ZHANG Qing, SHEN Xi-gang, NIU Kun, YAO Zhu-lin.Airworthiness Additional Integrity Assessment Method and Verification of Bird Ingestion for a TurbofanEngine[J].航空发动机,2024,50(5):97-104
Airworthiness Additional Integrity Assessment Method and Verification of Bird Ingestion for a TurbofanEngine
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Key Words:bird ingestion  turbofan engine  airworthiness  compliance verification
Author NameAffiliation
ZHANG Qing, SHEN Xi-gang, NIU Kun, YAO Zhu-lin AECC Shenyang Engine Research InstituteShenyang 110015China 
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Abstract:In order to explore the airworthiness compliance verification method applicable to China's turbofan engines, according to the airworthiness compliance verification requirements of bird ingestion, combined with the development of turbofan engines, focusing on the medium bird additional integrity assessment requirements, the test system requirements were put forward including test engine, test bed, special equipment for bird ingestion test, instrumentation scheme and so on. The specific test methods were proposed covering fan blade identification, bird launch system layout, bird projection parameter calibration, and bird (projectile) preparation, etc. The test parameters are established from the aspects of bird mass, projection position, projection speed, test conditions, and test procedure. Accord? ing to the established compliance verification method, the test verification of a turbofan engine was completed within an open-air test bed, and the exploration and practice of turbofan engine bird ingestion airworthiness compliance method in China was carried out. The results show that the engine thrust loss was 2% after the bird (projectile) with a mass of 0.71 kg was fired into an area at a blade span height of 70% with a speed of 99 m/s, which verifies the ability of stable operation of the turbofan engine after bird ingestion, and lays the foundation for subsequent turbofan engine bird ingestion airworthiness compliance research and verification.
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