Research on Safety of Aero-Engine Oil Pipe Under Heating Conditions Based on Fluid–Solid Thermal Coupling

Author:

Yang Yuepeng1,Wang Fang123,Wen Fang1,Jin Jie123

Affiliation:

1. School of Energy and Power Engineering, Beihang University (BUAA), Beijing 100191, China

2. Jiangxi Research Institute, Beihang University (BUAA), Nanchang 330096, China

3. Chengdu Innovation Research Institute on Aircraft Power, Beihang University (BUAA), Chengdu 611930, China

Abstract

This paper examines the safety of aero-engine pipelines under different heating conditions. Based on the fire test standard documents, a model of an aero-engine oil pipe was constructed, and its safety under heating conditions that meet the standard was analyzed using fluid–solid thermal coupling. The pipe material was stainless steel 1Cr18Ni9Ti, and the oil inside the pipeline was China RP-3 kerosene. To simulate the different working conditions or pump failure scenarios, various kerosene inlet flow rates were used for the calculations. The results indicate that the pipe wall exhibits an uneven temperature distribution under standard heating conditions. As the kerosene flow rate decreases, the pipe wall temperature rises, and heat transfer deterioration occurs. The increase in the pipe wall temperature reduces the material’s strength, while the uneven temperature distribution generates thermal stress, further increasing the safety risk. When the kerosene flow rate is reduced to a certain level, the equivalent stress in the pipe wall exceeds the material’s yield strength, leading to a high risk of rupture.

Funder

National Natural Science Foundation

Publisher

MDPI AG

Reference28 articles.

1. He, J., Sun, Y., and Wang, F. (2010, January 12). Analysis of airworthiness requirements for powerplant fire protection of transport category. Proceedings of the 2010 Airworthiness and Air Traffic Management Academic Annual Meeting, Beijing, China.

2. Ministry of Transport of the People’s Repiblic of China (2016). Aviation Engine Airworthiness Regulations.

3. US Department of Transportation, Federal Aviation Administration (2013). Airworthiness Standards: Aircraft engines, Federal Aviation Regulations.

4. European Union Aviation Safety Agency (2009). Certification Specification for Engine CS-E.

5. Wang, W., Lv, K., and Ye, Z. (2015, January 19). Convection and Radiation Heat Transfer Calculation of Aero-engine Fire Test. Proceedings of the CSAA Symposium on Aircraft Fire Protection System (2nd SAFPS 2015), Hefei, China.

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