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    PRESSURE BULKHEAD AND METHOD FOR SUBDIVISION OF AN AIRCRAFT OR SPACECRAFT
    11.
    发明申请
    PRESSURE BULKHEAD AND METHOD FOR SUBDIVISION OF AN AIRCRAFT OR SPACECRAFT 有权
    压力容器和用于分配飞机或间隙的方法

    公开(公告)号：US20100230539A1

    公开(公告)日：2010-09-16

    申请号：US12678723

    申请日：2008-06-18

    Applicant: Stephan Mischereit ,  Andreas Stephan

    Inventor： Stephan Mischereit ,  Andreas Stephan

    IPC: B64C1/10

    CPC classification number: B64C1/10

    Abstract: The present invention provides a pressure bulkhead for subdivision of an aircraft or spacecraft into an internal and an external pressure region. The pressure bulkhead comprises a pressure plate having an edge shaped so as to correspond to an inner contour of the aircraft or spacecraft, a supporting means which tiltably supports the edge on the inner contour, and a seal which seals the edge with the inner contour. A further aspect of the invention provides a method for subdivision of an aircraft or spacecraft into an internal and an external pressure region. Firstly, a pressure plate is provided that has an edge shaped so as to correspond to an inner contour of the aircraft or spacecraft. In further steps, the edge is tiltably supported on the inner contour and sealed with the inner contour.

    Abstract translation: 本发明提供一种用于将飞行器或航天器分成内部和外部压力区域的压力舱壁。 压力隔板包括压板，该压板具有与航空器或航天器的内轮廓相对应的边缘，可倾斜地支撑内轮廓上的边缘的支撑装置和将边缘与内轮廓密封的密封件。 本发明的另一方面提供了一种用于将飞行器或航天器细分成内部和外部压力区域的方法。 首先，提供压板，该压板的边缘成形为对应于飞行器或航天器的内轮廓。 在另外的步骤中，边缘可倾斜地支撑在内轮廓上并用内轮廓密封。

    Shadow mask and method for producing a shadow mask
    13.
    发明授权
    Shadow mask and method for producing a shadow mask 失效
    阴影掩模和产生荫罩的方法

    公开(公告)号：US07183043B2

    公开(公告)日：2007-02-27

    申请号：US10344710

    申请日：2001-08-14

    Applicant: Jan Meijer ,  Andreas Stephan ,  Ulf Weidenmuller ,  Ivo Rangelow

    Inventor： Jan Meijer ,  Andreas Stephan ,  Ulf Weidenmuller ,  Ivo Rangelow

    IPC: G03F1/00 ,  G03C5/00

    CPC classification number: G03F1/20

    Abstract: The disclosed device is directed towards a shadow mask for ion beams comprising a silicon wafer with a hole pattern arranged therein, wherein the silicon wafer is provided at a side confronting the incident ion beams with a metallic coating which stops the ion beams and dissipates heat, wherein an apertured region of the silicon wafer has a thickness from about 20 μm to about 200 μm and apertures in the shadow mask have lateral dimensions from about 0.5 μm to about 3 μm.

    Abstract translation: 所公开的装置指向用于离子束的阴影掩模，所述阴影掩模包含布置在其中的孔图案的硅晶片，其中所述硅晶片设置在与入射离子束相对的一侧，金属涂层停止所述离子束并散发热量， 其中硅晶片的有孔区域具有约20μm至约200μm的厚度，并且荫罩中的孔径具有约0.5μm至约3μm的横向尺寸。

    Method for producing a composite skin in the field of aeronautics and astronautics
    14.
    发明授权
    Method for producing a composite skin in the field of aeronautics and astronautics 有权
    在航空和航天领域生产复合皮肤的方法

    公开(公告)号：US09314875B2

    公开(公告)日：2016-04-19

    申请号：US12602459

    申请日：2008-05-15

    Applicant: Andreas Stephan

    Inventor： Andreas Stephan

    IPC: B23P11/00 ,  B21D53/88 ,  B23K26/24 ,  B21J15/00 ,  B21J15/14 ,  B23K15/00 ,  B23K20/12 ,  B23K26/26 ,  B64C1/06 ,  B64C1/12

    CPC classification number: B23K26/24 ,  B21J15/00 ,  B21J15/142 ,  B23K15/0006 ,  B23K20/122 ,  B23K26/26 ,  B23K2101/18 ,  B23K2103/10 ,  B64C1/069 ,  B64C1/12 ,  Y02T50/43 ,  Y10T29/49966 ,  Y10T29/49968 ,  Y10T428/12

    Abstract: A composite skin for the aeronautics and astronautics industries, and also a method for producing a composite skin of this type is provided. The method comprises the following method steps: removing excess material from a butt plate to form a butt strap at one end thereof, subsequently connecting the other end of the butt plate to a skin plate with a substance-to-substance bond, and then fastening a further skin plate to the butt strap to form the composite skin. The idea behind the invention involves replacing a rivet connection with a substance-to-substance bond. This provides the advantage that the weight of the composite skin and the production costs for the composite skin are reduced.

