than 1 μm while depositing the coating on the surfaces;
supplying a flow of gas through the reaction chamber to remove any volatile by-products from the reaction chamber;
splitting the coated coil into a plurality of separate coated piston rings each including an inner diameter surface, an outer diameter surface, and side surfaces each extending circumferentially around a center axis and including the coating deposited on each of the surfaces;
hardening the iron-based material of the coated piston ring; and
the hardening step including at least one of the following steps: heating and quenching, tempering, austempering, and martempering.

Assignees

• Federal Mogul Corp
• Fed Mogul Llc

Inventors

• Aharonov Robert
• Gekonde Haron

Classifications

• C23C16/36

  Carbonitrides · CPC title

• C23C16/34

  Nitrides {(C23C16/303 takes precedence)} · CPC title

• C23C16/403

  of aluminium, magnesium or beryllium · CPC title

• C23C16/32 Primary

  Carbides · CPC title

• C21D9/40

  for rings; for bearing races · CPC title