CTIA’s TZM Alloy in Aerospace Structural Components

CTIA’s TZM alloy (Titanium Zirconium Molybdenum) is manufactured through powder metallurgy processes. By precisely controlling Ti (0.40–0.55%), Zr (0.06–0.12%), and C (0.01–0.04%) contents, TiC and ZrC dispersion-strengthened phases are formed, providing excellent high-temperature strength, creep resistance, dimensional stability, and thermal cycling resistance. Aerospace high-temperature structural components are exposed to thermal loads, mechanical stresses, and severe temperature fluctuations during high-speed flight, requiring outstanding high-temperature performance and structural reliability. CTIA’s TZM alloy is suitable for load-bearing parts, support components, connecting parts, and precision structural components in aerospace engines, high-temperature testing equipment, space propulsion systems, and other high-temperature applications.

Advantages of CTIA’s TZM Alloy in Aerospace Structural Components
(1) High-Temperature Strength
Maintains reliable load-bearing capability under elevated temperatures to meet thermal load requirements of aerospace structural components.
(2) Excellent Creep Resistance
Reduces deformation under long-term high-temperature loads, maintaining component dimensional stability.
(3) Thermal Cycling Stability
Reduces thermal stress caused by temperature variations through a coefficient of thermal expansion of approximately 5.5–5.9×10⁻⁶/K.
(4) High-Temperature Microstructural Stability
Dispersion-strengthened phases inhibit grain growth and maintain long-term service performance under high-temperature conditions.

Applications of CTIA’s TZM Alloy in Aerospace Structural Components
(1) Aerospace Engine Components
Used for high-temperature load-bearing parts, support components, and connecting structures exposed to thermal and mechanical loads during operation.
(2) Space Propulsion Systems
Used for high-temperature structural supports and functional components under complex thermal cycling conditions.
(3) High-Temperature Testing Equipment
Used for load-bearing structures and fixing components to ensure stable operation during high-temperature testing.
(4) Advanced Thermal Protection and Material Processing Equipment
Used for critical high-temperature structural components to meet demanding thermal processing and testing requirements.

Specifications of CTIA’s TZM Alloy in Aerospace Structural Components
(1) Product Forms: TZM plates, rods, blocks, and precision-machined structural components.
(2) Dimensions: Customized sizes and complex structures are available.

CTIA GROUP has nearly 30 years of experience in molybdenum and molybdenum alloy manufacturing, specializing in TZM alloy production, powder metallurgy, and precision machining. With integrated manufacturing capabilities from raw material control to finished component processing, CTIA provides TZM plates, rods, blocks, and customized high-precision components for aerospace high-temperature structural applications. Strict quality control and process optimization ensure stable material performance and reliable operation under extreme high-temperature and high-load conditions.

For any inquiry, please contact molybdenum and molybdenum alloy manufacturer: CTIA GROUP

Email: sales@chinatungsten.com

Tel: 0086 592 5129696 / 0086 592 5129595

Website: www.molybdenum.com.cn

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