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1. 发明授权

US08220744B2 Fitting for introducing high forces into a fuselage cell of an aircraft 有权
标题翻译：适用于将高力量引入飞机的机身单元
公开(公告)号：US08220744B2
公开(公告)日：2012-07-17
申请号：US12009149
申请日：2008-01-16
申请人： Herrmann Benthien
发明人： Herrmann Benthien
IPC分类号： B64C1/06
CPC分类号： B60P7/0807 , B64D9/00 , B64D9/003 , Y02T50/46
摘要： Disclosed is a fitting for introducing great loads into a fuselage cell of an aircraft, in particular those which emanate from undercarriage components or are introduced into them. The fitting has a shoulder plate for bearing against the inside of the skin of the fuselage cell for example over its full surface area. Arranged underneath the shoulder plate is a vertical lug shackle with a lug for introducing the loads, wherein the lug shackle is led to the outside through a clearance in the skin of the fuselage cell. At least one approximately upright fastening shackle is provided on the upper side of the shoulder plate for connecting the fitting to a frame web. According to the invention, the loads occurring are introduced into the frame, substantially “moment-free” in the region of a neutral fiber, so that the said frame is not exposed to any appreciable flexural stresses and can be of a more lightweight design. The frame becomes the load introducing instrument and distributes the loads uniformly into the skin of the fuselage cell. Radially acting loads are transferred from the shoulder plate directly into the skin of the fuselage cell by way of shearing.
摘要翻译：公开了一种用于将大负载引入飞机的机身单元中的装置，特别是从起落架部件发出或被引入其中的那些。配件具有用于例如在其整个表面区域上抵靠机身单元的皮肤内部的肩板。安置在肩板下面的是具有用于引入负载的凸耳的垂直凸耳钩环，其中通过机身单元的皮肤中的间隙将凸耳钩环导向外部。至少一个大致直立的紧固钩环设置在肩板的上侧，用于将配件连接到框架网。根据本发明，发生的载荷被引入框架中，在中性纤维的区域中基本上“无力”，使得所述框架不暴露于任何明显的弯曲应力并且可以是更轻量化的设计。框架成为载荷引导仪器，并将载荷均匀分布到机身单元的皮肤中。径向作用载荷通过剪切从肩板直接传递到机身细胞的皮肤。

2. 发明授权

US07895810B2 Crash paddle for reinforcing a primary fuselage structure of an aircraft 有权
标题翻译：用于加强飞机的主要机身结构的碰撞桨
公开(公告)号：US07895810B2
公开(公告)日：2011-03-01
申请号：US12009620
申请日：2008-01-18
申请人： Herrmann Benthien
发明人： Herrmann Benthien
IPC分类号： E04C3/00 , B64C1/00
CPC分类号： B60P7/0807 , B64D9/00 , B64D9/003 , Y02T50/46
摘要： Disclosed is a crash paddle for reinforcing a primary fuselage structure of an aircraft. The crash paddle may be used for connecting the floor to the primary fuselage structure. The crash paddle includes a beam with in particular an H-shaped cross-sectional geometry, butt straps being arranged at both ends of the beam for connecting the crash paddle. In the region of the ends of the beam, the beam respectively has a resting surface 13, 14, the geometrical shape of which substantially corresponds to a hollow cylinder halved in the longitudinal direction. Placed around both resting surfaces and the longitudinal sides of the beam, in a peripheral groove is at least one endless loop. The endless loops respectively comprise an arrangement of reinforcing fibers, which is formed by a plurality of reinforcing fibers, such as for example carbon fibers, running substantially parallel to the longitudinal axis of the beam. The presence of the endless loops allows the crash paddle to absorb safely the tensile forces that are generally relevant in critical flying situations. The beam can therefore be dimensioned lighter for the usually considerably smaller compressive and tensile loads that occur in normal flying operation, so that a considerable weight saving is obtained.
摘要翻译：公开了一种用于加强飞行器的主机身结构的碰撞桨。防撞板可用于将地板连接到主机身结构。碰撞桨包括具有特别是H形横截面几何形状的梁，对接带布置在梁的两端以连接碰撞桨。在梁的端部的区域中，梁分别具有搁置表面13,14，其几何形状基本上对应于在纵向方向上减半的中空圆柱体。放置在两个搁置表面和横梁的纵向边缘的周边槽中是至少一个无限循环。无端环分别包括增强纤维的布置，其由多个增强纤维形成，例如碳纤维，其基本上平行于梁的纵向轴线延伸。无限循环的存在允许碰撞桨安全地吸收通常在关键飞行情况下相关的拉力。因此，对于在正常飞行操作中发生的通常相当小的压缩和拉伸载荷，梁的尺寸可以更轻，从而获得相当大的重量。

