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1. 发明申请

US20140202824A1 FASTENING DEVICE FOR RELEASABLY FASTENING A MECHANISM IN THE REGION OF A FLOOR OF AN AIRCRAFT OR SPACE CRAFT AND ARRANGEMENT FOR A CARGO LOADING SYSTEM 有权
标题翻译：适用于在航空器或空间布局和货物装载系统的布置区域中的机构的可移动装置
公开(公告)号：US20140202824A1
公开(公告)日：2014-07-24
申请号：US14163343
申请日：2014-01-24
申请人： AIRBUS OPERATIONS GMBH
发明人： Markus ESSER , Ali Lohmann , Jörg Pump , Sönke Hager , Johannes Völker
IPC分类号： B60R11/00 , B64C1/20 , B65G13/00 , B64D9/00
CPC分类号： B64C1/20 , B60R11/00 , B64D9/00 , B64D9/003 , B64D2009/006 , B64G1/22 , B65G13/00 , B65G13/11 , B65G21/02 , B65G21/06 , B65G39/12 , F16B21/02
摘要： A fastening device is disclosed for releasably fastening a mechanism in the region of a floor of an aircraft or spacecraft and includes a base component and a latch component. The latch component includes at least one holding portion including a latch-component-side holding face and is movably coupled to the base component between an unlocked and a locked position. When positioned in a predefined mounting position on the floor component and/or on the base component, the holding portion of the latch component engages a fastening portion, and the latch-component-side holding face faces the mechanism-side holding face. During passage of the latch component from locked position into unlocked position a gap between the latch-component-side holding face and the mechanism-side holding face continuously widens. The invention further relates to an arrangement for a cargo loading system.
摘要翻译：公开了一种紧固装置，用于将机构可释放地紧固在飞行器或航天器的地板区域中并且包括基座部件和闩锁部件。闩锁部件包括至少一个包括闩锁部件侧保持面的保持部分，并且在解锁和锁定位置之间可移动地联接到基部部件。当位于地板部件和/或基部部件上的预定安装位置时，闩锁部件的保持部分接合紧固部分，并且闩锁部件侧保持面面向机构侧保持面。在闩锁部件从锁定位置通过到解锁位置时，闩锁部件侧保持面和机构侧保持面之间的间隙持续变宽。本发明还涉及一种用于货物装载系统的装置。

2. 发明授权

US09975636B2 Cargo restraining assembly, cargo loading system and aircraft 有权
公开(公告)号：US09975636B2
公开(公告)日：2018-05-22
申请号：US14619819
申请日：2015-02-11
申请人： AIRBUS OPERATIONS GMBH
发明人： Frank Gutenkunst , André Koehler , Ali Lohmann , Joerg Pump , Soenke Hager
IPC分类号： B64D9/00 , B60P1/00 , B60P7/14
CPC分类号： B64D9/003 , B60P1/00 , B60P7/14
摘要： A cargo restraining assembly is configured to be mounted to a cargo deck surface of an aircraft, the cargo restraining assembly comprising two guidance and restraint bars running in parallel to each other, and at least one lateral bracket spanning between the two guidance and restraint bars and being fixedly connected to each of two guidance and restraint bars. The lateral bracket includes a bracket foot formed integrally with the lateral bracket and a quick release mechanism configured to quick-releasably couple the bracket foot to a seat track profile of the cargo deck surface of the aircraft.

