The invention belongs to the technical field of aerostat manufacturing, and discloses an airship empennage and airbag assembly position determination method, which comprises the following steps: step 1, preparing a test environment; 2, measuring the actual size of the finished empennage root rib; 3, measuring the theoretical size of the empennage root rib; 4, according to the actual size and the theoretical size of the finished empennage root rib, the scaling of the empennage root rib is determined, and a scaled actual root rib cutting picture is drawn according to the scaling; 5, cutting the scaled root rib template according to an actual root rib cutting picture; and 6, the installation position of the tail wing root rib is determined on the air bag cutting piece through the root rib template, and the tail wing root rib is assembled.

    本发明属于浮空器制造技术领域,公开了一种飞艇尾翼与气囊装配位置确定方法,包括以下步骤:步骤一:准备试验环境;步骤二:对尾翼根肋的成品实际尺寸进行测量;步骤三:对尾翼根肋的理论尺寸进行测量;步骤四:根据尾翼根肋的成品实际尺寸和理论尺寸确定尾翼根肋的缩放比例,并根据缩放比例绘制缩放后的实际根肋裁片图;步骤五:根据实际根肋裁片图,裁剪缩放后的根肋模板;步骤六:利用根肋模板在气囊裁片上确定尾翼根肋的安装位置并装配尾翼根肋。


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    Titel :

    Method for determining assembly positions of airship empennage and air bag


    Weitere Titelangaben:

    一种飞艇尾翼与气囊装配位置确定方法


    Beteiligte:
    YAO HAO (Autor:in) / LIU PINGPING (Autor:in) / WANG XIANDA (Autor:in) / YANG TONGMIN (Autor:in) / GONG MINGYANG (Autor:in)

    Erscheinungsdatum :

    2024-03-26


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    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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