    Abstract translation: 提供了一种用于航空和航天工业的复合皮肤，以及一种生产这种复合皮肤的方法。 该方法包括以下方法步骤：从对接板去除多余的材料以在其一端形成对接带，随后将对接板的另一端连接到具有物质 - 物质粘合的表皮板，然后紧固 一个进一步的皮肤板到对接带形成复合皮肤。 本发明的想法涉及用物质与物质之间的接合来更换铆钉连接。 这提供了复合皮肤的重量和复合皮肤的生产成本降低的优点。

    Structure, especially a fuselage structure of an aircraft or a spacecraft
    15.
    发明授权
    Structure, especially a fuselage structure of an aircraft or a spacecraft 有权
    结构，特别是飞机或航天器的机身结构

    公开(公告)号：US08366043B2

    公开(公告)日：2013-02-05

    申请号：US12740880

    申请日：2008-10-31

    Applicant: Andreas Stephan

    Inventor： Andreas Stephan

    IPC: B64C1/00

    CPC classification number: B64C1/10

    Abstract: The present invention provides a fuselage structure (1; 1′) of an aircraft comprising an annular skin segment (2; 2′) which has a cross-sectional opening (3; 3′), a pressure cap (4; 4′) for a pressure-tight closure of the cross-sectional opening (3; 3′), and a plurality of tension struts (7, 8, 9; 7′, 8′, 9′) which in each case connect the pressure cap (4; 4′) to the annular skin segment (2; 2′) and absorb loads acting on the pressure cap (4; 4′), as tensile loads. This advantageously means that the tension struts (7, 8, 9; 7′, 8′, 9′) do not have to absorb substantially any bending moments. Consequently, the tension struts can be produced with a relatively small cross section, which entails a reduction in weight. Furthermore, it is possible to produce and mount tension struts (7, 8, 9; 7′, 8′, 9′) of this type in a simple manner.

    Abstract translation: 本发明提供一种飞行器的机身结构（1; 1'），其包括具有横截面开口（3; 3'），压力盖（4; 4'）的环形皮肤段（2; 2'）， 用于横截面开口（3; 3'）的压力密封，以及多个张力支柱（7,8,9; 7'，8'，9'），其在每种情况下连接压力盖（ 4; 4'）连接到环形皮肤部分（2; 2'）并吸收作用在压力帽（4; 4'）上的负载作为拉伸载荷。 这有利地意味着张力支柱（7,8,9; 7'，8'，9'）不必基本上吸收任何弯曲力矩。 因此，张力支柱可以以相对小的横截面产生，这需要减轻重量。 此外，可以简单地制造和安装这种类型的张紧支柱（7,8,9，7'，8'，9'）。

    Air dryer cartridge
    19.
    发明授权
    Air dryer cartridge 有权
    空气干燥筒

    公开(公告)号：US07846242B2

    公开(公告)日：2010-12-07

    申请号：US10554922

    申请日：2004-05-19

    Applicant: Mark Paling ,  Andrew G. L. Blackwood ,  Ignitius Milomo ,  Stephan Niemeyer ,  Christian Fischer ,  Andreas Stephan

    Inventor： Mark Paling ,  Andrew G. L. Blackwood ,  Ignitius Milomo ,  Stephan Niemeyer ,  Christian Fischer ,  Andreas Stephan

    IPC: B01D53/02

    CPC classification number: B01D53/261 ,  B01D2201/291 ,  B60T17/004 ,  Y10S55/17

    Abstract: An air dryer desiccant cartridge, the cartridge comprising a base having an inlet and an outlet, and a casing connected to the base to define a cavity there between, wherein the cavity contains a filter and a desiccant, the filter being arranged upstream of the desiccant such that during normal operation fluid flow entering the cartridge through the inlet passes through the filter and then on to the desiccant before reaching the outlet, and during purging of the cartridge purge flow entering the outlet passes through the desiccant before reaching the filter, wherein further the cartridge includes a valve operable to permit a portion of the purge flow to bypass the filter.

    Abstract translation: 一种空气干燥剂干燥剂盒，所述盒包括具有入口和出口的底座，以及连接到所述基座以在其间限定空腔的壳体，其中所述空腔包含过滤器和干燥剂，所述过滤器布置在所述干燥剂的上游 使得在正常操作期间，通过入口进入料筒的流体流动通过过滤器，然后在到达出口之前进入干燥剂，并且在吹扫进入出口的料筒清洗流程在到达过滤器之前通过干燥剂，其中进一步 该墨盒包括可操作以允许清洗流的一部分绕过过滤器的阀。

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