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1. 发明授权

US08740150B2 Connection of a wing to a fuselage of an airplane 失效
标题翻译：将机翼连接到飞机机身上
公开(公告)号：US08740150B2
公开(公告)日：2014-06-03
申请号：US13058552
申请日：2009-08-18
申请人： Frank Werth , Andreas Poppe , Hermann Benthien , Bernd Beschorner
发明人： Frank Werth , Andreas Poppe , Hermann Benthien , Bernd Beschorner
IPC分类号： B64C1/26
CPC分类号： B64C1/26
摘要： An aerofoil connection on a fuselage airframe comprising a plurality of double-jointed coupling members. In each case at least two z-coupling members extending substantially parallel to a vertical axis of the aircraft and in each case at least two xz-coupling members are arranged in the region of two longitudinal edges of a fuselage airframe recess wherein the xz-coupling members are configured in each case for a first maximum of a load in the event of a crash and of a load in normal flight operation parallel to a longitudinal axis of the aircraft, and for a second maximum of a load in the event of a crash and of a load in normal flight operation parallel to the vertical axis. The xz-coupling members are capable of absorbing force components parallel to the x-axis as well as force components which arise parallel to the z-axis.
摘要翻译：在机身机身上的机翼连接，包括多个双接头联接构件。在每种情况下，至少两个基本上平行于飞行器的垂直轴延伸的z联接构件，并且在每种情况下至少两个xz耦合构件布置在机身机身凹部的两个纵向边缘的区域中，其中xz耦合在每种情况下，构件在发生碰撞的情况下的负载的第一最大值和平行于飞行器的纵向轴线的正常飞行操作中的负载被配置，并且在发生碰撞的情况下被配置为负载的第二最大值以及平行于垂直轴的正常飞行操作中的负载。 xz耦合构件能够吸收平行于x轴的力分量以及平行于z轴产生的力分量。

2. 发明申请

US20100040433A1 CONNECTING ELEMENT, IN PARTICULAR A SPEED NUT 有权
标题翻译：连接元件，特别是速度螺母
公开(公告)号：US20100040433A1
公开(公告)日：2010-02-18
申请号：US12539191
申请日：2009-08-11
申请人： Andreas Poppe , Hermann Benthien
发明人： Andreas Poppe , Hermann Benthien
IPC分类号： F16B37/08 , F16B37/00
CPC分类号： F16B37/067 , F16B19/1045
摘要： The invention relates to a connection element, in particular a plate nut, comprising a base body for attachment of an arbitrary component to a metallic planar object, in particular to a sheet metal.According to the invention, the base body comprises a securement portion the cross-sectional geometry of which deviates from a circular shape, the securement portion being at least partially positively receivable in a deformation in the sheet metal. The base body is, by means of a holding device, secured in the deformation against dropping out.In an alternative embodiment of the connection element, wherein unilateral accessibility to the sheet metal is sufficient, the holding device is formed by bead portions in a shaft area of the base body, which are plastically deformed into a bead by pull-out of a threaded bolt that is screwed into a thread portion.In accordance with a further embodiment the holding device is formed by a threaded nut engageable on the underside with the base body of the connection element or/and snappable onto the same, bilateral accessibility to the sheet metal however being required.
摘要翻译：本发明涉及连接元件，特别是板螺母，其包括用于将任意部件附接到金属平面物体，特别是金属板的基体。根据本发明，基体包括其横截面几何形状偏离圆形的固定部分，该固定部分至少部分地可在金属板的变形中正面接收。基体通过保持装置固定在变形中，不会脱落。在连接元件的替代实施例中，其中对金属板的单方面可接近性足够，保持装置由基体的轴区域中的胎圈部分形成，其通过拉出螺纹而被塑性变形成胎圈拧入螺纹部分的螺栓。根据进一步的实施例，保持装置由能够与连接元件的基体接合在下侧上的螺纹螺母形成，或/或可被卷绕到与金属板相同的双边可接近性上。