3. 发明授权

US09302851B2 Fastening device for releasably fastening a mechanism in the region of a floor of an aircraft or space craft and arrangement for a cargo loading system 有权
标题翻译：紧固装置，用于可释放地将机构紧固在飞机的地板区域或用于货物装载系统的航天器和装置的区域中
公开(公告)号：US09302851B2
公开(公告)日：2016-04-05
申请号：US14163343
申请日：2014-01-24
申请人： AIRBUS OPERATIONS GMBH
发明人： Markus Esser , Ali Lohmann , Jörg Pump , Sönke Hager , Johannes Völker
IPC分类号： B65G13/11 , B65G39/12 , B65G21/02 , B65G21/06 , B60R11/00 , B64C1/20 , B65G13/00 , F16B21/02 , B64D9/00
CPC分类号： B64C1/20 , B60R11/00 , B64D9/00 , B64D9/003 , B64D2009/006 , B64G1/22 , B65G13/00 , B65G13/11 , B65G21/02 , B65G21/06 , B65G39/12 , F16B21/02
摘要： A fastening device is disclosed for releasably fastening a mechanism in the region of a floor of an aircraft or spacecraft and includes a base component and a latch component. The latch component includes at least one holding portion including a latch-component-side holding face and is movably coupled to the base component between an unlocked and a locked position. When positioned in a predefined mounting position on the floor component and/or on the base component, the holding portion of the latch component engages a fastening portion, and the latch-component-side holding face faces the mechanism-side holding face. During passage of the latch component from locked position into unlocked position a gap between the latch-component-side holding face and the mechanism-side holding face continuously widens. The invention further relates to an arrangement for a cargo loading system.
摘要翻译：公开了一种紧固装置，用于将机构可释放地紧固在飞行器或航天器的地板区域中并且包括基座部件和闩锁部件。闩锁部件包括至少一个包括闩锁部件侧保持面的保持部分，并且在解锁和锁定位置之间可移动地联接到基部部件。当位于地板部件和/或基部部件上的预定安装位置时，闩锁部件的保持部分接合紧固部分，并且闩锁部件侧保持面面向机构侧保持面。在闩锁部件从锁定位置通过到解锁位置时，闩锁部件侧保持面和机构侧保持面之间的间隙持续变宽。本发明还涉及一种用于货物装载系统的装置。

4. 发明授权

US10071796B2 Fastening device for releasably fastening a mechanism in the region of a floor of an aircraft or space craft and arrangement for a cargo loading system 有权
公开(公告)号：US10071796B2
公开(公告)日：2018-09-11
申请号：US15089909
申请日：2016-04-04
申请人： AIRBUS OPERATIONS GMBH
发明人： Markus Esser , Ali Lohmann , Jörg Pump , Sönke Hager , Johannes Völker
IPC分类号： B64C1/20 , B65G13/11 , B65G39/12 , B65G21/02 , B65G21/06 , B60R11/00 , B64D9/00 , B65G13/00 , F16B21/02 , B64G1/22
CPC分类号： B64C1/20 , B60R11/00 , B64D9/00 , B64D9/003 , B64D2009/006 , B64G1/22 , B65G13/00 , B65G13/11 , B65G21/02 , B65G21/06 , B65G39/12 , F16B21/02
摘要： A fastening device is disclosed for releasably fastening a mechanism in the region of a floor of an aircraft or spacecraft and includes a base component and a latch component. The latch component includes at least one holding portion including a latch-component-side holding face and is movably coupled to the base component between an unlocked and a locked position. When positioned in a predefined mounting position on the floor component and/or on the base component, the holding portion of the latch component engages a fastening portion, and the latch-component-side holding face faces the mechanism-side holding face. During passage of the latch component from locked position into unlocked position a gap between the latch-component-side holding face and the mechanism-side holding face continuously widens. The invention further relates to an arrangement for a cargo loading system.

5. 发明授权

US09630716B2 Cargo restraining barrier, cargo loading system and aircraft 有权
公开(公告)号：US09630716B2
公开(公告)日：2017-04-25
申请号：US14620372
申请日：2015-02-12
申请人： Airbus Operations GmbH
发明人： Joerg Pump , Soenke Hager , Johannes Voelker , Andre Koehler , Ali Lohmann
IPC分类号： B60P1/00 , B64D9/00 , B60P7/14
CPC分类号： B64D9/003 , B60P1/00 , B60P7/14
摘要： A cargo restraining barrier configured to be mounted to a cargo deck surface of an aircraft. The cargo restraining barrier includes a base portion, a barrier portion arranged substantially perpendicular to the base portion at a first edge on the top side of the base portion, a plurality of force diverting struts mounted in parallel along the extension of the barrier portion between a backside of the barrier portion and a second edge of the base portion opposite to the first edge of the base portion. The force diverting struts are configured to divert forces acting on the front side of the barrier portion towards the base portion, and a plurality of first latches distributed over the bottom side of the base portion, hooking into tie down rings of a cargo deck surface and to direct the diverted forces from the force diverting struts into the cargo deck surface.

