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1. 发明授权

US08602356B2 Framework wing box for a wing 有权
公开(公告)号：US08602356B2
公开(公告)日：2013-12-10
申请号：US11990578
申请日：2006-08-17
申请人： Christian Maenz
发明人： Christian Maenz
IPC分类号： B64C3/22
CPC分类号： B64C3/22 , B64C3/00 , B64C3/26 , B64C5/06
摘要： A wing box for an aircraft wing with a framework and a first shell. The framework is connected to the first shell such that a load acting on the first shell can be transferred by the framework.

2. 发明授权

US07931234B2 Continuous fuselage connection 有权
标题翻译：连续机身连接
公开(公告)号：US07931234B2
公开(公告)日：2011-04-26
申请号：US12063736
申请日：2006-08-14
申请人： Christian Maenz
发明人： Christian Maenz
IPC分类号： B64C1/06
CPC分类号： B64C1/26 , B64C5/06
摘要： An attachment system for attaching a tail unit to an attachment surface of an aircraft is disclosed. An attachment surface may be a fuselage, for example. In an arrangement, the attachment system includes a mounting with a first bearing surface that is capable of resting against the tail unit, and a second bearing surface that is capable of resting against the attachment surface. The first bearing surface and the second bearing surface, of which there is at least one, include a common line of contact. In the arrangement, the planes of the first bearing surface and of the second bearing surface are at an angle that differs from 0° and 180°.
摘要翻译：公开了一种用于将尾部单元附接到飞行器的附接表面的附接系统。附接表面可以是例如机身。在一种布置中，附接系统包括具有能够抵靠尾部单元的第一支承表面的安装件和能够抵靠附接表面的第二支承表面。第一轴承表面和第二轴承表面（其中至少有一个）包括公共接触线。在该结构中，第一支承面和第二支承面的平面成为0°和180°不同的角度。

3. 发明申请

US20090294590A1 Framework wing box for a wing 有权
标题翻译：框架翼框为翼
公开(公告)号：US20090294590A1
公开(公告)日：2009-12-03
申请号：US11990578
申请日：2006-08-17
申请人： Christian Maenz
发明人： Christian Maenz
IPC分类号： B64C3/22
CPC分类号： B64C3/22 , B64C3/00 , B64C3/26 , B64C5/06
摘要： A wing box for an aircraft wing with a framework and a first shell. The framework is connected to the first shell such that a load acting on the first shell can be transferred by the framework.
摘要翻译：飞机机翼的翼盒，带有框架和第一个外壳。框架连接到第一壳体，使得作用在第一壳体上的负载可以由框架传递。

4. 发明申请

US20080203228A1 Double-Shell Design Center Box 审中-公开
标题翻译：双壳设计中心盒
公开(公告)号：US20080203228A1
公开(公告)日：2008-08-28
申请号：US11997490
申请日：2006-05-11
申请人： Christian Maenz
发明人： Christian Maenz
IPC分类号： B64C3/00
CPC分类号： B64C1/26 , B64C3/182 , B64C3/26 , B64C5/06
摘要： The present invention relates to a center box (5) for an aircraft wing, as well as to an aircraft comprising such a center box (5). The center box (5) essentially comprises two lateral surfaces (6), which in turn essentially comprise two internal and external skins (2, 1) that are arranged so as to be spaced apart from each other. In order to provide adequate stability to the lateral surface (6), the internal skin (2) and the external skin (1) are interconnected by way of a multitude of profiles (3).
摘要翻译：本发明涉及一种用于飞机机翼的中心箱（5）以及包括这种中心箱（5）的飞机。中心盒（5）基本上包括两个侧表面（6），该侧表面又基本上包括两个彼此间隔开的内部和外部表皮（2,1）。为了向侧表面（6）提供足够的稳定性，内部皮肤（2）和外部皮肤（1）通过多个轮廓（3）相互连接。

5. 发明申请

US20100170995A1 SUPPORT STRUCTURE FOR A WING 有权
标题翻译：支持结构
公开(公告)号：US20100170995A1
公开(公告)日：2010-07-08
申请号：US12063699
申请日：2006-08-16
申请人： Christian Maenz
发明人： Christian Maenz
IPC分类号： B64C3/00 , B64C1/06 , F16B7/00
CPC分类号： B64C1/26 , B64C3/00 , B64C3/26 , B64C5/06 , E04B2001/193 , Y10T403/4381
摘要： A support structure for an aircraft, includes one or several bar elements and one or several junction elements. At least one bar element includes a transition region which can be made to engage at least one junction element. When the transition region of the bar element engages at least one junction element, centric force transmission takes place between the bar element and the junction element.
摘要翻译：用于飞行器的支撑结构包括一个或几个杆元件和一个或多个接合元件。至少一个杆元件包括能够使至少一个接合元件接合的过渡区域。当杆元件的过渡区域接合至少一个接合元件时，在杆元件和接合元件之间发生中心的力传递。

6. 发明申请

US20090114772A1 CONTINUOUS FUSELAGE CONNECTION 有权
标题翻译：连续熔接连接
公开(公告)号：US20090114772A1
公开(公告)日：2009-05-07
申请号：US12063736
申请日：2006-08-14
申请人： Christian Maenz
发明人： Christian Maenz
IPC分类号： B64C1/26
CPC分类号： B64C1/26 , B64C5/06
摘要： An attachment system for attaching a tail unit to an attachment surface of an aircraft is disclosed. An attachment surface may be a fuselage, for example. In an arrangement, the attachment system includes a mounting with a first bearing surface that is capable of resting against the tail unit, and a second bearing surface that is capable of resting against the attachment surface. The first bearing surface and the second bearing surface, of which there is at least one, include a common line of contact. In the arrangement, the planes of the first bearing surface and of the second bearing surface are at an angle that differs from 0° and 180°.
摘要翻译：公开了一种用于将尾部单元附接到飞行器的附接表面的附接系统。附接表面可以是例如机身。在一种布置中，附接系统包括具有能够抵靠尾部单元的第一支承表面的安装件和能够抵靠附接表面的第二支承表面。第一轴承表面和第二轴承表面（其中至少有一个）包括公共接触线。在该结构中，第一支承面和第二支承面的平面成为0°和180°不同的角度。

7. 发明授权

US08205834B2 Support structure for a wing 有权
标题翻译：翼的支撑结构
公开(公告)号：US08205834B2
公开(公告)日：2012-06-26
申请号：US12063699
申请日：2006-08-16
申请人： Christian Maenz
发明人： Christian Maenz
IPC分类号： B64C3/22
CPC分类号： B64C1/26 , B64C3/00 , B64C3/26 , B64C5/06 , E04B2001/193 , Y10T403/4381
摘要： A support structure for an aircraft, includes one or several bar elements and one or several junction elements. At least one bar element includes a transition region which can be made to engage at least one junction element. When the transition region of the bar element engages at least one junction element, centric force transmission takes place between the bar element and the junction element.
摘要翻译：用于飞行器的支撑结构包括一个或几个杆元件和一个或多个接合元件。至少一个杆元件包括能够使至少一个接合元件接合的过渡区域。当杆元件的过渡区域接合至少一个接合元件时，在杆元件和接合元件之间发生中心的力传递。

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