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    Repair pressure applicator for in the field damaged aircraft
    2.
    发明授权
    Repair pressure applicator for in the field damaged aircraft 有权
    修理压力施加器在现场受损的飞机

    公开(公告)号：US06318433B1

    公开(公告)日：2001-11-20

    申请号：US09394793

    申请日：1999-09-13

    申请人： Carl A. Reis ,  Nicholas Thomas Castellucci ,  John C. Del Ferraro

    发明人： Carl A. Reis ,  Nicholas Thomas Castellucci ,  John C. Del Ferraro

    IPC分类号： B32B3500

    CPC分类号： B29C73/32 ,  B29C73/12 ,  B30B5/02

    摘要： A pressure application device for applying pressure to a repair patch of a variable contoured aircraft surface, the pressure applicator device is provided with an inflatable pressure bladder. The bladder is configured for applying pressure to the repair patch and is formed of a generally fluid tight elastic material. The pressure applicator device is further provided with at least one variable direction adjustable arm. The arm is disposed in mechanical communication with the bladder for facilitating the application of pressure by the bladder to the repair path upon inflation of the bladder. The bladder is further provided with at least one suction device for providing suction attachment to the aircraft surface. The bladder is attachable to a respective one of the at least one variable direction adjustable arm. The arm facilitates selective attachment of the respective suction device to the variable contoured aircraft surface while maintaining the position of the bladder with respect to the repair path.

    摘要翻译： 一种压力施加装置，用于向可变轮廓的飞行器表面的修补补片施加压力，所述压力施加器装置设置有可膨胀的压力囊。 囊被构造成向修补片施加压力，并且由通常是流体密封的弹性材料形成。 压力施加装置还设置有至少一个可变方向可调臂。 臂与膀胱机械连通地设置，以便于膀胱膨胀时膀胱施加压力至修复路径。 气囊还设置有至少一个用于提供对飞机表面的吸附附件的抽吸装置。 囊状物可附接到所述至少一个可变方向可调臂中的相应一个。 臂有助于将相应的抽吸装置选择性地附接到可变轮廓飞行器表面，同时保持囊相对于修复路径的位置。

    End gaps of filled honeycomb
    3.
    发明授权
    End gaps of filled honeycomb 有权
    填充蜂窝结束间隙

    公开(公告)号：US07575650B1

    公开(公告)日：2009-08-18

    申请号：US11166323

    申请日：2005-06-24

    申请人： Chandrakant Himatlal Shah ,  Tod Palm ,  Timothy Alan Dyer ,  Carl A. Reis

    发明人： Chandrakant Himatlal Shah ,  Tod Palm ,  Timothy Alan Dyer ,  Carl A. Reis

    IPC分类号： B32B37/00

    CPC分类号： B32B3/12 ,  B32B7/12 ,  B32B2305/028 ,  B32B2305/30 ,  E04C2/365 ,  Y10T428/236 ,  Y10T428/24157 ,  Y10T428/249976

    摘要： A sandwich panel includes a honeycomb core of a plurality of cells. A first skin is adhered to a first surface of the honeycomb core with an adhesive. A second skin is adhered to a second surface of the honeycomb core with the adhesive. The plurality of cells extend longitudinally between the first and second skins. The first and second skins adhere to the honeycomb core to form a sandwich panel having a surface area of at least 2.25 square feet. A foam fill is disposed within the cells of the honeycomb core. The foam fill and the honeycomb core define a first gap region proximate to the first skin and a second gap region proximate to the second skin.

    摘要翻译： 夹层板包括多个单元的蜂窝芯。 用粘合剂将第一皮肤附着在蜂窝芯的第一表面上。 用粘合剂将第二皮肤附着在蜂窝芯的第二表面上。 多个单元在第一和第二表皮之间纵向延伸。 第一和第二表皮粘附到蜂窝芯上以形成具有至少2.25平方英尺的表面积的夹芯板。 泡沫填充物设置在蜂窝芯的单元内。 泡沫填充物和蜂窝芯体限定靠近第一皮肤的第一间隙区域和靠近第二皮肤的第二间隙区域。

    END GAPS OF FILLED HONEYCOMB
    4.
    发明申请
    END GAPS OF FILLED HONEYCOMB 有权
    填充蜂窝电话的最终结果

    公开(公告)号：US20090205779A1

    公开(公告)日：2009-08-20

    申请号：US11166323

    申请日：2005-06-24

    申请人： Chandrakant Himatlal Shah ,  Tod Palm ,  Timothy Alan Dyer ,  Carl A. Reis

    发明人： Chandrakant Himatlal Shah ,  Tod Palm ,  Timothy Alan Dyer ,  Carl A. Reis

    IPC分类号： B32B37/14

    CPC分类号： B32B3/12 ,  B32B7/12 ,  B32B2305/028 ,  B32B2305/30 ,  E04C2/365 ,  Y10T428/236 ,  Y10T428/24157 ,  Y10T428/249976

    摘要： A sandwich panel includes a honeycomb core of a plurality of cells. A first skin is adhered to a first surface of the honeycomb core with an adhesive. A second skin is adhered to a second surface of the honeycomb core with the adhesive. The plurality of cells extend longitudinally between the first and second skins. The first and second skins adhere to the honeycomb core to form a sandwich panel having a surface area of at least 2.25 square feet. A foam fill is disposed within the cells of the honeycomb core. The foam fill and the honeycomb core define a first gap region proximate to the first skin and a second gap region proximate to the second skin.