3. 发明申请

US20080173756A1 Lining framework for an aircraft 有权
标题翻译：飞机的衬里框架
公开(公告)号：US20080173756A1
公开(公告)日：2008-07-24
申请号：US12009625
申请日：2008-01-18
申请人： Herrmann Benthien
发明人： Herrmann Benthien
IPC分类号： B64D11/06
CPC分类号： B60P7/0807 , B64D9/00 , B64D9/003 , Y02T50/46
摘要： Disclosed is a lining framework for fastening seats in an aircraft. The lining framework preferably comprises three seat rails, which are arranged in a spaced apart manner parallel to each other along both side walls of the fuselage cell. Sitting surfaces of a plurality of seats are suspended on the seat rails by textile straps consisting of high-strength, woven plastic material. At least two straps are arranged between the upper seat rail and two frames of the fuselage cell of the aircraft. In this case, a strap length is measured so that forces from the fuselage cell cannot be transmitted into the lining framework. By the same token, however, forces from the lining framework can be introduced into the fuselage cell by means of the straps so that the lining framework can be designed statically lighter. This leads to a weight reduction of the lining framework.
摘要翻译：公开了用于紧固飞机中的座椅的衬里框架。衬里框架优选地包括三个座椅导轨，它们以机身单元的两个侧壁彼此平行的间隔布置的方式布置。通过由高强度编织塑料材料组成的织物带将多个座位的座面悬挂在座椅导轨上。在上座椅导轨和飞机的机身单元的两个框架之间布置有至少两个带子。在这种情况下，测量带长度，使得来自机身单元的力不能传递到衬里框架中。然而，同样的道理，衬里框架的力可以通过带子被引入到机身单元中，使得衬里框架可以设计得更轻。这导致衬里框架的重量减轻。

4. 发明申请

US20080173755A1 Floor panel for forming a loading area in a cargo hold of an aircraft 有权
标题翻译：用于在飞机的货舱中形成装载区域的地板
公开(公告)号：US20080173755A1
公开(公告)日：2008-07-24
申请号：US12008975
申请日：2008-01-15
申请人： Herrmann Benthien
发明人： Herrmann Benthien
IPC分类号： B64C1/20
CPC分类号： B60P7/0807 , B64D9/00 , B64D9/003 , Y02T50/46
摘要： Disclosed is a floor panel, in particular for covering floors of cargo holds of aircraft. The floor panel is formed by a plurality of milled profiles, which are friction stir welded in each case along their longitudinal edges, with preference continuously to form longitudinal (butt) seams. The milled profiles each form a beam “of equal stress”, with an upper flange and a lower flange which are spaced apart from one another along their extent. The milled profiles have in each case a double-T-shaped cross-sectional profile, the upper flanges and the lower flanges being respectively connected by webs. With preference, the milled profiles are milled out in one piece from solid material of a sufficiently tough aluminium alloy. The joining together of the floor panel including a plurality of milled profiles that are arranged in parallel and friction stir welded allows a high mechanical load-bearing capacity of the floor panel in comparison with conventional sandwich floor panels along with a comparatively low weight.
摘要翻译：公开了一种地板，特别是用于覆盖飞机货舱的地板。地板镶板由多个铣削型材形成，每个铣削型材沿其纵向边缘在每种情况下摩擦搅拌焊接，优选连续地形成纵向（对接）接缝。铣削的型材每个都形成具有相等应力的梁，具有沿其范围彼此间隔开的上凸缘和下凸缘。铣削型材在每种情况下都是双T形横截面轮廓，上凸缘和下凸缘分别通过腹板连接。优选地，铣削型材由足够坚固的铝合金的固体材料一次研磨。包括平行布置和摩擦搅拌焊接的多个铣削型材的地板镶板的连接在一起，与现有的三明治地板面板相比较，具有较高的机械承载能力。