3. 发明申请

US20130327882A1 Connection arrangement, aircraft or spacecraft, method for dropping load and method for landing 有权
标题翻译：连接布置，飞机或航天器，降落荷载方法和着陆方法
公开(公告)号：US20130327882A1
公开(公告)日：2013-12-12
申请号：US13885597
申请日：2011-11-16
申请人： Hermann Benthien , Andreas Poppe
发明人： Hermann Benthien , Andreas Poppe
IPC分类号： B64C3/38
CPC分类号： B64C3/385 , B64C1/26 , B64D1/08
摘要： A connection arrangement having: a fuselage portion; a wing portion which is mounted on the fuselage portion in an upper region thereof; a first Z-coupling element which couples the wing portion to the fuselage portion in the vertical direction thereof; and two XZ-coupling elements which couple the wing portion to the fuselage portion in the vertical direction and longitudinal direction thereof; the first Z-coupling element being longitudinally adjustable in the vertical direction in order to thus adjust an angle of attack of the wing portion.
摘要翻译：一种连接装置，具有：机身部分; 翼部，其安装在机身部分的上部区域中; 第一Z联接元件，其将翼部沿垂直方向连接到机身部; 以及两个XZ耦合元件，其将翼部在垂直方向和纵向方向上耦合到机身部分; 第一Z联接元件在垂直方向上纵向可调，以便调整翼部的迎角。

4. 发明授权

US08262332B2 Connecting element, in particular a speed nut 有权
标题翻译：连接元件，特别是速度螺母
公开(公告)号：US08262332B2
公开(公告)日：2012-09-11
申请号：US12539191
申请日：2009-08-11
申请人： Andreas Poppe , Hermann Benthien
发明人： Andreas Poppe , Hermann Benthien
IPC分类号： F16B37/04
CPC分类号： F16B37/067 , F16B19/1045
摘要： The invention relates to a connection element, in particular a plate nut, comprising a base body for attachment of an arbitrary component to a metallic planar object, in particular to a sheet metal.According to the invention, the base body comprises a securement portion the cross-sectional geometry of which deviates from a circular shape, the securement portion being at least partially positively receivable in a deformation in the sheet metal. The base body is, by means of a holding device, secured in the deformation against dropping out.In an alternative embodiment of the connection element, wherein unilateral accessibility to the sheet metal is sufficient, the holding device is formed by bead portions in a shaft area of the base body, which are plastically deformed into a bead by pull-out of a threaded bolt that is screwed into a thread portion.In accordance with a further embodiment the holding device is formed by a threaded nut engageable on the underside with the base body of the connection element or/and snappable onto the same, bilateral accessibility to the sheet metal however being required.
摘要翻译：本发明涉及连接元件，特别是板螺母，其包括用于将任意部件附接到金属平面物体，特别是金属板的基体。根据本发明，基体包括其横截面几何形状偏离圆形的固定部分，该固定部分至少部分地可在金属板的变形中正面接收。基体通过保持装置固定在变形中，不会脱落。在连接元件的替代实施例中，其中对金属片的单方面可接近性是足够的，保持装置由基体的轴区域中的胎圈部分形成，其通过拉出螺纹而被塑性变形成胎圈拧入螺纹部分的螺栓。根据进一步的实施例，保持装置由能够与连接元件的基体接合在下侧上的螺纹螺母形成，或/或可被卷绕到与金属板相同的双边可接近性上。

5. 发明申请

US20100294884A1 ATTACHMENT ARRANGEMENT FOR A CARGO COMPARTMENT FLOOR OF AN AIRCRAFT AND AIRCRAFT WITH AN ATTACHMENT ARRANGEMENT OF THIS TYPE 有权
标题翻译：飞机上的货物装卸地点的附件安排和这种类型的附件安排的飞机
公开(公告)号：US20100294884A1
公开(公告)日：2010-11-25
申请号：US12777745
申请日：2010-05-11
申请人： Hermann Benthien , Andreas Poppe
发明人： Hermann Benthien , Andreas Poppe
IPC分类号： B64C1/18
CPC分类号： B64D9/003 , Y02T50/46
摘要： The present invention provides an aircraft floor of an aircraft consisting of a number of base plates and a number of longitudinal supports and provides an aircraft with a floor of this type. The aircraft floor has transverse joints for partitioning the floor into a plurality of segments transversely to a longitudinal axis of the aircraft, the respective segment consisting of a number of longitudinal support elements, partitioned by the transverse joints, of the longitudinal supports and of a number of base plate elements partitioned by the transverse joints, of the base plates and the segments being coupled together such that they have exclusively a translatory degree of freedom with respect to one another in the direction of the longitudinal axis of the aircraft.
摘要翻译：本发明提供一种由多个基板和多个纵向支撑件组成的飞机的飞机地板，并为飞机提供了这种类型的地板。飞机地板具有横向接头，用于将地板分成与飞行器的纵向轴线横向的多个段，相应的段由多个纵向支撑元件组成，由横向接头分隔开，纵向支撑件和数字通过横向接头分隔的基板元件，基板和节段联接在一起，使得它们在飞行器的纵向轴线方向上相对于彼此具有独立的平移自由度。

