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公开(公告)号：US5419034A
公开(公告)日：1995-05-30
申请号：US166835
申请日：1993-12-15
申请人： Kazuya Kigawa , Kenji Furukawa , Tetsu Deguchi , Sachiharu Inoue , Norikatsu Endo , Tatsuo Yanagisawa , Shinji Ikegami , Yasuyuki Omagari , Koji Kihara , Tachiki Sugawara , Kenzo Shimizu
发明人： Kazuya Kigawa , Kenji Furukawa , Tetsu Deguchi , Sachiharu Inoue , Norikatsu Endo , Tatsuo Yanagisawa , Shinji Ikegami , Yasuyuki Omagari , Koji Kihara , Tachiki Sugawara , Kenzo Shimizu
CPC分类号： F16F9/3271 , Y10T29/49719 , Y10T29/49721 , Y10T29/4973 , Y10T29/49821 , Y10T29/53087 , Y10T29/53657
摘要： To safely and quickly exchange a seal of a shock strut of a selected shock absorbing apparatus of an airplane, an apparatus is provided whereby the main body of the airplane is lifted by pressurizing and extending at least one other shock absorbing apparatus in order to extend the selected shock absorbing apparatus and expose the seal thereof. A shock strut of the selected shock absorbing apparatus is then lifted away from the associated wheels so that a new seal may be inserted from below the strut.
摘要翻译： 为了安全且快速地更换飞机所选择的减震装置的冲击支柱的密封件，提供了一种装置，通过对至少一个其它减震装置进行加压和延伸来提升飞机的主体，以便延长 选择的冲击吸收装置并暴露其密封。 然后将所选择的减震装置的冲击支柱从相关联的轮子提升离开，使得可以从支柱的下方插入新的密封件。
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公开(公告)号：US5323522A
公开(公告)日：1994-06-28
申请号：US948321
申请日：1992-09-22
申请人： Kazuya Kigawa , Kenji Furukawa , Tetsu Deguchi , Sachiharu Inoue , Norikatsu Endo , Tatsuo Yanagisawa , Shinji Ikegami , Yasuyuki Omagari , Koji Kihara , Tachiki Sugawara , Kenzo Shimizu
发明人： Kazuya Kigawa , Kenji Furukawa , Tetsu Deguchi , Sachiharu Inoue , Norikatsu Endo , Tatsuo Yanagisawa , Shinji Ikegami , Yasuyuki Omagari , Koji Kihara , Tachiki Sugawara , Kenzo Shimizu
CPC分类号： F16F9/3271 , Y10T29/49719 , Y10T29/49721 , Y10T29/4973 , Y10T29/49821 , Y10T29/53087 , Y10T29/53657
摘要： To safety and quickly exchange a seal of a shock strut of a selected shock absorbing apparatus of an airplane, the main body of the airplane is lifted by pressurizing and extending at least one other shock absorbing apparatus in order to extend the selected shock absorbing apparatus and expose the seal thereof. A shock strut of the selected shock absorbing apparatus is then lifted away from the associated wheels so that a new seal may be inserted from below the strut.
摘要翻译： 为了安全并快速地更换飞机所选择的减震装置的冲击支柱的密封，飞机的主体通过对至少一个其它减震装置进行加压和延伸来提升，以便延伸所选择的冲击吸收装置和 暴露其密封。 然后将所选择的减震装置的冲击支柱从相关联的轮子提升离开，使得可以从支柱的下方插入新的密封件。
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公开(公告)号：US5499796A
公开(公告)日：1996-03-19
申请号：US407658
申请日：1995-03-21
申请人： Kazuya Kigawa , Kenji Furukawa , Tetsu Deguchi , Sachiharu Inoue , Norikatsu Endo , Tatsuo Yanagisawa , Shinji Ikegami , Yasuyuki Omagari , Koji Kihara , Tachiki Sugawara , Kenzo Shimizu
发明人： Kazuya Kigawa , Kenji Furukawa , Tetsu Deguchi , Sachiharu Inoue , Norikatsu Endo , Tatsuo Yanagisawa , Shinji Ikegami , Yasuyuki Omagari , Koji Kihara , Tachiki Sugawara , Kenzo Shimizu
CPC分类号： F16F9/3271 , Y10T29/49719 , Y10T29/49721 , Y10T29/4973 , Y10T29/49821 , Y10T29/53087 , Y10T29/53657
摘要： To safely and quickly exchange a seal of a shock strut of a selected shock absorbing apparatus of an airplane, an apparatus is provided whereby the main body of the airplane is lifted by pressurizing and extending at least one other shock absorbing apparatus in order to extend the selected shock absorbing apparatus and expose the seal thereof. A shock strut of the selected shock absorbing apparatus is then lifted away from the associated wheels so that a new seal may be inserted from below the strut. To lift the strut, an apparatus is provided which includes a main body portion having an inclined surface substantially complementary to a downward-facing inclined surface of the strut, and a cylindrical portion which inserts into an attachment hole of the strut.
摘要翻译： 为了安全且快速地更换飞机所选择的减震装置的冲击支柱的密封件，提供了一种装置，通过对至少一个其它减震装置进行加压和延伸来提升飞机的主体，以便延长 选择的冲击吸收装置并暴露其密封。 然后将所选择的减震装置的冲击支柱从相关联的轮子提升离开，使得可以从支柱的下方插入新的密封件。 为了提升支柱，提供了一种装置，其包括具有与支柱的向下倾斜表面大致互补的倾斜表面的主体部分和插入支柱的附接孔中的圆柱形部分。
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