6. 发明授权

US08931986B2 End stop device, cargo loading system and aircraft 有权
标题翻译：终端装置，货物装载系统和飞机
公开(公告)号：US08931986B2
公开(公告)日：2015-01-13
申请号：US14295568
申请日：2014-06-04
申请人： Airbus Operations GmbH
发明人： Markus Esser , André Koehler , Ali Lohmann , Joerg Pump , Soenke Hager , Edward Elliot-May
IPC分类号： B60P7/08 , B64D9/00 , B60P7/13
CPC分类号： B64D9/003 , B60P7/0807 , B60P7/13 , Y02T50/46
摘要： An end stop device for restraining an ULD from movement across a cargo deck surface of an aircraft includes a main body; and a mounting interface connected to the main body which is configured and arranged to attach the end stop device to the cargo deck by means of a corresponding tie down ring. Each mounting interface includes a tongue-like support plate which is partially protruding below a bottom side of the main body, at least one recess arranged in an area above the support plate, wherein side walls of the recess form a frame-like structure. and a bolt portion extending from the support plate into the recess and partially surrounded by the frame-like structure. The bolt portion is configured to engage the tie down ring in an operation mode where the end stop device is fixed to a tie down ring.
摘要翻译：用于限制ULD在飞行器的货物甲板表面上移动的终止装置包括主体; 以及连接到主体的安装界面，其被构造和布置成通过相应的制动环将终止装置附接到货物甲板。每个安装接口包括舌状支撑板，其部分地突出在主体的底侧下方，至少一个凹槽布置在支撑板上方的区域中，其中凹部的侧壁形成框架状结构。以及螺栓部分，其从支撑板延伸到凹部中并且被框架状结构部分地包围。螺栓部分构造成在终止装置被固定到系紧环的操作模式下接合系紧环。

7. 发明授权

US09376210B2 Cargo handling system 有权
标题翻译：货物处理系统
公开(公告)号：US09376210B2
公开(公告)日：2016-06-28
申请号：US14304243
申请日：2014-06-13
申请人： AIRBUS OPERATIONS GMBH
发明人： Ali Lohmann , André Koehler , Johannes Voelker , Christian Grambole , Matthias Ulbrich , Joerg Pump , Soenke Hager
IPC分类号： B60P7/08 , B64D9/00
CPC分类号： B64D9/00 , B60P7/0892
摘要： The invention relates to a cargo handling system for loading and securing one or more freight containers in a cargo hold of an aircraft. The system includes bracket members configured to be secured to a base or floor of the cargo hold, and elongate guide members, each of which is mounted on and interconnects a number of the bracket members arranged in a row, wherein each guide member forms a restraint or a stop against lateral movement of a freight container loaded in the cargo hold. The bracket members include at least one fastening portion configured for tool-less fast-release engagement and locking with a seat track profile in the base or floor of the cargo hold. Furthermore, the bracket members typically extend transversely inwards or inboard of the elongate guide members.
摘要翻译：本发明涉及一种用于装载和固定飞机的货舱中的一个或多个货物集装箱的货物处理系统。该系统包括构造成固定到货舱的基座或底板上的支架构件，以及细长导向构件，每个导向构件安装在一排布置成一排的多个支架构件上并互连，其中每个导向构件形成约束或者阻止装载在货舱中的货物集装箱的横向运动。托架构件包括至少一个紧固部分，该紧固部分构造成用于无需工具的快速释放接合，并且与座舱轨道轮廓锁定在货舱的底座或地板中。此外，支架构件通常横向地延伸到细长引导构件的内侧或内侧。

