Binder-Jet Piston Crown Air Gaps for Lower Heat Transfer

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Solution Overview

Problem

Current additive manufacturing methods for pistons in internal combustion engines, such as DED and SLM, face challenges like high production costs, slow manufacturing time, and residual stresses due to laser use, which hinder large-scale production and efficient heat transfer reduction.

Innovation Solution

The use of binder jet technology to manufacture pistons with isolated crown and skirt sections, forming air gaps through a sintering process that eliminates the need for laser heating and reduces production time, allowing for faster and more efficient heat transfer resistance.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Loss of energy

If DED or SLM additive manufacturing methods are used to form air gaps in pistons, then heat transfer resistance is improved, but manufacturing time increases and production rate decreases

Engineering Contradiction:
Improveheat transfer lossVSAvoidproduction rate
Core Design Contradiction:
Loss of energyVSProductivity

Solution Approach 1:

The patent replaces laser-based thermal processing (DED/SLM) with binder jetting technology that uses a bonding agent to join metal particles. This substitution eliminates the need for intensive laser heating and melting, dramatically reducing manufacturing time while maintaining the ability to create complex air gap geometries for heat transfer reduction.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

Solution Approach 2:

The patent changes the fundamental processing parameters from high-energy laser melting to low-energy binder deposition followed by sintering. This parameter change transforms the manufacturing process from a slow, layer-by-layer melting operation to a faster binder application and consolidation process, improving production rate while preserving the air gap structure.

Inventive Principle:
Principle #35Parameter changes

2Manufacturing precision

If DED or SLM methods are used to manufacture pistons with air gaps, then geometric precision is improved, but residual stresses increase due to laser heating

Engineering Contradiction:
Improvegeometry controlVSAvoidresidual stress
Core Design Contradiction:
Manufacturing precisionVSStress or pressure

Solution Approach 1:

The patent substitutes laser-based thermal processing with binder jetting that uses a chemical bonding mechanism instead of thermal melting. This eliminates the intense localized heating that causes thermal gradients and residual stresses, while still achieving precise geometric control through controlled binder deposition and subsequent sintering.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

Solution Approach 2:

The patent changes the energy input method from high-energy laser to low-energy binder chemistry. This parameter change fundamentally alters the stress state during manufacturing by avoiding rapid thermal cycles, thereby reducing residual stresses while maintaining dimensional accuracy through the binder's controlled adhesion properties.

Inventive Principle:
Principle #35Parameter changes

3Loss of energy

If laser-based additive manufacturing is used to create air gaps, then heat transfer resistance is improved, but manufacturing cost increases

Engineering Contradiction:
Improveheat transfer lossVSAvoidmanufacturing cost
Core Design Contradiction:
Loss of energyVSEase of manufacture

Solution Approach 1:

The patent replaces expensive laser equipment and operation with binder jetting technology that uses lower-cost bonding agents and less energy-intensive processing. This substitution maintains the air gap geometry's heat transfer benefits while significantly reducing equipment costs, material costs, and operational expenses.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

Solution Approach 2:

The patent changes the energy consumption parameters from high-power laser operation to low-power binder application and sintering. This parameter change reduces both direct energy costs and indirect costs associated with laser equipment maintenance, operation time, and thermal management requirements, making the process more economically viable.

Inventive Principle:
Principle #35Parameter changes

4Manufacturing precision

If SLM is used to manufacture pistons, then air gap geometry is precisely controlled, but support structure removal is required increasing complexity

Engineering Contradiction:
Improveair gap geometryVSAvoidsupport structure requirements
Core Design Contradiction:
Manufacturing precisionVSDevice complexity

Solution Approach 1:

The patent replaces laser-based SLM with binder jetting that does not require support structures during the bonding process. The binder can be selectively applied only where needed to join particles, eliminating the need for extensive support material that would later require removal, thereby simplifying the overall manufacturing process while maintaining geometric precision.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

This approach significantly reduces manufacturing time, minimizes residual stresses, and enhances heat transfer resistance while maintaining the desired metallic properties, thereby improving fuel efficiency by reducing heat transfer losses from the combustion chamber.

Implementation Method 1

the green-state piece is then placed into a sintering oven (batch or continuous) to remove the binder and sinter the metal powder all in one step

Methodology Applied
Scientific EffectSintering: Sintering

Implementation Method 2

Binder jetting deposits droplets of binder within a metal powder bed, rather than selectively laser sintering individual powders together

Methodology Applied
Scientific EffectAdhesion: Adhesive

Implementation Method 3

the piston may include an air gap between the piston crown and piston skirt in order to increase the overall heat transfer resistance between the combustion chamber and the crankcase

Methodology Applied
Scientific EffectThermal insulation: Thermal Insulation

Data Source

PatentUS11112009B2Low heat transfer piston via binder jet technology
Publication Date: 2021.09.07 CUMMINS INC
  • US11112009B2 patent drawing
  • US11112009B2 patent drawing
  • US11112009B2 patent drawing

AI summary

A piston for an internal combustion engine includes a skirt and a crown coupled to the skirt. The crown is produced in isolation from the skirt using an additive manufacturing process. The piston includes a first air gap between the crown and the skirt. According to an example embodiment, the crown includes a plurality of sections produced in isolation from the skirt. The crown may include a second air gap disposed between two of the plurality of sections.