Cladding Structure with Transverse Secondary Bands

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Solution Overview

Problem

Machine components subjected to cyclic loading often experience premature fatigue and crack formation, leading to costly maintenance and potential catastrophic failure, as existing cladding strategies fail to effectively inhibit crack propagation in inter-pass clad boundaries.

Innovation Solution

A cladding structure featuring primary and secondary bands of cladding material deposited on a machine component's core, where primary bands are adjacent and abutting, and secondary bands are oriented transverse to inhibit crack propagation along inter-pass clad boundaries, thereby reducing stress concentrations and preventing crack propagation.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Duration of action of moving object

If machine components are subjected to cyclic loading, then operational functionality is maintained, but premature fatigue and crack formation occur

Engineering Contradiction:
Improveservice lifeVSAvoidfatigue resistance
Core Design Contradiction:
Duration of action of moving objectVSReliability

Solution Approach 1:

Different regions of the cladding are given different orientations to address local stress conditions. Primary and secondary bands are oriented differently to provide enhanced fatigue resistance in specific directions where stress concentrations are most likely to occur during cyclic loading.

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The cladding creates a composite structure with primary and secondary bands having different orientations and potentially different material compositions. This composite cladding structure provides superior fatigue resistance compared to conventional single-layer cladding by distributing cyclic stresses more effectively throughout the multi-directional structure.

Inventive Principle:
Principle #40Composite materials

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

The described cladding structure effectively inhibits crack propagation, reducing maintenance costs and extending the service life of machine components by interrupting crack paths and distributing stresses more uniformly, thus preventing critical failures.

Implementation Method 1

cladding the machine component may make the component more resistant to damage or failure by distributing stresses more uniformly across or through the materials of the machine component, and thereby reducing localized stress concentrations

Methodology Applied
Scientific EffectStress distribution:

Implementation Method 2

each of the secondary bands are oriented transverse to the primary bands to inhibit propagation of cracks through the cladding along directions of the primary bands

Methodology Applied
Scientific EffectCrack propagation inhibition: Fracture Mechanics

Implementation Method 3

a cladding extending throughout the at least one fatigue sensitive region. The cladding is formed by a set of primary bands of cladding material deposited upon and bonded to the core

Methodology Applied
Scientific EffectDeposition: Deposition (physical)

Data Source

PatentUS10479155B2Cladding structure and method
Publication Date: 2019.11.19 CATERPILLAR INC
  • US10479155B2 patent drawing
  • US10479155B2 patent drawing
  • US10479155B2 patent drawing

AI summary

A cladding structure and method for cladding machine components to inhibit crack propagation includes at least one set of primary bands, with each primary band being deposited adjacent to and abutting at least one other primary band, forming at least one inter-pass clad boundary, and at least one set of secondary bands deposited in a spaced configuration and oriented so as to intersect at least one inter-pass clad boundary.