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Publishing Language: Chinese

Critical ignition conditions of TiAl alloy under simulated compressor conditions

Yang YANG, Wentian YU, Runlin LU, Lili ZHENG( )
School of Aerospace Engineering, Tsinghua University, Beijing 100084, China
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Abstract

To extend the engineering applications of TiAl alloy in hot-section components of high-pressure compressors, it is essential to clarify its ignition boundaries under realistic service conditions. Focusing on the flammability of TiAl alloy under compressor conditions, the surface oxidation reaction rate of TiAl is obtained using both experimental energy balance analysis method and first-principles approach combined with thermodynamic statistics. The effects of incoming flow velocity, temperature, pressure, and angle of attack on the thermal autoignition of TiAl alloy are investigated via numerical simulation. The critical external energy density required for forced ignition under typical multistage compressor design-point conditions is also determined. Results show that although increased pressure promotes surface oxidation, it concurrently enhances convective heat transfer, thereby raising the critical incoming flow temperature for autoignition. At high angles of attack, flow separation significantly reduces heat transfer efficiency, leading to a lower critical autoignition temperature. Under typical simulated conditions of a multi-stage compressor, TiAl alloy does not spontaneously ignite without external energy. However, when the external energy density reaches the thermal levels corresponding to faults such as blade tip friction, there is a risk of forced ignition.

CLC number: V19 Document code: A Article ID: 1000-6893(2026)20-133152-11

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Acta Aeronautica et Astronautica Sinica

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Cite this article:
YANG Y, YU W, LU R, et al. Critical ignition conditions of TiAl alloy under simulated compressor conditions. Acta Aeronautica et Astronautica Sinica, 2026, 47(20). https://doi.org/10.7527/S1000-6893.2026.33152

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Received: 27 November 2025
Revised: 22 December 2025
Accepted: 18 May 2026
Published: 26 May 2026
© 2026 The Journal of Acta Aeronautica et Astronautica Sinica