The invention discloses a hoop for an airborne flare aircraft spreading device. The hoop comprises a fixing piece and adopts an integral design, wherein the lower end in the fixing piece protrudes toform a lower hoop body, the upper end in the fixing piece is fixed to an upper hoop body by means of a connecting piece to realize fixation, the upper hoop body is matched with a bolt and the fixing piece to lock the spreading device, stable lifting of the spreading device is achieved, and wrapping is achieved by means of the upper hoop body at the top part; auxiliary mechanisms are installed at the upper ends of the left side and the right side in the upper hoop body, protective pads arranged in the auxiliary mechanisms are positioned at four ends of the inner surfaces of the upper hoop bodyand the lower hoop body, and the two sets at the upper end can be adjusted by means of an adjusting mechanism to press the fixed spreading device, so that the fixed spreading device cannot loosen; andsealing and lubricating mechanisms are arranged at connecting positions between the upper hoop body and the fixing piece and can be compressed along with the downward screwing of the locking bolts, oil absorption cotton installed in the sealing and lubricating mechanisms can absorb lubricating oil, and the penetrating bolts are continuously lubricated, thereby reducing oxidation of the bolts.

    本发明公开了一种机载焰条飞机播撒装置用卡箍,包括固定件,本发明通过采用一体设计,在固定件内下端凸出为下卡箍,固定件内上端通过连接件与上卡箍实现固定,上卡箍配合螺栓与固定件即可对播撒装置进行锁紧,实现了对播撒装置的稳定托举,并且由顶部的上卡箍实现包裹;在上卡箍内左右两侧上端安装有辅助机构,辅助机构内设置有的防护垫于上下卡箍内表面四端,并且上端两组能通过调节机构实现调节,来对固定后的播撒装置进行压紧,使其不会发生松动;在上卡箍与固定件之间的连接位置设置有密封润滑机构,密封润滑机构能随着锁紧螺栓的旋下进行压缩,内部安装的吸油棉能对润滑油进行吸附,持续的对贯穿的螺栓进行持续润滑,减少螺栓的氧化。


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Hoop for airborne flare aircraft spreading device


    Weitere Titelangaben:

    一种机载焰条飞机播撒装置用卡箍


    Beteiligte:
    ZOU CHUNGEN (Autor:in) / WANG PU (Autor:in) / ZHU KEPING (Autor:in) / ZENG RUNPING (Autor:in) / GONG YI (Autor:in) / GU CHUNTAO (Autor:in) / HUANG HUAN (Autor:in) / SHAO WENZHENG (Autor:in) / ZHANG LIANGLIANG (Autor:in) / CHANG JIANG (Autor:in)

    Erscheinungsdatum :

    2020-04-21


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    F16M Rahmen, Gehäuse oder Grundplatten von Kraftmaschinen oder anderen Maschinen oder von Apparaten, nicht auf eine besondere Art von Maschine oder Apparat eingeschränkt, die anderweitig vorgesehen ist , FRAMES, CASINGS, OR BEDS, OF ENGINES OR OTHER MACHINES OR APPARATUS, NOT SPECIFIC TO AN ENGINE, MACHINE, OR APPARATUS PROVIDED FOR ELSEWHERE / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F16B DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES , Vorrichtungen zum Befestigen oder Sichern von Konstruktionselementen oder Maschinenteilen, z.B. Nägel, Bolzen, Schrauben, Sprengringe, Klemmen, Klammern oder Keile / F16F SPRINGS , Federn / F16N LUBRICATING , Schmierung



    HOOP LOAD BEARING AIRCRAFT TRANSPARENCY

    DEGANIS LUIS E / DI SONG / STEWART SHERMAN D | Europäisches Patentamt | 2016

    Freier Zugriff

    Hoop load bearing aircraft transparency

    DEGANIS LUIS E / SONG DI / STEWART SHERMAN D | Europäisches Patentamt | 2016

    Freier Zugriff

    HOOP LOAD BEARING AIRCRAFT TRANSPARENCY

    Europäisches Patentamt | 2016

    Freier Zugriff

    Hoop

    YONG LIANG STEVE TAN | Europäisches Patentamt | 2021

    Freier Zugriff

    AIRCRAFT LANDING FLARE

    Eduard Kovalevskiy / Valeriy Konin / Tetiana Olevinska | DOAJ | 2014

    Freier Zugriff