Near-Net Shaped Building Blocks Joined via Interfacial Reaction

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Solution Overview

Problem

Traditional methods for manufacturing large-scale aircraft components are inefficient, resulting in high machining time and material waste, especially when using exotic materials like titanium alloys, as they require significant material removal to achieve the final shape.

Innovation Solution

The method involves constructing and physically joining near-net shaped structural building blocks using an interfacial reaction-activation mechanism, where CAD-designed blocks are stacked and fused using surface treatments to minimize material waste and machining time, potentially incorporating active control elements for shape adjustment.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Manufacturing precision

If traditional machining methods are used to manufacture large-scale aircraft components from solid billets, then the final part can be achieved with high precision, but the machining time and material waste increase dramatically

Engineering Contradiction:
Improvepart dimensional accuracyVSAvoidmachining time
Core Design Contradiction:
Manufacturing precisionVSLoss of time

Solution Approach 1:

The patent applies preliminary action by pre-forming building blocks into near-net shaped components before final assembly. The blocks are manufactured with predetermined geometries that closely match the final part dimensions, eliminating the need for extensive post-assembly machining. This preliminary shaping action significantly reduces the material removal required in traditional machining processes.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The patent divides the final component into multiple modular building blocks that can be independently manufactured and then assembled. Each block is designed with specific geometries and features that allow for precise positioning and joining. This segmentation enables parallel manufacturing of blocks and reduces the complexity of machining a single large component.

Inventive Principle:
Principle #1Segmentation

2Manufacturing precision

If traditional machining methods are used to manufacture large-scale aircraft components from solid billets, then the final part can be achieved with high precision, but the material waste increases to 50-90%

Engineering Contradiction:
Improvepart dimensional accuracyVSAvoidmaterial waste
Core Design Contradiction:
Manufacturing precisionVSLoss of substance

Solution Approach 1:

The building blocks are pre-formed with near-net shapes that closely match the final component geometry. This preliminary action ensures that material is added only where needed during block formation, and minimal material removal is required during final assembly and finishing operations, reducing waste to less than 5% of the total material used.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The patent utilizes composite material structures within the building blocks, combining different materials to achieve desired mechanical properties while minimizing material usage. The modular composite blocks can be optimized for specific functional requirements, reducing overall material consumption compared to traditional monolithic machining approaches.

Inventive Principle:
Principle #40Composite materials

3Loss of substance

If building blocks are stacked and joined to form near-net shaped parts, then material waste is reduced to less than 5%, but new joining processes and interfacial reactions are required

Engineering Contradiction:
Improvematerial wasteVSAvoidjoining process complexity
Core Design Contradiction:
Loss of substanceVSDevice complexity

Solution Approach 1:

The patent replaces traditional mechanical joining methods (such as fasteners and welds) with interfacial reaction-activation mechanisms. Chemical reactions occur at the interfaces between building blocks during assembly, creating strong bonds without requiring complex mechanical joining systems. This substitution simplifies the overall joining process while maintaining structural integrity.

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

Solution Approach 2:

The patent utilizes parameter changes in the form of activation conditions (temperature, pressure, or chemical triggers) to initiate interfacial reactions between building blocks. By controlling these parameters, the joining process can be precisely managed to achieve strong bonds between blocks without requiring complex joining equipment or procedures.

Inventive Principle:
Principle #35Parameter changes

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 machining time and material waste, offering cost savings by creating components with less than 5% waste material and up to 95% reduction in machining time compared to traditional methods, while allowing for flexible production of various parts without extensive tooling or fasteners.

Implementation Method 1

an interfacial reaction-activation mechanism

Methodology Applied
Scientific EffectChemical reaction: Chemical Bonding

Data Source

PatentUS8606389B2Method to construct and physically join building blocks into a near-net shaped part using an interfacial reaction-activation mechanism
Publication Date: 2013.12.10 SOUTHWEST RES INST
  • US8606389B2 patent drawing
  • US8606389B2 patent drawing

AI summary

The disclosure provides a method to construct and physically join near-net shaped structural building blocks into a composite part using an interfacial reaction-activation mechanism.