The invention relates to an airplane anti-disturbance icing dynamic measuring system and method, the measuring system comprises an icing signal conversion device and a control system, the signal conversion device comprises an air pressure diaphragm capsule, a connecting rod mechanism, a closed shell, a first probe and a second probe, the air pressure diaphragm capsule is arranged in the closed shell, the air pressure diaphragm capsule is provided with two opposite stress ends, and the first probe and the second probe are arranged in the closed shell. The two stress ends are communicated through a pipeline, the two stress ends of the air pressure diaphragm capsule are connected with the control system through the connecting rod mechanism, the first probe and the second probe are connected to the closed shell, the first probe is communicated with an inner cavity of the closed shell, and the second probe is communicated with an inner cavity of the air pressure diaphragm capsule. And the control system comprises a power supply, a microswitch and an alarm indicator.
一种飞机防扰动结冰动态测量系统及测量方法,该测量系统含有结冰信号转换装置和控制系统,信号转换装置含有气压膜盒、连杆机构、封闭壳体以及第一探针和第二探针,所述的气压膜盒设置在封闭壳体内,气压膜盒有两个相对的应激端,两个应激端之间通过管路连通,所述的连杆机构将气压膜盒的两个应激端与控制系统连接,所述的第一探针和第二探针连接在封闭壳体上,第一探针与封闭壳体内腔连通,第二探针与气压膜盒的内腔连通,所述的控制系统含有电源、微动开关和告警指示。
Aircraft anti-disturbance icing dynamic measurement system and measurement method
一种飞机防扰动结冰动态测量系统及测量方法
2024-10-22
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
European Patent Office | 2022
|NTIS | 1971
European Patent Office | 2017
|European Patent Office | 2019
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