为保证飞机空调系统安全可靠运行,针对飞机空调系统各主要部件进行了故障模式影响分析(failure mode and effects analysis,简称FMEA),并结合故障树分析(fault tree analysis,简称FTA)方法,对飞机空调系统故障进行了诊断实验。同时利用M...为保证飞机空调系统安全可靠运行,针对飞机空调系统各主要部件进行了故障模式影响分析(failure mode and effects analysis,简称FMEA),并结合故障树分析(fault tree analysis,简称FTA)方法,对飞机空调系统故障进行了诊断实验。同时利用Matlab/Simulink软件建立了各部件的数值仿真模型,搭建了空调系统故障仿真平台,给出了系统关键部件的故障判据,对飞机空调系统进行了故障仿真,将实时数据与得到的仿真结果对比可以得出故障检修排序。以飞机座舱温度异常故障为例,阐述了飞机空调系统故障诊断方法。结果表明,涡轮故障时对座舱温度影响最大,在设计和维修中应重点考虑。展开更多
An aircraft cabin is a narrow,closed-space environment.To keep the air quality in cabin healthy for passengers,especially during an epidemic such as SARS-CoV-2(or 2019-nCoV)in 2020,a novel aircraft air conditioning sy...An aircraft cabin is a narrow,closed-space environment.To keep the air quality in cabin healthy for passengers,especially during an epidemic such as SARS-CoV-2(or 2019-nCoV)in 2020,a novel aircraft air conditioning system,called the ultra-high-temperature instantaneous sterilization air conditioning system(UHTACS),is proposed.Based on the proposed system,a simulation of the UHT-ACS is analysed in various flight states.In the UHT-ACS,the mixing air temperature of return and bleed air can reach temperature up to 148.8°C,which is high enough to kill bacilli and viruses in 2一8 s.The supply air temperature of the UHT-ACS in a mixing cavity is about 12 C in cooling mode both on the ground and in the air.The supply air temperature is about 42 C in heating mode.Compared with the air conditioning systems(ACS)of traditional aircraft the supply air temperatures of the UHT-ACS in the mixing cavity are in good agreement with those of a traditional ACS with 60%fresh air and 40%return air.Furthermore the air temperature at the turbine outlet of the UHT-ACS is higher than that of a traditional ACS which will help to reduce the risk of icing at the outlet.Therefore the UHT-ACS can operate normally in various flight states.展开更多
文摘为保证飞机空调系统安全可靠运行,针对飞机空调系统各主要部件进行了故障模式影响分析(failure mode and effects analysis,简称FMEA),并结合故障树分析(fault tree analysis,简称FTA)方法,对飞机空调系统故障进行了诊断实验。同时利用Matlab/Simulink软件建立了各部件的数值仿真模型,搭建了空调系统故障仿真平台,给出了系统关键部件的故障判据,对飞机空调系统进行了故障仿真,将实时数据与得到的仿真结果对比可以得出故障检修排序。以飞机座舱温度异常故障为例,阐述了飞机空调系统故障诊断方法。结果表明,涡轮故障时对座舱温度影响最大,在设计和维修中应重点考虑。
基金the Project Funded by the Priority Academic Program Development of Jiangsu Higher Education Institutions(PAPD)and the Foundation of Jiangsu Postdoctoral(No.2019K126)。
文摘An aircraft cabin is a narrow,closed-space environment.To keep the air quality in cabin healthy for passengers,especially during an epidemic such as SARS-CoV-2(or 2019-nCoV)in 2020,a novel aircraft air conditioning system,called the ultra-high-temperature instantaneous sterilization air conditioning system(UHTACS),is proposed.Based on the proposed system,a simulation of the UHT-ACS is analysed in various flight states.In the UHT-ACS,the mixing air temperature of return and bleed air can reach temperature up to 148.8°C,which is high enough to kill bacilli and viruses in 2一8 s.The supply air temperature of the UHT-ACS in a mixing cavity is about 12 C in cooling mode both on the ground and in the air.The supply air temperature is about 42 C in heating mode.Compared with the air conditioning systems(ACS)of traditional aircraft the supply air temperatures of the UHT-ACS in the mixing cavity are in good agreement with those of a traditional ACS with 60%fresh air and 40%return air.Furthermore the air temperature at the turbine outlet of the UHT-ACS is higher than that of a traditional ACS which will help to reduce the risk of icing at the outlet.Therefore the UHT-ACS can operate normally in various flight states.
