In-situ test platform based on function simulation of aircraft temperature control system

The invention provides an in-situ test platform based on the function simulation of an aircraft temperature control system, which comprises a signal processing system and a simulation workstation, wherein the signal processing system comprises a receiving assembly and a transmitting assembly, and th...

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Bibliographische Detailangaben
Hauptverfasser: ZHAO HONGXU, JIANG GUIJIA, CHAO DI, JIANG HONGYE, YANG ZHANGANG, YANG YONGFEI
Format: Patent
Sprache:chi ; eng
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Zusammenfassung:The invention provides an in-situ test platform based on the function simulation of an aircraft temperature control system, which comprises a signal processing system and a simulation workstation, wherein the signal processing system comprises a receiving assembly and a transmitting assembly, and the signal processing system is mainly used for the conversion between signals and data; and the simulation workstation includes a data reading module, a temperature simulation module and a data storage module, and the simulation workstation is mainly used for simulating the working process of an airconditioning assembly and the temperature distribution state of a passenger cabin. The beneficial effects are that the in-situ test platform combines a virtual instrument technology and software simulation, can test a temperature control panel in situ without the air conditioning assembly and is applicable to testing the temperature control panel in an aircraft final assembly stage. Meanwhile, thesimulation workstation ca