Mg Casting Alloys for the Aerospace Challenge

Abstract

- Core Objective of the Research: To evaluate the advantages and disadvantages of currently available magnesium casting alloys for aerospace applications, and to develop improved alloys and casting techniques that offer enhanced high-temperature capability, improved corrosion resistance, and the ability to produce larger, more complex castings with weight savings.

- Primary Methodology: The research involved a combination of materials characterization, alloy development, and casting process optimization. Existing magnesium alloys (Mg-Al-Zn and Mg-Zn-Zr systems) were analyzed to understand their limitations. New alloys were designed and developed by incorporating rare earth elements, zirconium, and other alloying additions to improve high-temperature strength, creep resistance, and weldability. Advanced casting techniques, such as resin-bonded sand casting and fluxless melting, were employed and evaluated to enhance the production of complex and larger castings.

- Key Results: The study identified limitations in existing Mg-Al-Zn alloys (e.g., susceptibility to stress corrosion cracking and rapid strength degradation above 250°F). The development of Mg-Zn-Zr alloys provided improved properties including better weldability and reduced hot cracking. The introduction of silver and neodymium-rich rare earths further enhanced high-temperature properties. The research culminated in the development of a novel magnesium alloy, WE54, which exhibits superior high-temperature properties compared to existing alloys and certain aluminum alloys. Significant advancements in casting technology, including resin-bonded sand casting and fluxless melting, enabled the production of larger, more complex castings with thinner wall thicknesses and closer tolerances.

Researcher Information:

- Affiliation: The paper does not explicitly state the author's affiliation.
- Author: A. Stevenson
- Primary Research Area: The paper does not explicitly state the author's primary research area. However, based on the content, it can be inferred as materials science and engineering, specifically focusing on magnesium alloys and casting technology.

Research Background and Objectives:

The aerospace industry demands materials with high strength-to-weight ratios, excellent high-temperature performance, and good corrosion resistance. Magnesium alloys offer significant weight advantages compared to aluminum and titanium alloys, but their applications in aerospace have been limited due to certain technological challenges. These challenges include:

  • Limited High-Temperature Properties: Conventional magnesium casting alloys exhibit a significant drop in mechanical properties at elevated temperatures, limiting their use in high-temperature aerospace components.
  • Susceptibility to Corrosion: Magnesium alloys are susceptible to corrosion, especially in harsh environments. Improved corrosion resistance is crucial for long-term durability.
  • Casting Limitations: Producing complex and large-sized castings with thin walls and close tolerances has been historically difficult with magnesium alloys due to their inherent casting characteristics, like microporosity and susceptibility to hot cracking.
  • Weldability Issues: Some magnesium alloys exhibit poor weldability, further restricting their applications in complex assemblies.

The objective of this research was to address these limitations by:

  1. Evaluating the strengths and weaknesses of existing magnesium casting alloys used in aerospace applications.
  2. Developing new magnesium alloys with enhanced high-temperature strength, creep resistance, corrosion resistance, and improved weldability.
  3. Improving casting techniques to enable the production of larger, more complex components with thinner walls and tighter tolerances while reducing weight.
Figure 6, This casting, produced in ZE41, weighs 620 Ibs. and is the main gearbox for the Westland WG34 helicopter.
Figure 6, This casting, produced in ZE41, weighs 620 Ibs. and is the main gearbox for the Westland WG34 helicopter.
Figure 7, Shown is a sectioned gearbox casting, revealing cored passageways.
Figure 7, Shown is a sectioned gearbox casting, revealing cored passageways.

Main Objectives and Research Content of the Paper:

The paper systematically addresses the challenges associated with the use of magnesium alloys in aerospace applications. It breaks down the research into these key areas:

1. Analysis of Existing Magnesium Alloys:

The paper begins by classifying magnesium casting alloys into two main categories: Mg-Al-Zn alloys and Mg-Zn-Zr alloys. It discusses the compositional variations within each system and their impact on mechanical properties, including yield strength, ultimate tensile strength, elongation, and fatigue strength. The influence of heat treatment on these properties is also examined, showing how different heat treatments (T4, T5, T6) affect the microstructure and, consequently, the mechanical behavior. The limitations of these existing alloys, particularly their susceptibility to stress corrosion cracking, microporosity, and the limitations in high-temperature performance, are highlighted.

2. Development of New Magnesium Alloys:

The research focuses on the development of novel magnesium alloys that overcome the shortcomings of existing systems. This involved exploring different alloying additions, including rare earth elements (RE), zirconium (Zr), and thorium (Th). The addition of Zr significantly improved grain refinement, leading to enhanced mechanical properties. The inclusion of rare earth elements along with Th enhanced the weldability and reduced susceptibility to hot cracking. The addition of silver and neodymium-rich rare earths significantly improved high-temperature properties, while the substitution of copper for part of the silver provided cost advantages. The research meticulously describes the effects of varying the proportions of these elements on the final alloy properties. Specific attention is paid to the alloys QE22A, QH21, EQ21, and ZE63A. The details of their composition, heat treatment, and resulting mechanical properties are presented. The development of WE54, a Mg-Y/Nd/Zr alloy, is a pivotal finding, exhibiting significantly improved creep resistance and high-temperature strength compared to existing magnesium alloys and even some aluminum alloys.

3. Optimization of Casting Techniques:

The paper emphasizes the crucial role of casting techniques in achieving high-quality magnesium components. The transition from CO2-silicate processes to resin-bonded sand casting systems is described, highlighting the improvements in the casting complexity, dimensional accuracy, and surface finish achievable with the newer methods. The development of techniques to produce longer and narrower cored passageways is a key advancement, enabling the creation of more intricate and complex castings. The adoption of fluxless melting further enhances the casting process by minimizing oxidation and improving the quality of the final product.

4. Comprehensive Testing and Evaluation:

The research includes a robust experimental program involving tensile testing, creep testing, fatigue testing, and fracture toughness testing. The results of these tests are presented in tabular and graphical formats, providing quantitative data on the mechanical properties of the developed alloys. The data highlights the improved high-temperature strength, creep resistance, and fatigue strength of the novel alloys, specifically WE54. Comparisons are made with both existing magnesium alloys and comparable aluminum alloys to demonstrate the advancements achieved. Detailed microstructural analysis was likely performed (though not explicitly described in the provided text) to understand the correlation between the alloy composition, heat treatment, and the resulting mechanical properties.

Results and Achievements:

The research yielded significant advancements in both magnesium alloy development and casting technologies:

  • Development of High-Performance Alloys: The research successfully developed new magnesium alloys with significantly improved high-temperature properties, including the WE54 alloy that surpasses existing magnesium alloys and even some aluminum alloys in certain performance metrics.
  • Advancements in Casting Technology: The adoption of resin-bonded sand casting and fluxless melting enabled the production of complex, larger castings with thinner walls, tighter tolerances, and improved surface finishes.
  • Enhanced Weldability: Certain alloy compositions resulted in enhanced weldability, facilitating the construction of complex assemblies.
  • Improved Creep Resistance: The WE54 alloy demonstrated exceptional creep resistance, an essential property for high-temperature aerospace applications.
  • Reduced Microporosity: Improved casting techniques led to a significant reduction in microporosity, enhancing the pressure tightness of the castings.

Copyright and References:

This summary is based on the paper "Mg Casting Alloys for the Aerospace Challenge" by A. Stevenson. This summary is for informational purposes only and should not be used for commercial purposes without proper authorization.