5. 发明授权

US08408492B2 Floor panel for forming a loading area in a cargo hold of an aircraft 有权
标题翻译：用于在飞机的货舱中形成装载区域的地板
公开(公告)号：US08408492B2
公开(公告)日：2013-04-02
申请号：US12008975
申请日：2008-01-15
申请人： Herrmann Benthien
发明人： Herrmann Benthien
IPC分类号： B64C1/18 , E04C3/00
CPC分类号： B60P7/0807 , B64D9/00 , B64D9/003 , Y02T50/46
摘要： A floor panel, in particular for covering floors of cargo holds of aircraft, is formed by a plurality of milled profiles, which are friction stir welded along their longitudinal edges, with preference continuously to form longitudinal (butt) seams. The milled profiles each form a beam “of equal stress”, with an upper flange and a lower flange spaced apart from one another along their extent. The milled profiles have a double-T-shaped cross-sectional profile, the upper flanges and the lower flanges being respectively connected by webs. With preference, the milled profiles are milled out in one piece from solid material of a sufficiently tough aluminum alloy. The joining together of the floor panel including a plurality of milled profiles that are arranged in parallel and friction stir welded allows a high mechanical load-bearing capacity of the floor panel in comparison with conventional sandwich floor panels along with a comparatively low weight.
摘要翻译：特别是用于覆盖飞机货架的地板的地板由多个铣削型材形成，多个铣削型材沿其纵向边缘摩擦搅拌焊接，优选地连续地形成纵向（对接）接缝。铣削型材每个都形成相等应力的梁，上凸缘和下凸缘沿其间隔彼此间隔开。研磨型材具有双T形横截面轮廓，上凸缘和下凸缘分别通过腹板连接。优选地，铣削型材由足够坚固的铝合金的固体材料一次研磨。包括平行布置和摩擦搅拌焊接的多个铣削型材的地板镶板的连接在一起，与现有的三明治地板面板相比较，具有较高的机械承载能力。

6. 发明授权

US07462006B2 Fastening arrangement for lashing brackets in the floor of a cargo hold of an aircraft 有权
标题翻译：紧固安装在一架飞机的货舱的地板上绑扎支架
公开(公告)号：US07462006B2
公开(公告)日：2008-12-09
申请号：US12009150
申请日：2008-01-16
申请人： Herrmann Benthien
发明人： Herrmann Benthien
IPC分类号： B60P7/08
CPC分类号： B60P7/0807 , B64D9/00 , B64D9/003 , Y02T50/46
摘要： Disclosed is a fastening arrangement for lashing brackets in the floor of a cargo hold of an aircraft. In this case, a plurality of channels that extend in the longitudinal direction of the aircraft, together with transverse profiles or frames lying under them, form a grid-like floor framework. The frames and the channels extend in each case preferably such that they are uniformly spaced apart and parallel to one another. A lashing bracket is pivotably accommodated in the at least one channel. The connection between the lashing bracket, the channel and the frame can be performed with two half-barrel nuts, which are arranged in the region of a thickening of the web of the frame and into which two screw bolts are screwed.
摘要翻译：公开了一种用于在飞机的货舱的地板上捆扎支架的紧固装置。在这种情况下，沿着飞行器的纵向方向延伸的多个通道以及位于其下方的横向轮廓或框架形成格栅状的地板框架。框架和通道在每种情况下优选地延伸使得它们彼此均匀间隔开并平行。绑定支架可枢转地容纳在至少一个通道中。捆扎支架，通道和框架之间的连接可以用两个半圆筒形螺母进行，这两个半圆筒螺母布置在框架的腹板的增厚区域中，并且两个螺栓被螺纹拧入。

