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公开(公告)号:EP3345844A3
公开(公告)日:2018-10-03
申请号:EP17202990.2
申请日:2017-11-22
申请人: Verma, Vishaal B.
发明人: Verma, Vishaal B.
CPC分类号: B65D33/007 , B29C53/06 , B65B67/1255 , B65D5/4266
摘要: A device (20) for selectively retaining a package opening in a gaping configuration and a package (60) including the device (20) applied to a package body (70). The device (20) includes a circumferential strip (24) with side seams formed as vertical or longitudinal hinges (28). One or more tabs (40) extend in a first axial direction from an upper edge of the circumferential strip (24) at the side seams. Each tab (40) is coupled to the circumferential strip (24) with a horizontal or transverse hinge (48). The tabs (40) are pivotable about the horizontal or transverse hinges (48) in opposite directions away from the opening axis to respective folded-out positions, which inhibits the device (20) from folding at the side seams and retains a gaping open configuration of the device (20) and package (60). The vertical hinges (28) include thru cuts or line of perforations that go through the entire material thickness of the circumferential strip (24) and the one or more tabs (40) and extend for a majority of the full axial length of the device (20). The horizontal hinges (48) may be in the form of a living hinge or alternatively thru cuts or a line of perforations.
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公开(公告)号:EP2853376B1
公开(公告)日:2018-09-19
申请号:EP13186016.5
申请日:2013-09-25
CPC分类号: F17C1/02 , B29C53/582 , B29C53/602 , B32B37/142
摘要: A composite material comprises of at least first and second layers, each comprising a polymeric matrix material and wound tows (4, 8) for reinforcement. The tows (4, 8) are wound in opposite directions in each of the first and second layers such that overlapping tows form crossover regions (6, 10). The wound tows (8) in the second layer are arranged such that the crossover regions (10) are formed to be laterally offset from the crossover regions (6) in the first layer.
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公开(公告)号:EP2697038B1
公开(公告)日:2018-09-19
申请号:EP12722758.5
申请日:2012-04-10
CPC分类号: B29C70/32 , B29C53/562 , B29C53/8075 , B29C2053/8025 , B65H18/103 , B65H23/0328 , B65H2557/51 , B65H2701/177
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公开(公告)号:EP3362249A1
公开(公告)日:2018-08-22
申请号:EP16794502.1
申请日:2016-09-28
申请人: OKE Group GmbH
CPC分类号: A47C23/061 , B29C35/02 , B29C48/06 , B29C48/12 , B29C48/154 , B29C48/156 , B29C48/2883 , B29C48/30 , B29C48/34 , B29C48/79 , B29C53/60 , B29C70/521
摘要: The invention relates to an inline method for producing a spring strip profile (1) for a slatted frame, which spring strip profile (1) comprises at least one core strand (2) formed by a fibre-reinforced plastic and at least one thermoplastic cover layer (3) surrounding the core strand (2), wherein the method comprises at least the following steps: joining multiple fibres, threads and/or filaments to form a fibre bundle (2.1); impregnating the fibre bundle (2.1) with a thermally activatable reaction resin; moulding the outer contour of the fibre bundle (2.1) impregnated with the reaction resin; thermally activating the reaction resin (2.1) to form a cured core strand; introducing the core strand (2) into an extruder head (110); applying thermoplastic melt in the extruder head (110) to form the cover layer (3) on the spring strip profile (1); cooling and calibrating the spring strip profile (1) in a cooling and calibrating device (111, 112, 113), wherein, in a winding machine (105), the outer contour of the fibre bundle (2.1) is wrapped around by at least one thread or filament (2.2) supplied laterally in relation to the fibre bundle in at least one position and orientation, and wherein, in a heating section (106), before the core strand (2) is introduced into the extruder head (110), at least a partial curing of the reaction resin is achieved at least in the wrapped outer layer of the fibre bundle (2.1).
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165.
公开(公告)号:EP3356116A1
公开(公告)日:2018-08-08
申请号:EP16806054.9
申请日:2016-12-02
申请人: Robert Bosch GmbH
摘要: A component (1) for a fuel injection system, in particular a high pressure fuel injection system, comprises a main body (2), at least some portions of which are tubular. A tubular portion (5) of the main body (2) has, along a longitudinal axis (7') of the tubular portion (5) that passes perpendicularly through cross sections (8) of the tubular portion (5), a longitudinal bend (6). At the longitudinal bend (6) in the tubular portion (5) the main body (2) is designed so that an ovality (x) of the cross sections (8) of the tubular portion (5) is reduced and/or is less than 8% at the longitudinal bend (6).
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166.