8. 发明申请

US20150225084A1 CARGO RESTRAINING BARRIER, CARGO LOADING SYSTEM AND AIRCRAFT 有权
标题翻译：货物限制障碍物，货物装载系统和飞机
公开(公告)号：US20150225084A1
公开(公告)日：2015-08-13
申请号：US14620372
申请日：2015-02-12
申请人： Airbus Operations GmbH
发明人： Joerg Pump , Soenke Hager , Johannes Voelker , Andre Koehler , Ali Lohmann
IPC分类号： B64D9/00 , B60P1/00
CPC分类号： B64D9/003 , B60P1/00 , B60P7/14
摘要： A cargo restraining barrier configured to be mounted to a cargo deck surface of an aircraft. The cargo restraining barrier includes a base portion, a barrier portion arranged substantially perpendicular to the base portion at a first edge on the top side of the base portion, a plurality of force diverting struts mounted in parallel along the extension of the barrier portion between a backside of the barrier portion and a second edge of the base portion opposite to the first edge of the base portion. The force diverting struts are configured to divert forces acting on the front side of the barrier portion towards the base portion, and a plurality of first latches distributed over the bottom side of the base portion, hooking into tie down rings of a cargo deck surface and to direct the diverted forces from the force diverting struts into the cargo deck surface.
摘要翻译：构造成安装在飞机的货物甲板表面上的货物限制障碍物。货物限制障碍物包括基部，在基部的顶侧上的第一边缘处基本上垂直于基部布置的阻挡部分，沿着阻挡部分的延伸部平行安装的多个力转向支柱所述阻挡部分的背面和所述基部的与所述基部的第一边缘相反的第二边缘。力转向支柱构造成将作用在阻挡部分的前侧上的力朝向基部部分转移，并且分配在基部的底侧上的多个第一闩锁钩住货物甲板表面的固定环，将转向力从转向支柱引导到货物甲板表面。

9. 发明申请

US20140369781A1 End Stop Device, Cargo Loading System And Aircraft 有权
标题翻译：终止装置，货物装载系统和飞机
公开(公告)号：US20140369781A1
公开(公告)日：2014-12-18
申请号：US14295568
申请日：2014-06-04
申请人： Airbus Operations GmbH
发明人： Markus Esser , André Koehler , Ali Lohmann , Joerg Pump , Soenke Hager , Edward Elliot-May
IPC分类号： B64D9/00 , B60P7/08 , B60P7/13
CPC分类号： B64D9/003 , B60P7/0807 , B60P7/13 , Y02T50/46
摘要： An end stop device for restraining an ULD from movement across a cargo deck surface of an aircraft includes a main body; and a mounting interface connected to the main body which is configured and arranged to attach the end stop device to the cargo deck by means of a corresponding tie down ring. Each mounting interface includes a tongue-like support plate which is partially protruding below a bottom side of the main body, at least one recess arranged in an area above the support plate, wherein side walls of the recess form a frame-like structure. and a bolt portion extending from the support plate into the recess and partially surrounded by the frame-like structure. The bolt portion is configured to engage the tie down ring in an operation mode where the end stop device is fixed to a tie down ring.
摘要翻译：用于限制ULD在飞行器的货物甲板表面上移动的终止装置包括主体; 以及连接到主体的安装界面，其被构造和布置成通过相应的制动环将终止装置附接到货物甲板。每个安装接口包括舌状支撑板，其部分地突出在主体的底侧下方，至少一个凹槽布置在支撑板上方的区域中，其中凹部的侧壁形成框架状结构。以及螺栓部分，其从支撑板延伸到凹部中并且被框架状结构部分地包围。螺栓部分构造成在终止装置被固定到系紧环的操作模式下接合系紧环。

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