6. 发明授权

US09248902B2 Connection arrangement, aircraft or spacecraft, method for dropping load and method for landing 有权
公开(公告)号：US09248902B2
公开(公告)日：2016-02-02
申请号：US13885597
申请日：2011-11-16
申请人： Hermann Benthien , Andreas Poppe
发明人： Hermann Benthien , Andreas Poppe
IPC分类号： B64C3/38 , B64C1/26 , B64D1/08
CPC分类号： B64C3/385 , B64C1/26 , B64D1/08
摘要： A connection arrangement having: a fuselage portion; a wing portion which is mounted on the fuselage portion in an upper region thereof; a first Z-coupling element which couples the wing portion to the fuselage portion in the vertical direction thereof; and two XZ-coupling elements which couple the wing portion to the fuselage portion in the vertical direction and longitudinal direction thereof; the first Z-coupling element being longitudinally adjustable in the vertical direction in order to thus adjust an angle of attack of the wing portion.

7. 发明授权

US08424803B2 Attachment arrangement for a cargo compartment floor of an aircraft and aircraft with an attachment arrangement of this type 有权
标题翻译：具有这种附件装置的飞机和飞机的货舱地板的附件安排
公开(公告)号：US08424803B2
公开(公告)日：2013-04-23
申请号：US12777745
申请日：2010-05-11
申请人： Hermann Benthien , Andreas Poppe
发明人： Hermann Benthien , Andreas Poppe
IPC分类号： B64C1/18 , B64C1/20
CPC分类号： B64D9/003 , Y02T50/46
摘要： The present invention provides an aircraft floor of an aircraft consisting of a number of base plates and a number of longitudinal supports and provides an aircraft with a floor of this type. The aircraft floor has transverse joints for partitioning the floor into a plurality of segments transversely to a longitudinal axis of the aircraft, the respective segment consisting of a number of longitudinal support elements, partitioned by the transverse joints, of the longitudinal supports and of a number of base plate elements partitioned by the transverse joints, of the base plates and the segments being coupled together such that they have exclusively a translatory degree of freedom with respect to one another in the direction of the longitudinal axis of the aircraft.
摘要翻译：本发明提供一种由多个基板和多个纵向支撑件组成的飞机的飞机地板，并为飞机提供了这种类型的地板。飞机地板具有横向接头，用于将地板分成与飞行器的纵向轴线横向的多个段，相应的段由多个纵向支撑元件组成，由横向接头分隔开，纵向支撑件和数字通过横向接头分隔的基板元件，基板和节段联接在一起，使得它们在飞行器的纵向轴线方向上相对于彼此具有独立的平移自由度。

8. 发明申请

US20110210206A1 CONNECTION OF A WING TO A FUSELAGE OF AN AIRPLANE 失效
标题翻译：一个机会与一个机场的联系的连接
公开(公告)号：US20110210206A1
公开(公告)日：2011-09-01
申请号：US13058552
申请日：2009-08-18
申请人： Frank Werth , Andreas Poppe , Hermann Benthien , Bernd Beschorner
发明人： Frank Werth , Andreas Poppe , Hermann Benthien , Bernd Beschorner
IPC分类号： B64C1/26
CPC分类号： B64C1/26
摘要： An aerofoil connection on a fuselage airframe comprising a plurality of double-jointed coupling members. In each case at least two z-coupling members extending substantially parallel to a vertical axis of the aircraft and in each case at least two xz-coupling members are arranged in the region of two longitudinal edges of a fuselage airframe recess wherein the xz-coupling members are configured in each case for a first maximum of a load in the event of a crash and of a load in normal flight operation parallel to a longitudinal axis of the aircraft, and for a second maximum of a load in the event of a crash and of a load in normal flight operation parallel to the vertical axis. The xz-coupling members are capable of absorbing force components parallel to the x-axis as well as force components which arise parallel to the z-axis.
摘要翻译：在机身机身上的机翼连接，包括多个双接头联接构件。在每种情况下，至少两个基本上平行于飞行器的垂直轴延伸的z联接构件，并且在每种情况下至少两个xz耦合构件布置在机身机身凹部的两个纵向边缘的区域中，其中xz耦合在每种情况下，构件在发生碰撞的情况下的负载的第一最大值和平行于飞行器的纵向轴线的正常飞行操作中的负载被配置，并且在发生碰撞的情况下被配置为负载的第二最大值以及平行于垂直轴的正常飞行操作中的负载。 xz耦合构件能够吸收平行于x轴的力分量以及平行于z轴产生的力分量。

