Turbine Nozzle Insert Repair via Plug Welding

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Turbine nozzle assemblies in air cycle machines face challenges in maintaining containment requirements during repair, particularly under high axial loads, as existing repair methods may compromise the structural integrity and safety standards.

Innovation Solution

A method involving the use of an insert secured to the support structure of the turbine nozzle assembly via plug welds, ensuring the assembly remains integral and maintains containment capacity, even under extreme conditions.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of repair

If repair work is performed on the turbine nozzle assembly, then maintenance and repair needs are met, but the containment capacity and structural integrity are compromised

Engineering Contradiction:
Improverepair capabilityVSAvoidcontainment capacity
Core Design Contradiction:
Ease of repairVSReliability

Solution Approach 1:

The support structure is divided into an insert portion and a base structure. The insert can be independently replaced during repair while the base structure remains intact, allowing maintenance without compromising the overall containment capacity of the assembly.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The insert is extracted as a separate replaceable component from the support structure. This allows the insert to be removed and replaced during repair operations, enabling maintenance while preserving the integrity of the main containment structure.

Inventive Principle:
Principle #2Taking out (Extraction)

2Strength

If the turbine nozzle assembly is designed to withstand high axial loads, then safety requirements are met, but the complexity of repair work increases

Engineering Contradiction:
Improveaxial load capacityVSAvoidrepair complexity
Core Design Contradiction:
StrengthVSDevice complexity

Solution Approach 1:

The support structure is segmented into a replaceable insert and a permanent base structure. This segmentation allows the high-strength requirements to be concentrated in the insert design, while the base structure provides stable mounting, simplifying repair operations.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The insert is designed as a sacrificial component that can be replaced rather than repaired. This allows the use of high-strength materials and designs optimized for load-bearing, while the replaceable nature simplifies maintenance by eliminating complex repair procedures.

Inventive Principle:
Principle #27Cheap short-living objects (Disposable)

3Reliability

If the insert is securely attached to the support structure, then containment requirements are maintained, but the manufacturing complexity increases

Engineering Contradiction:
Improvecontainment integrityVSAvoidmanufacturing simplicity
Core Design Contradiction:
ReliabilityVSEase of manufacture

Solution Approach 1:

The insert and base structure are designed with compatible materials and geometric features that simplify the welding process. The attachment interface uses standardized configurations that reduce manufacturing complexity while ensuring secure attachment and maintaining containment integrity.

Inventive Principle:
Principle #33Homogeneity

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 solution enables the turbine nozzle assembly to withstand high axial loads and maintain safety standards during containment events, improving durability and reducing downtime by providing a robust and reliable repair method that integrates the insert and support structure as a single, secure unit.

Implementation Method 1

plug welding the insert to the support structure of the turbine nozzle assembly

Methodology Applied
Scientific EffectWelding: Welding

Data Source

PatentUS8770933B2Turbine nozzle assemblies and methods for repairing turbine nozzle assemblies
Publication Date: 2014.07.08 HONEYWELL INTERNATIONAL INC
  • US8770933B2 patent drawing
  • US8770933B2 patent drawing
  • US8770933B2 patent drawing

AI summary

A method is provided for repairing a turbine nozzle assembly with an insert and a support structure. The method includes positioning the insert on the support structure of the turbine nozzle assembly; and plug welding the insert to the support structure of the turbine nozzle assembly.