The invention discloses a flow display control device for an aircraft oxygen system, which comprises a shell, and a cavity B and a cavity D are arranged at the lower end of the shell and are respectively connected with an air inlet pipeline and an air outlet pipeline; a cavity C is formed in the upper end of the cavity D, and the cavity B is communicated with the cavity D through the cavity C; a flow limiter is arranged at the communicated part of the upper end of the cavity D and the cavity C; a mounting cavity is formed in the portion, above the cavity B, of the shell, a cap is assembled on the mounting cavity, a pressure sensing diaphragm, a pressing ring and an indicating gasket are arranged below the cap, and the pressure sensing diaphragm is arranged at the bottom of the mounting cavity and can expand upwards when the interior of the pressure sensing diaphragm is pressed. The circumference of the pressure sensing diaphragm is fixedly sealed through a pressing ring. The indication gasket is installed above the pressing ring, the indication gasket is of a circular structure made of rubber, and a cross-shaped notch is formed in the indication gasket; wherein the lower portion of the pressure sensing diaphragm is a cavity E, a cavity F is arranged between the cap and the pressure sensing diaphragm, the cavity E is communicated with the cavity C through a hole channel, and the cavity F is communicated with the cavity D through a hole channel.

    本发明公开了一种用于飞机氧气系统的流量显示控制装置,包括壳体,壳体的下端设有B腔、D腔两个腔体,分别与进气管路、出气管路连接;D腔的上端设置有C腔,B腔与D腔通过C腔连通;D腔上端与C腔连通的部位安装有限流器;B腔上方的壳体上有一个安装腔体,安装腔体上装配有帽盖,帽盖下方设置有感压膜片、压环以及指示垫片,其中:感压膜片设置在安装腔体的底部,内部受压时会向上膨胀;感压膜片的圆周通过压环进行固定密封;指示垫片安装在压环上方,指示垫片为橡胶材质的圆形结构,在指示垫片上开设有十字形槽口;其中,感压膜片下部为E腔,帽盖与感压膜片之间为F腔,E腔通过孔道与C腔连通,F腔通过孔道与D腔连通。


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    Title :

    Flow display control device for aircraft oxygen system


    Additional title:

    一种用于飞机氧气系统的流量显示控制装置


    Contributors:
    WAN LI (author) / LIU WENBIAO (author) / HUI YONGQIANG (author) / SU CHENG (author) / ZHANG CHAO (author) / PENG GUANGMEI (author)

    Publication date :

    2023-12-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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