The invention provides a civil helicopter ground joint test manned rotor control system which comprises a flight control system displacement sensor 1, an analog signal acquisition device 2, a data acquisition and processing computer 3, a control display computer 4, a control display computer support 5, a test cable 6 and a data cable 7. Wherein the flight control system displacement sensor 1 comprises at least four displacement sensors, each displacement sensor is connected with the input end of the analog signal acquisition equipment 2 through the test cable 6, and the output end of the analog signal acquisition equipment 2 is connected with the input end of the data acquisition and processing computer 3 through the data cable 7; the output end of the data acquisition and processing computer 3 is connected with the control display computer 4 through a data cable 7; the control display computer 4 is arranged in a cockpit instrument panel 5.3 of the helicopter; the flight control system displacement sensor 1 is used for measuring the input quantity of a control system booster on a helicopter.
本申请提供一种民用直升机地面联合试验有人旋翼操纵系统,所述系统包括飞行操纵系统位移传感器1、模拟信号采集设备2、数据采集及处理计算机3、操纵显示计算机4、操纵显示计算机支架5、测试线缆6、数据线缆7,其中:飞行操纵系统位移传感器1包括至少四个位移传感器,每个位移传感器均通过测试线缆6与模拟信号采集设备2的输入端连接,模拟信号采集设备2的输出端通过数据线缆7与数据采集及处理计算机3的输入端连接,数据采集及处理计算机3的输出端通过数据线缆7与操纵显示计算机4连接;操纵显示计算机4设置在直升机的驾驶舱仪表板5.3内;飞行操纵系统位移传感器1是直升机上用于测量操纵系统助力器的输入量。
Civil helicopter ground joint test manned rotor control system
一种民用直升机地面联合试验有人旋翼操纵系统
2024-01-16
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 |
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