Regional turbofan aircraft,which are used for medium-short distances,have a heightened risk of high-altitude Wake Vortices(VV)because of their tail-mounted engines and high horizontal tail configurations.For some regi...Regional turbofan aircraft,which are used for medium-short distances,have a heightened risk of high-altitude Wake Vortices(VV)because of their tail-mounted engines and high horizontal tail configurations.For some regional medium-short-range turbofan aircraft,this threat is higher than that for conventionally designed aircraft.To analyze the flight safety of turbofan aircraft during cruise,this study developed a model to assess wake vortex encounters based on evolutionary high-altitude wake flow patterns.First,the high-altitude wake vortex aircraft dissipation patterns were analyzed by combining Quick Access Recorder(QAR)flight data with the wake vortex evolution model.Then,to consider the uniqueness of the medium-short-range turbofan aircraft,the severity of the wake vortex encounters was simulated using an induced roll moment coefficient.The proposed high-altitude wake vortex encounter model was able to identify and assess the highaltitude wake vortex changes,the bearing moments at different altitudes,and the atmospheric pressure conditions.Using the latest wake separation standards from the International Civil Aviation Organization(ICAO),acceptable safety wake intervals for follower aircraft in different scenarios were determined for the safety assessment.The results indicate that compared to mid and low altitudes,the high-altitude aircraft wake vortex dissipation rate is faster,the ultimate bearing moment is weaker,and the roll moment coefficient is higher,which confirm that there is elevated wake vortex encounter severity for regional turbofan aircraft.As safety is found to deteriorate when encountering wake vortices at altitudes higher than 8 km,new medium-short-range turbofan regional aircraft require higher safety margins than the latest wake separation standards.展开更多
The reliability assessment of aircraft ejection separation systems is crucial for aviation safety,but traditional methods exhibit significant shortcomings in dynamic behavior modeling,rare event quantification,and bid...The reliability assessment of aircraft ejection separation systems is crucial for aviation safety,but traditional methods exhibit significant shortcomings in dynamic behavior modeling,rare event quantification,and bidirectional consistency verification of function and fault paths.This paper proposes an innovative GO-FTA-GERTS dual model that integrates goal-oriented(GO)methods,fault tree analysis(FTA),and graphical evaluation and review technique(GERT)networks.The core innovation lies in constructing a bidirectional logical interlocking mechanism between the GO success tree and the FTA failure tree,leveraging the dynamic state transfer characteristics of GERT to achieve mathematical equivalence verification of function paths and fault paths.Using a specific aircraft ejection subsystem as an example,the model demonstrates excellent accuracy in ultra-low failure probability calculations:the mean system failure probability calculated by the FTA-GERT network is approximately 5.26×10^(−10) per flight hour,meeting airworthiness standards.At the same time,Monte Carlo simulation and Welch’s t-test are also used to verify that the success probability of GO-GERT model is strictly complementary to the system failure probability calculated by FTA-GERT network.This novel model effectively addresses the limitations of static analysis,dynamic path quantification,and rare event evaluation,providing a new method for reliability analysis of critical aviation safety systems.展开更多
基金supported by the National Natural Science Foundation of China(Nos.U2333209,U1733203)the National Key R&D Program of China(No.2021YFF0603904)the Civil Aviation Administration of China(No.AQ20200019)。
文摘Regional turbofan aircraft,which are used for medium-short distances,have a heightened risk of high-altitude Wake Vortices(VV)because of their tail-mounted engines and high horizontal tail configurations.For some regional medium-short-range turbofan aircraft,this threat is higher than that for conventionally designed aircraft.To analyze the flight safety of turbofan aircraft during cruise,this study developed a model to assess wake vortex encounters based on evolutionary high-altitude wake flow patterns.First,the high-altitude wake vortex aircraft dissipation patterns were analyzed by combining Quick Access Recorder(QAR)flight data with the wake vortex evolution model.Then,to consider the uniqueness of the medium-short-range turbofan aircraft,the severity of the wake vortex encounters was simulated using an induced roll moment coefficient.The proposed high-altitude wake vortex encounter model was able to identify and assess the highaltitude wake vortex changes,the bearing moments at different altitudes,and the atmospheric pressure conditions.Using the latest wake separation standards from the International Civil Aviation Organization(ICAO),acceptable safety wake intervals for follower aircraft in different scenarios were determined for the safety assessment.The results indicate that compared to mid and low altitudes,the high-altitude aircraft wake vortex dissipation rate is faster,the ultimate bearing moment is weaker,and the roll moment coefficient is higher,which confirm that there is elevated wake vortex encounter severity for regional turbofan aircraft.As safety is found to deteriorate when encountering wake vortices at altitudes higher than 8 km,new medium-short-range turbofan regional aircraft require higher safety margins than the latest wake separation standards.
基金supported by Shanghai Central Guidance Science and Technology Development Fund(NO:YDZX20233100004008)National Natural Science Foundation of China(NO:T2441003).
文摘The reliability assessment of aircraft ejection separation systems is crucial for aviation safety,but traditional methods exhibit significant shortcomings in dynamic behavior modeling,rare event quantification,and bidirectional consistency verification of function and fault paths.This paper proposes an innovative GO-FTA-GERTS dual model that integrates goal-oriented(GO)methods,fault tree analysis(FTA),and graphical evaluation and review technique(GERT)networks.The core innovation lies in constructing a bidirectional logical interlocking mechanism between the GO success tree and the FTA failure tree,leveraging the dynamic state transfer characteristics of GERT to achieve mathematical equivalence verification of function paths and fault paths.Using a specific aircraft ejection subsystem as an example,the model demonstrates excellent accuracy in ultra-low failure probability calculations:the mean system failure probability calculated by the FTA-GERT network is approximately 5.26×10^(−10) per flight hour,meeting airworthiness standards.At the same time,Monte Carlo simulation and Welch’s t-test are also used to verify that the success probability of GO-GERT model is strictly complementary to the system failure probability calculated by FTA-GERT network.This novel model effectively addresses the limitations of static analysis,dynamic path quantification,and rare event evaluation,providing a new method for reliability analysis of critical aviation safety systems.
