Corrosion-Resistant Zirconium Alloy for Nuclear Fuel Cladding

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Solution Overview

Problem

Conventional zirconium alloys used in nuclear fuel cladding tubes, such as Zircaloy-4, face accelerated corrosion and hydrogen brittleness issues under high-burnup conditions, limiting their corrosion resistance and mechanical properties, necessitating the development of improved alloys with enhanced corrosion resistance for nuclear reactors.

Innovation Solution

A zirconium alloy composition comprising 0.5 to 1.2 wt% Nb, 0.4 to 0.8 wt% Mo, 0.1 to 0.15 wt% Cu, and 0.15 to 0.2 wt% Fe, with optimized annealing processes including solution heat treatment, hot rolling, and multiple vacuum annealing steps, is developed to enhance corrosion resistance beyond that of Zircaloy-4, particularly in high-concentration Li atmospheres.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If conventional Zircaloy-2 and Zircaloy-4 are used for nuclear fuel cladding tubes, then the material provides basic corrosion resistance, but corrosion is accelerated under high-burnup conditions causing hydrogen brittleness and deteriorating mechanical properties

Engineering Contradiction:
Improvecorrosion resistanceVSAvoidmechanical properties
Core Design Contradiction:
ReliabilityVSStrength

Solution Approach 1:

The patent changes the chemical composition parameters by eliminating Sn and reducing Fe content while increasing Mo content to 0.4-0.8 wt%, and adjusts processing parameters by implementing multiple vacuum annealing steps at different temperatures (570-590°C, 560-580°C, 560-580°C) to control microstructure and achieve superior corrosion resistance and mechanical properties

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The patent creates a composite alloy system combining Zr, Nb, Mo, Cu, Fe, and O with specific compositional ratios, where Nb (0.5-1.2 wt%) and Mo (0.4-0.8 wt%) work synergistically to provide both corrosion resistance and mechanical strength, forming a multi-element composite material that overcomes the limitations of conventional binary or ternary alloys

Inventive Principle:
Principle #40Composite materials

2Reliability

If the amount of Sn is reduced to improve corrosion resistance, then corrosion resistance improves, but mechanical properties and strength may be compromised

Engineering Contradiction:
Improvecorrosion resistanceVSAvoidmechanical properties
Core Design Contradiction:
ReliabilityVSStrength

Solution Approach 1:

The patent changes the compositional parameters by setting Sn content to 0 wt% (complete elimination) and Fe content to 0.15-0.2 wt% (precise control), while increasing Mo content to 0.4-0.8 wt%, thereby achieving superior corrosion resistance without compromising mechanical properties through optimized element distribution

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The patent applies local quality by creating specific microstructural features through controlled vacuum annealing processes that produce fine precipitates and optimize grain structure in specific regions, allowing the material to exhibit different local properties that collectively provide both corrosion resistance and mechanical strength

Inventive Principle:
Principle #3Local quality

3Reliability

If multiple vacuum annealing steps are implemented to optimize microstructure, then corrosion resistance and mechanical properties improve, but manufacturing process complexity increases

Engineering Contradiction:
Improvecorrosion resistanceVSAvoidmanufacturing process complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent segments the annealing process into three distinct vacuum annealing steps at different temperature ranges (570-590°C for 3-4 hr, 560-580°C for 2-3 hr, and 560-580°C for 2-3 hr), with each step serving a specific microstructural purpose, thereby achieving superior material properties through systematic process division

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent applies preliminary action by performing solution heat treatment at 1000-1050°C for 30-40 min before the vacuum annealing sequence to homogenize the alloy composition and prepare the microstructure for subsequent controlled annealing, ensuring optimal final properties

Inventive Principle:
Principle #10Preliminary action

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 proposed zirconium alloy exhibits superior corrosion resistance, with weight gains ranging from 17 to 21 mg/dm² in pure water and 26 to 51 mg/dm² in a 70 ppm Li atmosphere after 100 days, significantly outperforming Zircaloy-4, and maintaining performance in high-concentration Li environments, thus ensuring improved durability for nuclear fuel cladding tubes and spacer grids.

Implementation Method 1

subjecting the ingot prepared in step (1) to solution heat treatment at 1,000 to 1,050° C. (β) for 30 to 40 min

Methodology Applied
Scientific EffectSolution heat treatment: Heat Treatment

Implementation Method 2

subjecting the material hot-rolled in step (3), to primary intermediate vacuum annealing at 570 to 590° C. for 3 to 4 hr

Methodology Applied
Scientific EffectAnnealing: Annealing

Data Source

PatentUS11195628B2Method of manufacturing a corrosion-resistant zirconium alloy for a nuclear fuel cladding tube
Publication Date: 2021.12.07 KEPCO NUCLEAR FUEL CO LTD
  • US11195628B2 patent drawing
  • US11195628B2 patent drawing
  • US11195628B2 patent drawing

AI summary

A method of manufacturing a zirconium alloy for a nuclear fuel cladding tube includes melting a mixture of 0.5 wt % of Nb, 0.4 wt % of Mo, 0.1 to 0.15 wt % of Cu, 0.15 to 0.2 wt % of Fe, and a balance of zirconium to prepare a melted ingot; heat treating the melted ingot at 1,000 to 1,050° C. for 30 to 40 min. followed by quenching in water to prepare a heat-treated ingot; preheating the heat-treated ingot at 630 to 650° C. for 20 to 30 min. to prepare a preheated ingot followed by hot rolling the preheated ingot at a reduction ratio of 60 to 65% to provide a hot-rolled material; thrice performing vacuum annealing followed by cold-rolling; and vacuum annealing a third cold-rolled material in a final vacuum annealing at 510 to 520° C. for 7 to 9 hrs. to provide the zirconium alloy as a cold-rolled material.