公开(公告)号：US20130341847A1

公开(公告)日：2013-12-26

申请号：US14011104

申请日：2013-08-27

Applicant: Airbus Operations GmbH

Inventor： Rolf Bense ,  Eugen Gorr ,  Tim Strohbach

IPC: B25B11/00

CPC classification number: B25B11/007 ,  B25B5/12 ,  B64F5/10

Abstract: A device for the temporary position fixing of adjacently arranged aircraft structures to be interconnected includes a support frame with at least one vacuum suction cup for temporary surface attachment and with clamping means for the position fixing of the aircraft structures to be interconnected. The support frame with the at least one vacuum suction cup in the region of a transverse gap is attached on the side of one aircraft structure. The support frame includes mechanical contact pressure means for the gap-bridging position fixing of the adjacent other aircraft structure. On the support frame there is a counter support to pressure elements of the contact pressure means.

Abstract translation: 用于临时定位要相互连接的相互排列的飞机结构的装置包括具有至少一个用于临时表面附接的真空吸盘的支撑框架和用于待连接的飞机结构的位置固定的夹紧装置。 在横向间隙的区域中具有至少一个真空吸盘的支撑框架附接在一个飞行器结构的一侧。 支撑框架包括用于相邻的其它飞行器结构的间隙桥接位置固定的机械接触压力装置。 在支撑框架上，对接触压力装置的压力元件有反向支撑。

公开(公告)号：US09364939B2

公开(公告)日：2016-06-14

申请号：US14011104

申请日：2013-08-27

Applicant: Airbus Operations GmbH

Inventor： Rolf Bense ,  Eugen Gorr ,  Tim Strohbach

IPC: B25B11/00 ,  B25B5/12 ,  B64F5/00

CPC classification number: B25B11/007 ,  B25B5/12 ,  B64F5/10

Abstract: A device for the temporary position fixing of adjacently arranged aircraft structures to be interconnected includes a support frame with at least one vacuum suction cup for temporary surface attachment and with clamping means for the position fixing of the aircraft structures to be interconnected. The support frame with the at least one vacuum suction cup in the region of a transverse gap is attached on the side of one aircraft structure. The support frame includes mechanical contact pressure means for the gap-bridging position fixing of the adjacent other aircraft structure. On the support frame there is a counter support to pressure elements of the contact pressure means.

Abstract translation: 用于临时定位要相互连接的相互排列的飞机结构的装置包括具有至少一个用于临时表面附接的真空吸盘的支撑框架和用于待连接的飞机结构的位置固定的夹紧装置。 在横向间隙的区域中具有至少一个真空吸盘的支撑框架附接在一个飞行器结构的一侧。 支撑框架包括用于相邻的其它飞行器结构的间隙桥接位置固定的机械接触压力装置。 在支撑框架上，对接触压力装置的压力元件有反向支撑。

公开(公告)号：US09897131B2

公开(公告)日：2018-02-20

申请号：US13826918

申请日：2013-03-14

Applicant: Airbus Operations GmbH

Inventor： Rolf Bense ,  Eugen Gorr ,  Joerg Jendrny ,  Tim Strohbach

IPC: F16B39/00 ,  F16B19/05 ,  F16B19/08 ,  B21J15/02 ,  B21J15/36 ,  F16B5/04 ,  B29C65/56 ,  B29C65/00

CPC classification number: F16B39/00 ,  B21J15/022 ,  B21J15/025 ,  B21J15/36 ,  B29C65/562 ,  B29C66/02242 ,  B29C66/1122 ,  B29C66/21 ,  B29C66/41 ,  B29C66/721 ,  B29C66/7212 ,  F16B5/04 ,  F16B19/05 ,  F16B19/086 ,  Y10T29/49948 ,  Y10T29/5377 ,  B29K2305/00 ,  B29K2301/00 ,  B29K2311/00

Abstract: A method for the connection of moulded parts, wherein a locking collar pin with locking grooves or with an external thread, is driven through the moulded parts and subsequently a locking collar is locked together with at least some of the locking grooves, or with threaded sections of the locking collar pin, by the application of radial pressure, or by means of a screwing operation. A connecting system with a locking ring pin, which has a punching section for purposes of punching through the moulded parts, and also locking grooves for purposes of active engagement with a locking ring; the latter extends over at least two adjacent locking grooves in the axial direction, or over at least two adjacent threads in the axial direction.

公开(公告)号：US20130239398A1

公开(公告)日：2013-09-19

申请号：US13826918

申请日：2013-03-14

Applicant: AIRBUS OPERATIONS GMBH

Inventor： Rolf Bense ,  Eugen Gorr ,  Joerg Jendrny ,  Tim Strohbach

IPC: F16B39/00

CPC classification number: F16B39/00 ,  B21J15/022 ,  B21J15/025 ,  B21J15/36 ,  B29C65/562 ,  B29C66/02242 ,  B29C66/1122 ,  B29C66/21 ,  B29C66/41 ,  B29C66/721 ,  B29C66/7212 ,  F16B5/04 ,  F16B19/05 ,  F16B19/086 ,  Y10T29/49948 ,  Y10T29/5377 ,  B29K2305/00 ,  B29K2301/00 ,  B29K2311/00

Abstract: A method for the connection of moulded parts, wherein a locking collar pin with locking grooves or with an external thread, is driven through the moulded parts and subsequently a locking collar is locked together with at least some of the locking grooves, or with threaded sections of the locking collar pin, by the application of radial pressure, or by means of a screwing operation. A connecting system with a locking ring pin, which has a punching section for purposes of punching through the moulded parts, and also locking grooves for purposes of active engagement with a locking ring; the latter extends over at least two adjacent locking grooves in the axial direction, or over at least two adjacent threads in the axial direction.

Abstract translation: 用于连接模制部件的方法，其中具有锁定槽或带有外螺纹的锁定环销被驱动通过模制部件，随后锁定套环与至少一些锁定槽锁定在一起，或者与螺纹部分 通过施加径向压力，或通过螺丝拧紧操作。 具有锁定环销的连接系统，其具有用于冲压穿过模制部件的冲压部分，以及用于与锁定环主动接合的锁定槽; 后者在轴向方向上延伸至少两个相邻的锁定槽，或在轴向方向上延伸至少两个相邻的螺纹。