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：US20190108765A1

公开(公告)日：2019-04-11

申请号：US16138399

申请日：2018-09-21

Applicant: Airbus Operations GmbH

Inventor： Rolf Bense ,  Daniel Lahidjanian ,  Misha Kappelhoff

IPC: G08G5/06 ,  B64F1/22 ,  G05D1/02 ,  B64D47/08

Abstract: A system for navigating an aircraft in a hangar, having at least one optical sensor firmly connected to the aircraft. The sensor can be used to continuously capture surroundings contour data relative to the aircraft. A data processing apparatus, connected to the sensor, has a data memory storing reference data and can be used to determine an aircraft actual position by continuously matching captured surroundings contour data with the reference data and to identify a position deviation by comparing the determined actual position with a stored target position. Also, a method for navigating an aircraft in a hangar with such a system.

公开(公告)号：US20160368012A1

公开(公告)日：2016-12-22

申请号：US15251272

申请日：2016-08-30

Applicant: Airbus Operations GmbH

Inventor： Dirk Bausen ,  Birgit Kuhlenschmidt ,  Karl Hausmann ,  Rolf Bense ,  Rebecca Siewert ,  Daniel Lahidjanian

IPC: B05B13/04 ,  B05D1/02 ,  B05B7/24 ,  B05B12/14 ,  B05B12/12

CPC classification number: B05B13/0431 ,  B05B1/14 ,  B05B7/2472 ,  B05B12/00 ,  B05B12/02 ,  B05B12/10 ,  B05B12/122 ,  B05B12/124 ,  B05B12/1409 ,  B05B12/1472 ,  B05B13/0452 ,  B05B13/0457 ,  B05B13/0468 ,  B05B13/0473 ,  B05C5/0208 ,  B05C5/0216 ,  B05D1/02 ,  B41J3/4073 ,  B41J25/308 ,  G05B2219/45013

Abstract: A device for painting a curved outer surface of an aircraft includes a paint applicator having a plurality of spray painting heads each assigned to one of a plurality of different base color supply units containing one of polyurethane aircraft paint and ink. The device further includes a spatially adjustable positioning device configured to move the paint applicator relative to the curved outer surface and at least one sensor device configured to determine a three-dimensional geometry of the curved outer surface. The device also includes a control unit configured to coordinate a movement of the positioning device with a paint output of the paint applicator, wherein the control unit is configured to alternately activate each of the plurality of spray painting heads so as to produce a picture motif so as to derive a two-dimensional driving geometry based on the three-dimensional geometry.

Abstract translation: 用于喷涂飞行器的弯曲外表面的装置包括涂料涂料器，其具有多个喷涂头，每个喷涂头分配给包含聚氨酯飞机涂料和油墨之一的多个不同基色供应单元中的一个。 该装置还包括空间可调的定位装置，其被配置成相对于弯曲的外表面移动涂料施加器，以及配置成确定弯曲的外表面的三维几何形状的至少一个传感器装置。 该装置还包括控制单元，该控制单元被配置为协调定位装置与涂料涂料的涂料输出的运动，其中控制单元被配置为交替地激活多个喷涂头中的每一个，以便产生图片图案 以便基于三维几何导出二维驱动几何。

公开(公告)号：US20130205576A1

公开(公告)日：2013-08-15

申请号：US13766095

申请日：2013-02-13

Applicant: Airbus Operations GmbH

Inventor： Rolf Bense ,  Eugen Gorr ,  Joerg Jendrny

IPC: F16B19/06

CPC classification number: F16B19/06 ,  B21J15/025 ,  Y10T29/49956

Abstract: A method for the joining of moulded components with a punching, stamping rivet, wherein a punched hole is radially widened in at least certain sections of the moulded components that are to be punched. A punching, stamping rivet is provided which has a deforming section that has a greater external diameter than a punching section.

Abstract translation: 一种用冲压铆钉铆接模制部件的方法，其中冲压孔在待冲压的模制部件的至少某些部分中径向加宽。 提供一种冲孔的冲压铆钉，其具有比冲压部分具有更大外径的变形部分。

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：US20190108763A1

公开(公告)日：2019-04-11

申请号：US16138377

申请日：2018-09-21

Applicant: Airbus Operations GmbH

Inventor： Rolf Bense ,  Daniel Lahidjanian ,  Misha Kappelhoff

IPC: G08G5/04 ,  G08G5/00 ,  G01S17/08 ,  G01S17/93

Abstract: A system for navigating an aircraft in a hangar, having at least one optical sensor firmly connected to the aircraft, wherein the sensor can be used to continuously capture surroundings contour data relative to the aircraft, and having a data processing apparatus, connected to the sensor, that has a data memory storing reference data, wherein the data processing apparatus can be used to detect an aircraft collision risk by continuously matching captured surroundings contour data with the reference data. Also, methods of navigating an aircraft in a hangar.

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：US20150356236A1

公开(公告)日：2015-12-10

申请号：US14729213

申请日：2015-06-03

Applicant: AIRBUS OPERATIONS GMBH

Inventor： Rolf Bense ,  Oliver Weiss

IPC: G06F17/50

CPC classification number: G06F17/5095 ,  B64C1/069 ,  B64F5/10 ,  G01B11/272 ,  G05B19/41805 ,  G05B2219/37048 ,  G06T7/73 ,  G06T2207/30164 ,  Y02P90/04

Abstract: An apparatus for aligning segments with one another include a positioning device and a projection device, installed on the construction site, projecting projection lines onto the segments from different directions so that distances between the projection lines and reference points applied to the segments can be determined. The position of the individual reference points on the segments can be determined with reference to a coordinate system by an evaluation device. Based on the spatial arrangement of the reference points, theoretical best-fit planes and best-fit lines are then generated for each segment. The segments are levelled by moving the positioning device or adjusting the shortest possible distance between the theoretical best-fit planes and best-fit lines to the projection lines and are aligned by again moving the positioning device so that the distances between the theoretical best-fit planes and best-fit lines of the first segment and of the second segment are minimised.

Abstract translation: 用于将片段彼此对准的装置包括安装在施工现场的定位装置和投影装置，从不同方向将投影线投影到片段上，使得可以确定投影线和参考点之间的距离。 可以参考评估装置的坐标系确定各个参考点在分段上的位置。 基于参考点的空间排列，然后为每个段生成理论最佳拟合平面和最佳拟合线。 通过移动定位装置或者将理论最佳拟合平面和最佳拟合线之间的最短可能距离调整到投影线，来对分段进行平整，并且通过再次移动定位装置使对准，使得理论最佳拟合 第一段和第二段的平面和最佳拟合线最小化。

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。