IMPROVED TROUGH REFLECTORS FOR SOLAR ENERGY COLLECTORS
    1.
    发明申请
    IMPROVED TROUGH REFLECTORS FOR SOLAR ENERGY COLLECTORS 审中-公开
    改善太阳能收集器的彻底反射器

    公开(公告)号:WO2007087680A1

    公开(公告)日:2007-08-09

    申请号:PCT/AU2007/000095

    申请日:2007-02-02

    Inventor: JOHNSTON, Glen

    Abstract: A trough reflector for solar energy collection is constructed from transverse ribs (10) which support a reflective surface (12). Side edge support rails (20), which are mounted on the ends of the ribs, support the linear edges (14) of the reflective surface. The edge support rails (20) have a channel-like construction with an inner flange member (22) which is in contact with the top of the reflective surface, and a lip member (24) extending from an outer flange member (23). The edge region of the reflective surface (12) rests on the lip member (24) with the edge (14) of the reflective surface in contact with the outer flange member (23). Tightening the bolts (30) which secure the edge support rails (20) to the ends of the ribs (10) applies a turning moment to the edge regions of the reflective surface, to ensure that the entire reflective surface is parabolic. The preferred construction of the trough reflector uses flexible, resilient ribs (10) which initially have an arcuate profile. The arcuate profile is converted into a parabolic profile by the application of a force to the ends of the ribs. A respective chordal strap (34) is used to hold each rib in its parabolic profile. The trough reflector is preferably mounted on rotatable hoop members (42, 43) to form a solar energy concentrator. Rotation of the hoop members is effected by a combination of pinch bearings (57) and pinch rollers (50), which are driven by a motor (56). Preferably, a microprocessor is used to control of the activation of the motor.

    Abstract translation: 用于太阳能收集的槽反射器由支撑反射表面(12)的横肋(10)构成。 安装在肋的端部上的侧边缘支撑轨道(20)支撑反射表面的直线边缘(14)。 边缘支撑轨道(20)具有通道状结构,其具有与反射表面的顶部接触的内部凸缘构件(22)和从外部凸缘构件(23)延伸的唇形构件(24)。 反射表面(12)的边缘区域位于唇形构件(24)上,反射表面的边缘(14)与外凸缘构件(23)接触。 将固定边缘支撑轨道(20)的螺栓(30)紧固到肋(10)的端部时,向反射表面的边缘区域施加转动力矩,以确保整个反射表面是抛物线的。 槽反射器的优选结构使用柔性弹性肋(10),其最初具有弧形轮廓。 通过向肋的端部施加力将弓形轮廓转换成抛物线轮廓。 相应的弦带(34)用于将每个肋保持在其抛物线轮廓中。 槽反射器优选地安装在可转动的环形构件(42,43)上以形成太阳能集中器。 箍构件的旋转通过由电动机(56)驱动的夹紧轴承(57)和夹送辊(50)的组合来实现。 优选地,微处理器用于控制电动机的启动。

    AIRCRAT WING BOX AND MANUFACTURE THEREOF
    2.
    发明申请
    AIRCRAT WING BOX AND MANUFACTURE THEREOF 审中-公开
    AIRCRAT WING BOX及其制造商

    公开(公告)号:WO2008012569A3

    公开(公告)日:2009-03-12

    申请号:PCT/GB2007050416

    申请日:2007-07-19

    Inventor: CRAWFORD TRISTAN

    CPC classification number: B64C3/187 B64F5/10 Y10T29/49883

    Abstract: An aircraft wing box comprises a pair of half ribs (18, 20) joined to form a rib extending from an upper wing skin (12) to a lower wing skin (10). Each half rib (18) comprises a base (19) and a plurality of projections (4) that extend away from the base (19), the projections (4) defining a series of troughs (2a) and peaks (4a). Respective projections of one half rib (18) overlap with respective projections of the other half rib (20) thereby defining overlapping portions (3), the half ribs (18, 20) being joined in the regions of the overlapping portions (3). There may be projections (4) shaped such that the overlapping portion (3b) defined by the two projections is separated from the neutral axis N of the rib (18, 20). The half ribs may be joined in the regions of the overlapping portions (3) by means of a fixing arrangement (7) that enables the position of joining of the half ribs to be adapted during initial assembly of the half-ribs (18, 20) to accommodate relative movement of the half ribs in a direction substantially parallel to the plane of one of the half ribs. The half ribs (18, 20) may be formed by deforming extruded metal sections. During assembly, in-wing systems (32) may be inserted before joining two wing-box halves.