7. 发明授权

US07775479B2 Lining framework for an aircraft 有权
标题翻译：飞机的衬里框架
公开(公告)号：US07775479B2
公开(公告)日：2010-08-17
申请号：US12009625
申请日：2008-01-18
申请人： Herrmann Benthien
发明人： Herrmann Benthien
IPC分类号： B64D25/00
CPC分类号： B60P7/0807 , B64D9/00 , B64D9/003 , Y02T50/46
摘要： Disclosed is a lining framework for fastening seats in an aircraft. The lining framework preferably comprises three seat rails, which are arranged in a spaced apart manner parallel to each other along both side walls of the fuselage cell. Sitting surfaces of a plurality of seats are suspended on the seat rails by textile straps consisting of high-strength, woven plastic material. At least two straps are arranged between the upper seat rail and two frames of the fuselage cell of the aircraft. In this case, a strap length is measured so that forces from the fuselage cell cannot be transmitted into the lining framework. By the same token, however, forces from the lining framework can be introduced into the fuselage cell by means of the straps so that the lining framework can be designed statically lighter. This leads to a weight reduction of the lining framework.
摘要翻译：公开了用于紧固飞机中的座椅的衬里框架。衬里框架优选地包括三个座椅导轨，它们以机身单元的两个侧壁彼此平行的间隔布置的方式布置。通过由高强度编织塑料材料组成的织物带将多个座位的座面悬挂在座椅导轨上。在上座椅导轨和飞机的机身单元的两个框架之间布置有至少两个带子。在这种情况下，测量带长度，使得来自机身单元的力不能传递到衬里框架中。然而，同样的道理，衬里框架的力可以通过带子被引入到机身单元中，使得衬里框架可以被设计得更轻。这导致衬里框架的重量减轻。

8. 发明申请

US20080175685A1 Fastening arrangement for lashing brackets in the floor of a cargo hold of an aircraft 有权
公开(公告)号：US20080175685A1
公开(公告)日：2008-07-24
申请号：US12009150
申请日：2008-01-16
申请人： Herrmann Benthien
发明人： Herrmann Benthien
IPC分类号： B61D45/00
CPC分类号： B60P7/0807 , B64D9/00 , B64D9/003 , Y02T50/46
摘要： Disclosed is a fastening arrangement for lashing brackets in the floor of a cargo hold of an aircraft. In this case, a plurality of channels that extend in the longitudinal direction of the aircraft, together with transverse profiles or frames lying under them, form a grid-like floor framework. The frames and the channels extend in each case preferably such that they are uniformly spaced apart and parallel to one another. A lashing bracket is pivotably accommodated in the at least one channel. The connection between the lashing bracket, the channel and the frame can be performed with two half-barrel nuts, which are arranged in the region of a thickening of the web of the frame and into which two screw bolts are screwed.

