The invention relates to a test flight test data acquisition system for a double-wing general-purpose aircraft. The test flight test data acquisition system comprises a left upper wing data acquisition assembly mounted on a left upper wing of the aircraft, a cockpit internal data acquisition assembly mounted in a cockpit, a passenger cabin data acquisition assembly mounted in a passenger cabin and a tail cabin data acquisition assembly mounted in a tail cabin, the left upper wing data acquisition assembly, the cockpit internal data acquisition assembly, the passenger cabin data acquisition assembly and the stern room data acquisition assembly are all connected with the data recorder through data lines; and after the flight is finished, the recorded data is exported, and the data acquired by the test flight can be analyzed and researched, so that whether the maneuverability of the aircraft meets the requirements of related airworthiness clauses or not is verified.
本发明涉及一种双翼通用飞机试飞测试数据采集系统,其包括安装在飞机左上翼的左上翼数据采集组件、安装在驾驶舱内的驾驶舱内数据采集组件、安装在客舱内的客舱数据采集组件以及安装在尾舱内的尾舱数据采集组件;所述左上翼数据采集组件、驾驶舱内数据采集组件、客舱数据采集组件以及尾舱数据采集组件均通过数据线与数据记录仪连接;在飞行结束后,导出记录的数据,即可对试飞采集到的数据进行分析研究,从而验证飞机操纵性是否满足相关适航条款的要求。
Universal double-wing aircraft test flight test data acquisition system
一种双翼通用飞机试飞测试数据采集系统
2024-03-22
Patent
Elektronische Ressource
Chinesisch
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 / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
A Flight Test Avionics Data Acquisition System for Future Fokker Aircraft
British Library Conference Proceedings | 1995
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