    Abstract translation: 飞机机翼盒包括一对半肋条(18,20),所述一对半肋条(18,20)被连接以形成从上机翼皮肤(12)向下机翼皮肤(10)延伸的肋条。 每个半肋(18)包括基部(19)和远离基部(19)延伸的多个突起(4),凸起(4)限定一系列槽(2a)和峰(4a)。 一半肋(18)的相应突起与另一半肋(20)的相应突起重叠,由此限定重叠部分(3),半重肋(18,20)在重叠部分(3)的区域中被连接。 可以有凸起(4)成形为使得由两个突起限定的重叠部分(3b)与肋(18,20)的中性轴线N分离。 半肋可以通过固定装置(7)连接在重叠部分(3)的区域中,所述固定装置使得能够在半肋(18,20)的初始组装期间适配半肋的接合位置 )以适应半肋的基本上平行于半肋中的一个的平面的方向的相对运动。 半肋(18,20)可以通过使挤压的金属部变形而形成。 在组装期间,可以在连接两个翼盒半部之前插入机翼系统(32)。

    A PROCESS FOR MANUFACTURING A CAN WITH A POLYGONAL CROSS SECTION AND A CAN WITH A POLYGONAL CROSS SECTION
    3.
    发明申请
    A PROCESS FOR MANUFACTURING A CAN WITH A POLYGONAL CROSS SECTION AND A CAN WITH A POLYGONAL CROSS SECTION 审中-公开
    具有多边形交叉部分的CAN制造方法和具有多边形横截面的CAN

    公开(公告)号:WO99051373A1

    公开(公告)日:1999-10-14

    申请号:PCT/BR1999/000023

    申请日:1999-03-30

    Abstract: A process for manufacturing a can with a polygonal cross section and a can with a polygonal cross section, the process comprising the steps of: milling the cylindrical lateral wall of a tubular body (10), providing said wall with a plurality of circumferential ribs (20), which are continuous and axially spaced from each other and defined by a certain degree of radial plastic deformation of the respective circumferential region of the cylindrical lateral wall of the tubular body (10); expanding the formed tubular body (10), deforming it, in order to define longitudinal edges (12) in whose region the circumferential ribs (20) are eliminated; and double-seaming a bottom and an upper wall of the can to the tubular body (10). This process defines a can having any polygonal cross section and circumferential ribs (20) on the lateral wall thereof, between the longitudinal edges (12).

    Abstract translation: 一种用于制造具有多边形横截面的罐和具有多边形横截面的罐的方法,所述方法包括以下步骤:铣削管状体(10)的圆柱形侧壁,为所述壁提供多个周向肋( 20),其彼此连续并且轴向间隔开并且由管状体(10)的圆柱形侧壁的相应周向区域的一定程度的径向塑性变形限定; 使形成的管状体(10)膨胀,使其变形,以限定在其区域中消除周向肋(20)的纵向边缘(12); 并且将所述罐的底壁和上壁双重缝合到所述管状体(10)。 该过程在纵向边缘(12)之间限定了具有任何多边形横截面的罐和在其侧壁上的周向肋(20)。

    PARABOLIC TROUGH SOLAR REFLECTOR WITH AN INDEPENDENTLY SUPPORTED COLLECTOR TUBE
    4.
    发明申请
    PARABOLIC TROUGH SOLAR REFLECTOR WITH AN INDEPENDENTLY SUPPORTED COLLECTOR TUBE 审中-公开
    具有独立支撑收集器管的抛物面太阳能反射器

    公开(公告)号:WO2010033721A3

    公开(公告)日:2010-06-03

    申请号:PCT/US2009057343

    申请日:2009-09-17

    Applicant: JENNINGS KEVIN

    Inventor: JENNINGS KEVIN

    Abstract: A parabolic trough solar collector system has a parabolic reflector used with an independently supported collector tube. The parabolic reflector has a reflective surface formed on a reflective surface support structure, supported by a circular support beam. This assembly rests on a plurality of support and drive rollers supported by a roller support arm, supported by a roller support column. The parabolic reflector assembly rotates against the rollers along a single axis to maintain a focus line of the parabolic reflector surface at the same location as the center of the circle described by the outer edge of the circular support beam. Located at this same focus line is the independently supported collector tube not attached to the parabolic trough reflector. The collector tube is supported on pipe roller hangers, which in turn are supported by a wire catenary system connected to support towers which straddle the parabolic reflector.