9. 发明申请

US20080173761A1 Fitting for introducing high forces into a fuselage cell of an aircraft 有权
标题翻译：适用于将高力量引入飞机的机身单元
公开(公告)号：US20080173761A1
公开(公告)日：2008-07-24
申请号：US12009149
申请日：2008-01-16
申请人： Herrmann Benthien
发明人： Herrmann Benthien
IPC分类号： B64C1/06
CPC分类号： B60P7/0807 , B64D9/00 , B64D9/003 , Y02T50/46
摘要： Disclosed is a fitting for introducing great loads into a fuselage cell of an aircraft, in particular those which emanate from undercarriage components or are introduced into them. The fitting has a shoulder plate for bearing against the inside of the skin of the fuselage cell for example over its full surface area. Arranged underneath the shoulder plate is a vertical lug shackle with a lug for introducing the loads, wherein the lug shackle is led to the outside through a clearance in the skin of the fuselage cell. At least one approximately upright fastening shackle is provided on the upper side of the shoulder plate for connecting the fitting to a frame web. According to the invention, the loads occurring are introduced into the frame, substantially “moment-free” in the region of a neutral fiber, so that the said frame is not exposed to any appreciable flexural stresses and can be of a more lightweight design. The frame becomes the load introducing instrument and distributes the loads uniformly into the skin of the fuselage cell. Radially acting loads are transferred from the shoulder plate directly into the skin of the fuselage cell by way of shearing.
摘要翻译：公开了一种用于将大负载引入飞机的机身单元中的装置，特别是从起落架部件发出或被引入其中的那些。配件具有用于例如在其整个表面区域上抵靠机身单元的皮肤内部的肩板。安置在肩板下面的是具有用于引入负载的凸耳的垂直凸耳钩环，其中通过机身单元的皮肤中的间隙将凸耳钩环导向外部。至少一个大致直立的紧固钩环设置在肩板的上侧，用于将配件连接到框架网。根据本发明，发生的载荷被引入框架中，在中性纤维的区域中基本上“无力”，使得所述框架不暴露于任何明显的弯曲应力并且可以是更轻的设计。框架成为载荷引导仪器，并将载荷均匀分布到机身单元的皮肤中。径向作用载荷通过剪切从肩板直接传递到机身细胞的皮肤。

10. 发明申请

US20080173758A1 Crash paddle for reinforcing a primary fuselage structure of an aircraft 有权
标题翻译：用于加强飞机的主要机身结构的碰撞桨
公开(公告)号：US20080173758A1
公开(公告)日：2008-07-24
申请号：US12009620
申请日：2008-01-18
申请人： Herrmann Benthien
发明人： Herrmann Benthien
IPC分类号： B64C1/00
CPC分类号： B60P7/0807 , B64D9/00 , B64D9/003 , Y02T50/46
摘要： Disclosed is a crash paddle for reinforcing a primary fuselage structure of an aircraft. The crash paddle may be used for connecting the floor to the primary fuselage structure. The crash paddle includes a beam with in particular an H-shaped cross-sectional geometry, butt straps being arranged at both ends of the beam for connecting the crash paddle. In the region of the ends of the beam, the beam respectively has a resting surface 13, 14, the geometrical shape of which substantially corresponds to a hollow cylinder halved in the longitudinal direction. Placed around both resting surfaces and the longitudinal sides of the beam, in a peripheral groove is at least one endless loop. The endless loops respectively comprise an arrangement of reinforcing fibers, which is formed by a plurality of reinforcing fibers, such as for example carbon fibers, running substantially parallel to the longitudinal axis of the beam. The presence of the endless loops allows the crash paddle to absorb safely the tensile forces that are generally relevant in critical flying situations. The beam can therefore be dimensioned lighter for the usually considerably smaller compressive and tensile loads that occur in normal flying operation, so that a considerable weight saving is obtained.
摘要翻译：公开了一种用于加强飞行器的主机身结构的碰撞桨。防撞板可用于将地板连接到主机身结构。碰撞桨包括具有特别是H形横截面几何形状的梁，对接带布置在梁的两端以连接碰撞桨。在梁的端部的区域中，梁分别具有搁置表面13,14，其几何形状基本上对应于在纵向方向上减半的中空圆柱体。放置在两个搁置表面和横梁的纵向边缘的周边槽中是至少一个无限循环。无端环分别包括增强纤维的布置，其由多个增强纤维形成，例如碳纤维，其基本上平行于梁的纵向轴线延伸。无限循环的存在允许碰撞桨安全地吸收通常在关键飞行情况下相关的拉力。因此，对于在正常飞行操作中发生的通常相当小的压缩和拉伸载荷，梁的尺寸可以更轻，从而获得相当大的重量。

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