Piston including a composite layer applied to a metal substrate

Patent metadata

Field	Value
Publication number	US-11511515-B2
Application number	US-201916601918-A
Country	US
Kind code	B2
Filing date	Oct 15, 2019
Priority date	Dec 28, 2015
Publication date	Nov 29, 2022
Grant date	Nov 29, 2022

Abstract

A piston for a heavy duty diesel engine including a composite layer forming at least a portion of a combustion surface is provided. The composite layer has a thickness greater than 500 microns and includes a mixture of components typically used to form brake pads, such as a thermoset resin, an insulating component, strengthening fibers, and an impact toughening additive. According to one example, the thermoset resin is a phenolic resin, the insulating component is a ceramic, the strengthening fibers are graphite, and the impact toughening additive is an aramid pulp of fibrillated chopped synthetic fibers. The composite layer also has a thermal conductivity of 0.8 to 5 W/m·K. The body portion of the piston can include an undercut scroll thread to improve mechanical locking of the composite layer. The piston can also include a ceramic insert between the body portion and the composite layer.

First claim

The invention claimed is:

1. A method of manufacturing a piston, comprising the steps of: applying a composite layer to a body portion formed of metal, the composite layer forming at least a portion of a combustion surface, and the composite layer including a thermoset resin, an insulating component, strengthening fibers, and an impact toughening additive,
wherein the thermoset resin is a phenolic resin, the insulating component is a ceramic, the strengthening fibers are graphite, and the impact toughening additive is an aramid pulp of fibrillated chopped synthetic fibers.

2. The method of claim 1 , wherein the step of applying the composite layer to the body portion includes molding a mixture to an uppermost surface of the body portion.

3. The method of claim 2 , wherein the molding step includes a B-stage, the B-stage includes applying heat and pressure to the mixture on the body portion, and the mixture does not fully cure during the B-stage.

4. The method of claim 3 , wherein the molding step further includes increasing the temperature of the mixture while applying pressure to the mixture after the B-stage until the mixture fully cures.

5. The method of claim 1 , wherein the step of applying the composite layer to the body portion includes forming a preform insert of a mixture, and molding the preform insert to an uppermost portion of the body portion.

6. The method of claim 1 , wherein the step of applying the composite layer to the body portion includes disposing an insert formed of ceramic on an uppermost surface of the body portion and disposing the composite layer on the ceramic insert.

7. The method claim 1 , wherein the composite layer has a thermal conductivity of 0.8 to 5 W/m·K.

8. The method of claim 1 , further including the steps of:
providing the body portion formed of aluminum or steel;
forming an undercut scroll thread in an uppermost surface of the body portion before applying the composite layer;
disposing the body portion in a mold;
mixing the thermoset resin, the insulating component, the strengthening fibers, and the impact toughening additive;
disposing the mixture on the uppermost surface of the body portion in the mold;
molding the mixture to the uppermost surface to form the composite layer;
the molding step including applying pressure to the mixture on the body portion of up to p to 2.5 tons/square inch, and heating the mixture to 120 to 130° C. for 5 to 60 minutes such that the mixture does not fully cure; and
the molding step including increasing the temperature of the compressed mixture to 180 to 250° C. while applying pressure to the mixture on the body portion until the mixture fully cures and forms the composite layer.

9. A method of manufacturing a piston, comprising the steps of: applying a composite layer to a body portion formed of metal, the composite layer forming at least a portion of a combustion surface, and the composite layer including a thermoset resin, an insulating component, strengthening fibers, and an impact toughening additive,
wherein the thermoset resin is present in an amount of 25 wt. % to 35 wt. %, based on the total weight of the composite layer; the insulating component is present in an amount of 50 wt. % to 70 wt. %, based on the total weight of the composite layer; the strengthening fibers are present in an amount of 1 wt. 00 to 10 wt. %, based on the total weight of the composite layer; and the impact toughening additive is present in an amount of I wt. % to 10 wt. %, based on the total weight of the composite layer.

Assignees

• Tenneco Inc

Inventors

• Lineton Warran Boyd
• Evers Ross Allen
• Salenbien Greg

Classifications

• B32B15/14

  next to a fibrous or filamentary layer · CPC title

• B32B27/06

  as the main or only constituent of a layer, {which is} next to another layer of {the same or of} a {different material (next to a layer of a particular substance B32B9/045; next to a bituminous or tarry layer B32B11/046; next to a water setting substance layer B32B13/12; next to a metal layer B32B15/08; next to a glass layer B32B17/10; next to a layer formed of natural mineral fibres or particles B32B19/045; next to a wood layer B32B21/08; next to a cellulosic plastic layer B32B23/08; next to a natural or synthetic rubber layer B32B25/08)} · CPC title

• B32B5/00

  Layered products characterised by the non- homogeneity or physical structure {, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts} · CPC title

• B32B2262/105

  Ceramic fibres · CPC title

• B32B27/00

  Layered products comprising {a layer of} synthetic resin {(fibrous or filamentary layer made of a synthetic resin B32B5/02; particulate layer made of a synthetic resin B32B5/16; foamed layer made of a synthetic resin B32B5/18)} · CPC title