The invention provides a compact redundancy design leakage simulation device for civil aircraft test flight. The device comprises a control module, a water storage module, a pressure stabilization module and a redundancy flow regulation module, the water storage module is connected with the pressure stabilizing module, and the pressure stabilizing module is connected with the redundant flow adjusting module; the control module is connected with the water storage module, the pressure stabilizing module and the redundant flow adjusting module. The device has the advantages of being convenient to install, high in universality, diversified in combination and wide in application range.
本发明提供了一种关于民机试飞紧凑型冗余设计模拟泄露的装置,包括:控制模块、储水模块、稳压模块和冗余式流量调节模块;所述储水模块与所述稳压模块连接,所述稳压模块与所述冗余式流量调节模块连接;所述控制模块分别与所述储水模块、所述稳压模块和所述冗余式流量调节模块连接。本发明具有安装方便,通用性强,组合多样化的特点,且适用范围广泛。
Civil aircraft test flight compact redundancy design leakage simulation device
一种关于民机试飞紧凑型冗余设计模拟泄露的装置
2023-06-27
Patent
Electronic Resource
Chinese
IPC: | B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen |
Flight Control Simulation System Design of a Civil Aircraft
British Library Conference Proceedings | 2012
|Computer redundancy for aircraft flight control
AIAA | 1977
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