9. 发明申请

US20140023789A1 COATING AGENTS HAVING HIGH SCRATCH RESISTANCE AND WEATHERING STABILITY 审中-公开
标题翻译：具有高耐蚀性和耐候性的涂料代理
公开(公告)号：US20140023789A1
公开(公告)日：2014-01-23
申请号：US14036367
申请日：2013-09-25
申请人： Matthijs Groenewolt , Andreas Poppe , Gunter Klein , Manuela Niemeier , Elke Westhoff , Wilfried Stubbe , Simone Hesener
发明人： Matthijs Groenewolt , Andreas Poppe , Gunter Klein , Manuela Niemeier , Elke Westhoff , Wilfried Stubbe , Simone Hesener
IPC分类号： C09D175/14
CPC分类号： C09D175/14 , C08G18/289 , C08G18/6254 , C08G18/778 , C08G18/809 , C09D175/04
摘要： Disclosed are coating compositions comprising (a) at least one hydroxyl-containing compound (A), (b) at least one compound (B) having isocyanate groups, and (c) at least one catalyst (D) for the crosslinking of silane groups, said catalyst (D) comprising phosphorus. It is an aspect of the disclosed coating compositions that (i) one or more constituents of the coating composition contain hydrolyzable silane groups and (ii) the coating composition can be finally cured to a coating which has statistically distributed regions of an Si—O—Si network.
摘要翻译：公开了包含（a）至少一种含羟基化合物（A），（b）至少一种具有异氰酸酯基团的化合物（B）和（c）至少一种用于硅烷基团交联的催化剂（D），所述催化剂（D）包含磷。所公开的涂料组合物的一个方面是（i）涂料组合物中的一种或多种组分含有可水解的硅烷基团，和（ii）涂料组合物可以最终固化成具有统计分布的Si-O- Si网络。

10. 发明申请

US20120189858A1 COATING COMPOSITIONS AND RESULTANT COATINGS WITH HIGH SCRATCH RESISTANCE AND STABILITY TO SOLVENT POPPING 有权
标题翻译：涂层组合物和具有高耐蚀性和稳定性的溶解性涂料的涂料
公开(公告)号：US20120189858A1
公开(公告)日：2012-07-26
申请号：US13376330
申请日：2010-03-08
申请人： Andreas Poppe , Joachim Woltering , Beate Gebauer , Alfred König , Simone Jurczik
发明人： Andreas Poppe , Joachim Woltering , Beate Gebauer , Alfred König , Simone Jurczik
IPC分类号： B32B9/04 , B05D3/02 , C09D133/14 , B05D1/36
CPC分类号： C08G18/678 , C08G18/161 , C08G18/1866 , C08G18/2045 , C08G18/2063 , C08K5/29 , C08K5/3465 , C09D175/04 , Y10T428/31551 , Y10T428/31663 , C08L2666/16
摘要： The invention provides coating compositions comprising at least one compound (A) containing hydroxyl groups, at least one compound (B) containing isocyanate groups, at least 5.0% by weight, based on the nonvolatile constituents of the coating composition, of at least one amino resin (C), wherein the coating composition comprises at least one unsaturated, cyclic, sterically hindered amine (D) and the coating composition contains less than 2.5 mol % of hydrolyzable silane groups, based on the sum of hydroxyl groups, isocyanate groups, and hydrolyzable silane groups. The invention additionally relates to multistage coating processes using these coating compositions and also to the use of the coating compositions as clearcoat material and to the use of the coating process for automotive OEM finishing and automotive refinish.
摘要翻译：本发明提供包含至少一种含有羟基的化合物（A），至少一种含有异氰酸酯基团的化合物（B），至少5.0重量％，基于涂料组合物不挥发成分的至少一种氨基树脂（C），其中所述涂料组合物包含至少一种不饱和的环状空间位阻胺（D），并且所述涂料组合物包含小于2.5mol％的可水解硅烷基团，基于羟基，异氰酸酯基和可水解硅烷基团。本发明还涉及使用这些涂料组合物的多阶段涂布方法以及涂料组合物作为透明涂层材料的用途以及用于汽车OEM整理和汽车修补漆的涂覆方法的使用。

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