The invention belongs to the technical field of airplane component strength testing, and particularly relates to an airplane component strength testing heating device which comprises: a box body, wherein the box body is provided with an inert gas inlet communicated with the internal space of the box body, an inert gas outlet communicated with the internal space of the box body and a radiation heating window communicated with the internal space of the box body; a graphite heating element which is arranged in the internal space of the box body; and glass which is arranged in the radiation heating window and blocks the radiation heating window, wherein the graphite heating element can radiatively heat the aircraft component through the glass. In addition, the invention relates to an airplane component strength testing heating method implemented based on the airplane component strength testing heating device.
本申请属于飞机部件强度测试技术领域,具体涉及一种飞机部件强度测试加热装置,包括:箱体,箱体上具有与其内部空间连通的惰性气体进口、与其内部空间连通的惰性气体出口、与其内部空间连通的辐射加热窗口;石墨加热元件,石墨加热元件在箱体内部空间内设置;玻璃,玻璃在辐射加热窗口中设置,将辐射加热窗口封堵;石墨加热元件能够透过玻璃对飞机部件进行辐射加热。此外,涉及一种基于上述飞机部件强度测试加热装置实施的飞机部件强度测试加热方法。
Airplane component strength testing heating device and method thereof
一种飞机部件强度测试加热装置及其方法
2021-07-02
Patent
Electronic Resource
Chinese
IPC: | G01N Untersuchen oder Analysieren von Stoffen durch Bestimmen ihrer chemischen oder physikalischen Eigenschaften , INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES / 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 |
Strength testing in airplane construction
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