公开(公告)号：US20100196733A1

公开(公告)日：2010-08-05

申请号：US12602459

申请日：2008-05-15

Applicant: Andreas Stephan

Inventor： Andreas Stephan

IPC: B32B15/01 ,  B23K31/02 ,  B23K20/12 ,  B23K15/00 ,  B23K26/20

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: The present invention provides a composite skin for the aeronautics and astronautics industries, and also a method for producing a composite skin of this type. 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: 本发明提供了一种用于航空和航天工业的复合皮肤，以及这种类型的复合皮肤的制造方法。 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。

公开(公告)号：US20100192377A1

公开(公告)日：2010-08-05

申请号：US12721085

申请日：2010-03-10

Applicant: Andreas Stephan

Inventor： Andreas Stephan

IPC: B21D53/88

CPC classification number: B64C1/068 ,  B64C2001/0072 ,  B64F5/10 ,  Y02T50/43 ,  Y10T29/49616 ,  Y10T29/49622 ,  Y10T29/49947 ,  Y10T29/49956

Abstract: Disclosed is a method for producing a fuselage of an aircraft, wherein several fuselage sections that are arranged one behind another are joined together, comprises the following steps: a) production of an outer skin segment, the outer skin segment having on the underside a continuous longitudinal opening, b) widening the outer skin segment in order to introduce at least one floor frame, c) joining the outer skin segments to a rigid fuselage section which is already present, with the formation of a partial transverse seam, d) positioning a prefabricated lower shell in the longitudinal opening, in order to close the outer skin segment on the peripheral side, e) completing the partial transverse seam to form a transverse seam and joining the lower shell together with the outer skin segment with the formation of at least two longitudinal seams, and f) joining the floor frame together with the outer skin segment.

Abstract translation: 本发明公开了一种飞机机身的制造方法，其特征在于，将一个彼此靠后配置的几个机身部分接合在一起，包括以下步骤：a）制造外皮段，所述外皮部分在下侧具有连续的 纵向开口，b）加宽外皮段以便引入至少一个地板框架，c）将外皮段连接到已经存在的刚性机身部分，形成部分横向接缝，d）将 在纵向开口中预制的下壳体，以便封闭外周侧的外皮段，e）完成部分横向接缝以形成横向接缝，并将下壳体与外皮段连接至少形成 两个纵向接缝，以及f）将地板框架与外部皮肤部分连接在一起。

公开(公告)号：US20080250772A1

公开(公告)日：2008-10-16

申请号：US11783593

申请日：2007-04-10

Applicant: Stefan Becker ,  Carsten Schippers ,  Wolfgang Heikamp ,  Tobias Neumann ,  Andreas Stephan ,  Jens Gutekunst ,  Peter Biebricher

Inventor： Stefan Becker ,  Carsten Schippers ,  Wolfgang Heikamp ,  Tobias Neumann ,  Andreas Stephan ,  Jens Gutekunst ,  Peter Biebricher

IPC: B01D46/00

CPC classification number: B01D50/002 ,  B01D45/06 ,  B01D45/16 ,  B01D46/003 ,  B01D46/0031 ,  B01D2267/40 ,  F04C29/026

Abstract: Disclosed is a device for separating liquids from gases comprising a preseparator that separates an untreated gas region from a preseparator gas region, a main separator comprising a coalescing element for increasing the size of liquid droplets and a post-separator.

Abstract translation: 公开了一种用于从气体中分离液体的装置，包括将未处理气体区域与预分离器气体区域分离的预分离器，包括用于增加液滴尺寸的聚结元件的主分离器和后分离器。