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公开(公告)号：US07438167B2
公开(公告)日：2008-10-21
申请号：US11499155
申请日：2006-08-04
IPC分类号： F16H48/22 , F16D25/0638
CPC分类号： F16H48/22 , F16H48/08 , F16H48/30 , F16H48/32 , F16H48/34 , F16H2048/204 , F16H2048/346 , F16H2048/382 , F16H2200/2071 , Y10T29/49464 , Y10T29/49465 , Y10T29/4984 , Y10T29/49947 , Y10T29/49948 , Y10T29/49963 , Y10T74/19642
摘要： A coupling device (11) and method of assembly, the device being of the type including a plenum member (17) disposed at one axial end of the coupling housing (13,15), the method comprising configuring the plenum member (17) such that each of the required features (55,57,61,66) is disposed circumferentially between an adjacent pair of fastener holes (18H). Next, the input ring gear (R) is installed about the housing (13,15) of the coupling device (11), from an axial end opposite said plenum member (17), into assembly position adjacent said flange portion (18). Each of a plurality (N) of fasteners (89) is inserted through one of the fastener holes (18H) and into initial threaded engagement with the input ring gear (R). Finally, by means of a fastener driver, all of the plurality (N) of fasteners (89) are driven into full threaded engagement, substantially simultaneously, with the input ring gear (R).
摘要翻译： 一种联接装置（11）和组装方法，该装置的类型包括设置在联接壳体（13,15）的一个轴向端部处的增压构件（17），该方法包括将增压构件（17） 每个所需特征（55,57,61,66）周向设置在相邻的一对紧固件孔（18H）之间。 接下来，输入齿圈（R）围绕联接装置（11）的壳体（13,15）从与气室构件（17）相对的轴向端部安装到邻近所述凸缘部分（18）的组装位置。 多个（N）个紧固件（89）中的每一个通过其中一个紧固件孔（18H）插入并与输入齿圈（R）初始螺纹接合。 最后，通过紧固件驱动器，所有多个（N）个紧固件（89）被驱动成与输入齿圈（R）基本同时地完全螺纹接合。
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公开(公告)号：US20050252746A1
公开(公告)日：2005-11-17
申请号：US10846444
申请日：2004-05-14
CPC分类号： F16H48/22 , F16H48/08 , F16H48/30 , F16H48/32 , F16H48/34 , F16H2048/204 , F16H2048/346 , F16H2048/382 , F16H2200/2071 , Y10T29/49464 , Y10T29/49465 , Y10T29/4984 , Y10T29/49947 , Y10T29/49948 , Y10T29/49963 , Y10T74/19642
摘要： A coupling device (11) and method of assembly, the device being of the type including a plenum member (17) disposed at one axial end of the coupling housing (13,15), the method comprising configuring the plenum member (17) such that each of the required features (55,57,61,66) is disposed circumferentially between an adjacent pair of fastener holes (18H). Next, the input ring gear (R) is installed about the housing (13,15) of the coupling device (11), from an axial end opposite said plenum member (17), into assembly position adjacent said flange portion (18). Each of a plurality (N) of fasteners (89) is inserted through one of the fastener holes (18H) and into initial threaded engagement with the input ring gear (R). Finally, by means of a fastener driver, all of the plurality (N) of fasteners (89) are driven into full threaded engagement, substantially simultaneously, with the input ring gear (R).
摘要翻译： 一种联接装置（11）和组装方法，该装置的类型包括设置在联接壳体（13,15）的一个轴向端部处的增压构件（17），该方法包括将增压构件（17） 每个所需特征（55,57,61,66）周向设置在相邻的一对紧固件孔（18H）之间。 接下来，输入齿圈（R）围绕联接装置（11）的壳体（13,15）从与气室构件（17）相对的轴向端部安装到邻近所述凸缘部分（18）的组装位置。 多个（N）个紧固件（89）中的每一个通过其中一个紧固件孔（18H）插入并与输入齿圈（R）初始螺纹接合。 最后，通过紧固件驱动器，所有多个（N）个紧固件（89）被驱动成与输入齿圈（R）基本同时地完全螺纹接合。
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公开(公告)号：US20060266145A1
公开(公告)日：2006-11-30
申请号：US11499155
申请日：2006-08-04
IPC分类号： F16H57/02
CPC分类号： F16H48/22 , F16H48/08 , F16H48/30 , F16H48/32 , F16H48/34 , F16H2048/204 , F16H2048/346 , F16H2048/382 , F16H2200/2071 , Y10T29/49464 , Y10T29/49465 , Y10T29/4984 , Y10T29/49947 , Y10T29/49948 , Y10T29/49963 , Y10T74/19642
摘要： A coupling device (11) and method of assembly, the device being of the type including a plenum member (17) disposed at one axial end of the coupling housing (13,15), the method comprising configuring the plenum member (17) such that each of the required features (55,57,61,66) is disposed circumferentially between an adjacent pair of fastener holes (18H). Next, the input ring gear (R) is installed about the housing (13,15) of the coupling device (11), from an axial end opposite said plenum member (17), into assembly position adjacent said flange portion (18). Each of a plurality (N) of fasteners (89) is inserted through one of the fastener holes (18H) and into initial threaded engagement with the input ring gear (R). Finally, by means of a fastener driver, all of the plurality (N) of fasteners (89) are driven into full threaded engagement, substantially simultaneously, with the input ring gear (R).
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公开(公告)号：US07131201B2
公开(公告)日：2006-11-07
申请号：US10846444
申请日：2004-05-14
CPC分类号： F16H48/22 , F16H48/08 , F16H48/30 , F16H48/32 , F16H48/34 , F16H2048/204 , F16H2048/346 , F16H2048/382 , F16H2200/2071 , Y10T29/49464 , Y10T29/49465 , Y10T29/4984 , Y10T29/49947 , Y10T29/49948 , Y10T29/49963 , Y10T74/19642
摘要： A coupling device (11) and method of assembly, the device being of the type including a plenum member (17) disposed at one axial end of the coupling housing (13,15), the method comprising configuring the plenum member (17) such that each of the required features (55,57,61,66) is disposed circumferentially between an adjacent pair of fastener holes (18H). Next, the input ring gear (R) is installed about the housing (13,15) of the coupling device (11), from an axial end opposite said plenum member (17), into assembly position adjacent said flange portion (18). Each of a plurality (N) of fasteners (89) is inserted through one of the fastener holes (18H) and into initial threaded engagement with the input ring gear (R). Finally, by means of a fastener driver, all of the plurality (N) of fasteners (89) are driven into full threaded engagement, substantially simultaneously, with the input ring gear (R).
摘要翻译： 一种联接装置（11）和组装方法，该装置的类型包括设置在联接壳体（13,15）的一个轴向端部处的增压构件（17），该方法包括将增压构件（17） 每个所需特征（55,57,61,66）周向设置在相邻的一对紧固件孔（18H）之间。 接下来，输入齿圈（R）围绕联接装置（11）的壳体（13,15）从与气室构件（17）相对的轴向端部安装到邻近所述凸缘部分（18）的组装位置。 多个（N）个紧固件（89）中的每一个通过其中一个紧固件孔（18H）插入并与输入齿圈（R）初始螺纹接合。 最后，通过紧固件驱动器，所有多个（N）个紧固件（89）被驱动成与输入齿圈（R）基本同时地完全螺纹接合。
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