    Abstract translation: 抛物面槽式太阳能收集器系统具有与独立支撑的收集器管一起使用的抛物面反射器。 抛物面反射器具有形成在由圆形支撑梁支撑的反射表面支撑结构上的反射表面。 该组件搁置在由辊支撑臂支撑的多个支撑和驱动辊上,辊支撑臂由辊支撑柱支撑。 抛物面反射器组件沿着单个轴逆着辊旋转以将抛物面反射器表面的聚焦线保持在与由圆形支撑梁的外边缘描述的圆的中心相同的位置处。 位于这个相同的焦点线上的是独立支撑的收集器管,其不连接到抛物面槽式反射器。 收集器管道支撑在管道滚筒吊架上,而后者又通过连接到跨越抛物面反射器的支撑塔架的线架系统支撑。

    PARABOLIC TROUGH SOLAR REFLECTOR WITH AN INDEPENDENTLY SUPPORTED COLLECTOR TUBE
    6.
    发明申请
    PARABOLIC TROUGH SOLAR REFLECTOR WITH AN INDEPENDENTLY SUPPORTED COLLECTOR TUBE 审中-公开
    具有独立支撑的收集管的PARABOLIC TROUGH太阳能反射器

    公开(公告)号:WO2010033721A2

    公开(公告)日:2010-03-25

    申请号:PCT/US2009/057343

    申请日:2009-09-17

    Inventor: JENNINGS, Kevin

    Abstract: A parabolic trough solar collector system has a parabolic reflector used with an independently supported collector tube. The parabolic reflector has a reflective surface formed on a reflective surface support structure, supported by a circular support beam. This assembly rests on a plurality of support and drive rollers supported by a roller support arm, supported by a roller support column. The parabolic reflector assembly rotates against the rollers along a single axis to maintain a focus line of the parabolic reflector surface at the same location as the center of the circle described by the outer edge of the circular support beam. Located at this same focus line is the independently supported collector tube not attached to the parabolic trough reflector. The collector tube is supported on pipe roller hangers, which in turn are supported by a wire catenary system connected to support towers which straddle the parabolic reflector.

    Abstract translation: 抛物槽太阳能收集器系统具有与独立支撑的收集管一起使用的抛物面反射器。 抛物面反射器具有形成在由圆形支撑梁支撑的反射表面支撑结构上的反射表面。 该组件由多个由辊支撑臂支撑的支撑和驱动辊支撑,所述支撑和驱动辊由辊支撑柱支撑。 抛物面反射器组件沿着单个轴线旋转抵靠辊子,以将抛物面反射器表面的焦点线保持在与由圆形支撑梁的外边缘描述的圆的中心相同的位置。 位于同一焦点线上的是独立支撑的收集器管,其未连接到抛物面的反射器。 收集管被支撑在管道滚筒悬挂器上,管道悬挂器又由连接到跨过抛物面反射器的支撑塔的连线系统支撑。

    KOLBEN FÜR EINE KOLBEN-ZYLINDER-ANORDNUNG UND HERSTELLUNGSVERFAHREN
    7.
    发明申请
    KOLBEN FÜR EINE KOLBEN-ZYLINDER-ANORDNUNG UND HERSTELLUNGSVERFAHREN 审中-公开
    活塞,活塞气缸组件和方法

    公开(公告)号:WO2009015710A1

    公开(公告)日:2009-02-05

    申请号:PCT/EP2008/003127

    申请日:2008-04-18

    Abstract: Die Erfindung betrifft einen Kolben (10) für eine Kolben-Zylinder-Anordnung, insbesondere einen Stoβdämpferkolben, mit: einem Kolbenkörper (11), der eine Umfangsfläche (13) aufweist; einer Dichtmanschette (12), die eine äuβere Umfangsflache (15), eine innere Umfangsfläche (16), eine erste Randfläche (17) und eine erste Dichtlippe (19) aufweist und die um die Umfangsfläche (13) des Kolbenkörpers herum verläuft und in axialer Richtung wenigstens einen Teil der Umfangsflache bedeckt, wobei: die erste Randfläche an einem ersten Ende der Dichtmanschette die beiden Umfangsflächen miteinander verbindet; die erste Dichtlippe durch die erste Randfläche und die äuβere Umfangsfläche begrenzt wird; und die erste Dichtlippe in Umfangsrichtung gleichformig ausgebildet ist.

