The invention relates to the technical field, in particular to an aircraft engine compartment operation protection device which comprises a frame strip frame, two rectangular frames are hinged to the two ends of the frame strip frame through first transverse shafts, lifting assemblies are installed at the ends, close to the frame strip frame, of the two rectangular frames, and adjusting assemblies are installed at the ends, close to anti-skid plates, of the two rectangular frames. The whole device is easy and convenient to use and can meet various different operation requirements, meanwhile, the independent pedal is arranged, the operation environment of operators is effectively improved, meanwhile, multiple anti-skid modes are used, multiple protection is conducted on the operators, personal safety is guaranteed, and safety accidents are avoided.

    本发明涉及技术领域,尤其是一种飞机发动机舱作业防护装置,包括框条架,框条架的两端通过第一横轴铰接有两个矩形框,两个矩形框靠近框条架一端安装有升降组件,两个矩形框靠近防滑板一端安装有调节组件。本装置整体使用简单方便,可适应多种不同作业需要,同时设立单独踏板,对操作人员作业环境进行有效提升,同时使用多种防滑方式,对操作人员进行多重防护,保障人身安全,避免安全事故。


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    Title :

    Aircraft engine compartment operation protection device


    Additional title:

    一种飞机发动机舱作业防护装置


    Contributors:
    SHENG MINGHU (author) / YANG LIU (author) / LI ZHIJUN (author) / WANG CHAO (author)

    Publication date :

    2023-11-14


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    E06C LADDERS , Leitern / 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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