公开(公告)号:EP3352983A1
公开(公告)日:2018-08-01
申请号:EP16849100.9
申请日:2016-09-01
申请人: Innventia AB
CPC分类号: B32B3/28 , B29C53/04 , B29C53/24 , B31D3/002 , B31D3/04 , B31D5/04 , B31D2205/0052 , B65D65/12 , B65D65/406
摘要: A fibre-containing sheet comprising a folding pattern and a partly or fully folded sheet product obtained from the fibre-containing sheet is disclosed. The folding pattern of the fibre-containing sheet comprises a series of parallel straight fold lines and a series of zigzag fold lines. Each zigzag fold line has a breadth which is greater than a breadth of a straight fold line. The partly folded sheet product can be shaped into various complex geometrical shapes, including spheres and saddle points, as a result of the folding pattern. A method for producing the fibre-containing sheet as well as use of the fibre-containing sheet is also disclosed.
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公开(公告)号:EP2949453B1
公开(公告)日:2018-07-11
申请号:EP15169221.7
申请日:2015-05-26
申请人: The Boeing Company
CPC分类号: B29C66/301 , B29C53/04 , B29C53/80 , B29C65/48 , B29C66/02241 , B29C66/03 , B29C70/34 , B29D99/0014 , B29K2105/089 , B29L2009/00 , B29L2031/3076 , B64C2001/0072 , Y02T50/43
摘要: A composite filler (1204) and a method for its manufacture. A composite ply (1239) is folded. The composite ply (1239) comprises fibers arranged at an angle relative to a central axis of the composite ply such that the composite filler (1204) has a varying cross-sectional orientation of fibers. A force is applied to the folded composite ply (1239) after folding to form a desired shape for the composite filler(1204).
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公开(公告)号:EP3090856B1
公开(公告)日:2018-07-04
申请号:EP16168638.1
申请日:2016-05-06
申请人: AVIO S.p.A.
CPC分类号: B29C70/388 , B29C53/66 , B29C53/8016 , F02K9/34 , F05D2230/31 , Y10T156/1788
摘要: In a machine (1) for forming a hollow body (3), for example a casing of a solid propellant engine, a tensioned and guided belt (29) comprising a layer (30) of adhesive material and a protective strip (31) is fed from a deposit head (13), supported by a robot (14) and comprising an unwinding device (27) for unwinding the belt (29), a winding device (35) for winding the strip (31), a first pressing roller (45) for pressing the strip (31) and the layer (30) of adhesive material and rotatable about an axis (47) thereof orthogonal to the feed path (P) of the belt (29) and a second pressing roller (54) for pressing the adhesive material and the strip (31), rotatable about an axis (55) thereof forming an angle other than 90° to the feed path (P) and movable in opposite directions in a direction (65A) transversal to feed path (P).
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公开(公告)号:EP2743066B1
公开(公告)日:2018-06-27
申请号:EP12400056.3
申请日:2012-12-14
发明人: Fink, Axel
CPC分类号: B32B3/12 , B29C53/36 , B29C70/68 , B29D24/005 , B32B5/245 , B32B7/12 , B32B2266/02 , B32B2266/0228 , B32B2266/0235 , B32B2266/0242 , B32B2266/025 , B32B2266/0278 , B32B2266/04 , Y10T29/49904 , Y10T428/24149
摘要: The invention is related to a grid type element (1) of fibre composite structure, comprising a plurality of open polygonal cells (5) made of at least three core segments (16), said open polygonal cells (5) being stringed together alongside said ribs (16) to form a grid structure, and an essentially planar skin sheet (4), said essentially planar skin sheet (4) being attached unilaterally to the grid structure. A multipartite core (6) is provided, said core segments (6a, 6b, 6c) with respectively rectangular cross sections being formed of said multipartite core (6). Said at least three core segments (6a, 6b, 6c) are pivotable interconnected with at least two reduced cross sections (9) between two of said at least three core segments (6a, 6b, 6c) and at least one fibre composite layer (8, 7) is provided with said multipartite core (6), said at least one fibre composite layer (8, 7) sheathing at least partly said multipartite core (6). The invention is as well related to a method of manufacturing such grid type elements.
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170.
公开(公告)号:EP2678535B1
公开(公告)日:2018-06-27
申请号:EP12706542.3
申请日:2012-02-23
申请人: DBW Holding GmbH
IPC分类号: F01N1/24 , F01N13/08 , D04H1/4382 , D04H3/002 , D04H3/015 , D04H3/004 , D04H3/073 , D04H5/08 , B29C53/60 , B29C53/56 , B29C65/56 , B32B37/14
CPC分类号: F01N13/08 , B29C53/564 , B29C65/562 , B32B37/142 , D04H1/4382 , D04H5/08 , F01N1/24 , F01N2310/02 , Y10T442/25
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