    Abstract translation: 本发明涉及一种活塞(10),用于活塞 - 气缸装置,特别是减振器活塞包括:活塞体(11)具有外周表面(13); 具有具有外圆周表面(15)的密封套筒(12),内周边表面(16),第一边缘面(17)和一个第一密封唇(19)和围绕所述活塞体的外周表面(13)的轴向延伸的左右 至少圆周面的一部分的方向被覆盖,其特征在于:在所述密封套筒的第一端连接所述第一边缘表面,两个周面彼此接合; 第一密封唇由第一边缘表面和外周表面界定; 和第一密封唇被形成在圆周方向上gleichformig。

    METHODS OF FORMING POLARIZED PANES FOR VARIABLE TRANSMISSION WINDOWS
    8.
    发明申请
    METHODS OF FORMING POLARIZED PANES FOR VARIABLE TRANSMISSION WINDOWS 审中-公开
    形成用于可变传输窗口的极化平板的方法

    公开(公告)号:WO2015013157A1

    公开(公告)日:2015-01-29

    申请号:PCT/US2014/047351

    申请日:2014-07-21

    Abstract: Methods of forming polarized panes for variable transmission windows are disclosed. The polarized panes are formed from transparent substrates that are brushed with a brushing pattern that varies continuously in a select direction over each of one or more periods. A layer of polarizable material such as POLARCOAT material can be deposited on and responds to the brushed surface by forming a polarization pattern that substantially matches the brushing pattern and thus also includes one or more periods.

    Abstract translation: 公开了用于形成可变透光窗的偏振窗的方法。 偏光板由透明衬底形成,该衬底通过在一个或多个周期中的每个周期上以选择方向连续变化的刷涂图案进行刷洗。 可以通过形成基本上与刷洗图案相匹配的偏振图案,并且因此还包括一个或多个周期,可以在诸如POLARCOAT材料的层之间沉积并对其进行响应。

    AIRCRAT WING BOX AND MANUFACTURE THEREOF
    10.
    发明申请
    AIRCRAT WING BOX AND MANUFACTURE THEREOF 审中-公开
    AIRCRAT WING BOX及其制造商

    公开(公告)号:WO2008012569A2

    公开(公告)日:2008-01-31

    申请号:PCT/GB2007/050416

    申请日:2007-07-19

    CPC classification number: B64C3/187 B64F5/10 Y10T29/49883

    Abstract: An aircraft wing box comprises a pair of half ribs (18, 20) joined to form a rib extending from an upper wing skin (12) to a lower wing skin (10). Each half rib (18) comprises a base (19) and a plurality of projections (4) that extend away from the base (19), the projections (4) defining a series of troughs (2a) and peaks (4a). Respective projections of one half rib (18) overlap with respective projections of the other half rib (20) thereby defining overlapping portions (3), the half ribs (18, 20) being joined in the regions of the overlapping portions (3). There may be projections (4) shaped such that the overlapping portion (3b) defined by the two projections is separated from the neutral axis N of the rib (18, 20). The half ribs may be joined in the regions of the overlapping portions (3) by means of a fixing arrangement (7) that enables the position of joining of the half ribs to be adapted during initial assembly of the half-ribs (18, 20) to accommodate relative movement of the half ribs in a direction substantially parallel to the plane of one of the half ribs. The half ribs (18, 20) may be formed by deforming extruded metal sections. During assembly, in-wing systems (32) may be inserted before joining two wing-box halves.

    Abstract translation: 飞机机翼盒包括一对半肋条(18,20),它们连接成形成从上机翼皮肤(12)延伸到下机翼皮肤(10)的肋条。 每个半肋(18)包括基部(19)和远离基部(19)延伸的多个突起(4),所述突起(4)限定一系列槽(2a)和峰(4a)。 一半肋(18)的相应突起与另一半肋(20)的相应突起重叠,从而限定重叠部分(3),半重肋(18,20)在重叠部分(3)的区域中被连接。 可以有凸起(4)成形为使得由两个突起限定的重叠部分(3b)与肋(18,20)的中性轴线N分离。 半肋条可以通过固定装置(7)连接在重叠部分(3)的区域中,固定装置(7)能够使半肋条的连接位置在半肋条(18,20)的初始组装期间适应 ),以适应半肋的基本平行于半肋之一的平面的方向的相对运动。 半肋(18,20)可以通过使挤出的金属部变形而形成。 在组装期间,可以在连接两个翼盒半部之前插入机翼系统(32)。

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