Laser Cladding Impeller Shroud Manufacturing

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Solution Overview

Problem

Existing methods for manufacturing impeller assemblies face challenges in maintaining structural stability and efficiency, particularly when the overall size increases, due to deformation issues during welding and brazing processes, and difficulty in forming precise 3D blades and stable fillet portions.

Innovation Solution

The impeller assembly is manufactured using a laser cladding technique where a shroud is formed by melting and applying metal onto the blades, allowing for a stable and firm structure without the need for welding, and enabling the use of multiple layers for enhanced stability and precision.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If welding process is used to join shroud and impeller, then joining strength is improved, but thermal deformation increases causing fillet portion distortion

Engineering Contradiction:
Improvejoining strengthVSAvoidfillet portion precision
Core Design Contradiction:
StrengthVSManufacturing precision

Solution Approach 1:

The patent replaces the welding process (thermal field) with a laser cladding process that uses controlled metal deposition and rapid solidification. This substitution eliminates the excessive thermal input that causes fillet portion deformation while still achieving strong joining between the shroud and impeller blades through direct metal bonding.

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

Solution Approach 2:

The patent changes the thermal parameters by using laser cladding instead of conventional welding. The laser process provides concentrated, controlled thermal input with rapid cooling rates, which prevents the excessive heat accumulation that causes fillet portion distortion in traditional welding, while maintaining adequate joining strength.

Inventive Principle:
Principle #35Parameter changes

2Stability of the object's composition

If shroud thickness is increased to support large-sized impeller assembly, then structural stability is improved, but welding deformation increases due to excessive input power

Engineering Contradiction:
Improvestructural stabilityVSAvoiddeformation control
Core Design Contradiction:
Stability of the object's compositionVSManufacturing precision

Solution Approach 1:

The patent replaces conventional welding with laser cladding technology. This substitution allows the process to handle thick shrouds in large-sized impeller assemblies by providing controlled, concentrated energy input that melts and bonds material without generating the excessive thermal fields that cause deformation in traditional welding processes.

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

Solution Approach 2:

The laser cladding process applies thermal energy in a segmented, localized manner rather than as a broad thermal field. This segmentation of energy input allows the thick shroud to be processed without uniform thermal expansion and deformation, maintaining structural stability while enabling manufacturing of large-sized assemblies.

Inventive Principle:
Principle #1Segmentation

3Object-affected harmful factors

If vacuum brazing process is used to join shroud and impeller, then thermal damage to base material is reduced, but adhesive strength decreases and fillet portion deforms due to cooling rate variation

Engineering Contradiction:
Improvethermal damage to base materialVSAvoidadhesive strength
Core Design Contradiction:
Object-affected harmful factorsVSStrength

Solution Approach 1:

The patent replaces the vacuum brazing process with laser cladding. This substitution eliminates the need for filler materials and achieves direct metal-to-metal bonding between the shroud and impeller blades, resulting in superior adhesive strength comparable to or exceeding conventional welding, while maintaining the advantage of localized thermal input that prevents base material damage.

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

Solution Approach 2:

The laser cladding process creates a composite structure where the cladded metal forms a strong metallurgical bond with the base material. This composite approach eliminates the intermediate filler material layer used in brazing, achieving direct bonding with higher strength while the controlled laser parameters prevent excessive thermal damage to the base material.

Inventive Principle:
Principle #40Composite materials

4Manufacturing precision

If fillet portion size is reduced to about 0.8 mm radius, then joining precision is improved, but stress concentration increases making it unsuitable for large-sized products

Engineering Contradiction:
Improvejoining precisionVSAvoidstress resistance
Core Design Contradiction:
Manufacturing precisionVSStrength

Solution Approach 1:

The laser cladding process enables precise control of the fillet portion dimensions and geometry through parameter optimization. The process can create fillet portions with radii larger than 0.8 mm while maintaining precise joining, and the gradual transition of material provides stress distribution that reduces stress concentration, making it suitable for large-sized products.

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The patent replaces conventional joining methods that create small, stress-concentrated fillets with laser cladding that can create optimized fillet geometries. The controlled deposition and solidification process allows for larger, more gradual fillet transitions that reduce stress concentration while maintaining joining precision, enabling application to large-sized impeller assemblies.

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 method simplifies the manufacturing process, ensures structural stability, and allows for the production of both large and small-sized impeller assemblies with improved mechanical performance and reduced thermal deformation, enabling efficient fluid compression.

Implementation Method 1

a shroud is formed by melting and applying metal onto the blades

Methodology Applied
Scientific EffectLaser: Laser

Implementation Method 2

the shroud is formed by melting a metal and applying the melted metal onto the radially outward portions of plurality of blades

Methodology Applied
Scientific EffectMelting: Melting

Data Source

PatentUS9835163B2Impeller assembly of fluid rotary machine and manufacturing method thereof
Publication Date: 2017.12.05 HANWHA AEROSPACE CO LTD
  • US9835163B2 patent drawing
  • US9835163B2 patent drawing
  • US9835163B2 patent drawing

AI summary

Provided is a method of manufacturing an impeller assembly, the method including providing an impeller including: a rotary shaft; a base portion radially extending outward from the rotary shaft; and a plurality of blades extending radially outward from the rotary shaft and disposed on the base portion, each of the plurality of blades provided apart from one another in a circumferential direction around the rotary shaft; providing a mold in an area between the plurality of blades; and forming a shroud covering upper portions of the plurality of blades and an upper portion of the mold, wherein the forming the shroud comprises applying a melted metal on the upper portions of the plurality of blades and the upper portion of the mold.