    摘要翻译： 夹层板包括多个单元的蜂窝芯。 用粘合剂将第一皮肤附着在蜂窝芯的第一表面上。 用粘合剂将第二皮肤附着在蜂窝芯的第二表面上。 多个单元在第一和第二表皮之间纵向延伸。 第一和第二表皮粘附到蜂窝芯上以形成具有至少2.25平方英尺的表面积的夹芯板。 泡沫填充物设置在蜂窝芯的单元内。 泡沫填充物和蜂窝芯体限定靠近第一皮肤的第一间隙区域和靠近第二皮肤的第二间隙区域。

    Environmentally sound and safe apparatus for removing coatings
    5.
    发明授权
    Environmentally sound and safe apparatus for removing coatings 失效
    环保，安全的去除涂层的设备

    公开(公告)号：US5575035A

    公开(公告)日：1996-11-19

    申请号：US590798

    申请日：1996-01-24

    申请人： Carl A. Reis ,  Nicholas T. Castellucci ,  Richard A. Osterman

    发明人： Carl A. Reis ,  Nicholas T. Castellucci ,  Richard A. Osterman

    IPC分类号： A47L13/02 ,  B44D3/16 ,  A47L9/06

    CPC分类号： A47L13/02 ,  B44D3/164 ,  B44D3/168

    摘要： The present invention is a hand held tool for removing coatings from a substrate. The hand held tool includes a housing having a front section with an outlet, a mid section with an inlet, and a rear section, a heat source disposed within the front section of the housing for emitting heat through the outlet, and a vacuum source disposed within the mid section of the housing for providing suction through the inlet. The hand held coating remover further includes a power source disposed within the rear section for supplying power to the heat source and the vacuum source, a control panel having a heat controller for adjusting and controlling the heat emitted from the heat source through the outlet and a vacuum controller for adjusting and controlling the suction provided by the vacuum through the inlet, and a blade located adjacent to the inlet and resiliently coupled to the housing. The coating is safely removed from the substrate by first heating the coating, moving the blade across the heated coating to scape the coating, and vacuuming the coating as it is scraped or removed from the substrate. Also, any fumes that are created when the coating is heated is easily removed by the vacuum.

    摘要翻译： 本发明是用于从基材去除涂层的手持工具。 手持工具包括具有出口的前部的壳体，具有入口的中间部分和后部部分，设置在壳体的前部中的热源，用于通过出口发射热量，以及设置真空源 在壳体的中间部分内，用于通过入口提供吸力。 手持涂布去除器还包括设置在后部中用于向热源和真空源供电的电源，控制面板，具有用于调节和控制通过出口从热源发出的热量的热控制器，以及 用于调节和控制由真空通过入口提供的抽吸的真空控制器，以及与入口相邻并且弹性地联接到壳体的叶片。 通过首先加热涂层，将刀片移动穿过加热的涂层以对涂层进行涂层，并将涂层从基材刮下或从基材上除去时对涂层进行真空抽吸，从而将涂层安全地从基材上除去。 此外，当涂层被加热时产生的任何烟雾容易被真空除去。

    Drying tool for honeycomb core
    7.
    发明授权
    Drying tool for honeycomb core 失效
    蜂窝芯干燥机

    公开(公告)号：US06665949B1

    公开(公告)日：2003-12-23

    申请号：US09911990

    申请日：2001-07-24

    申请人： Carl A. Reis ,  Doris Andren Reis

    发明人： Carl A. Reis ,  Doris Andren Reis

    IPC分类号： F26B1900

    CPC分类号： F26B21/006 ,  F26B21/004

    摘要： A drying tool for drying moisture present in cells of a honeycomb core. The tool includes an inflatable bladder compartment having a bendable exterior surface and a plurality of open-ended nozzles protruding from this exterior surface, with each nozzle having a passage in fluid communication with the bladder compartment. A connector element is connectible with a hot air source for delivering hot air into the bladder compartment for subsequent dispatch through the plurality of nozzles. Preferably, the nozzles are situated in a grid formation and are of a generally conical configuration. In use, the bendable exterior surface with the protruding nozzles is bowed or curved to generally configure to the exterior shape of the honeycomb core such that hot air is pinpointed in a grid pattern to drive heated air into the core and thereby cause circulation through the core cells for moisture evaporation.

    摘要翻译： 用于干燥存在于蜂窝芯的单元中的水分的干燥工具。 该工具包括具有可弯曲外表面的可充气囊室，以及从该外表面突出的多个开口喷嘴，每个喷嘴具有与膀胱隔室流体连通的通道。 连接器元件可与热空气源连接，用于将热空气输送到气囊室中，以便随后通过多个喷嘴进行分配。 优选地，喷嘴位于格栅形状中，并且具有大致圆锥形的构造。 在使用中，具有突出喷嘴的可弯曲外表面是弯曲或弯曲的，以大致配置为蜂窝芯的外部形状，使得热空气被精确地定位成网格图案，以将加热的空气驱动到芯中，从而引起循环通过芯 水分蒸发的细胞。

    Repair pressure applicator for in the field damaged aircraft
    8.
    发明授权
    Repair pressure applicator for in the field damaged aircraft 失效
    修理压力施加器在现场受损的飞机

    公开(公告)号：US5975183A

    公开(公告)日：1999-11-02

    申请号：US46484

    申请日：1998-03-23

    申请人： Carl A. Reis ,  Nicholas Thomas Castellucci ,  John C. Del Ferraro

    发明人： Carl A. Reis ,  Nicholas Thomas Castellucci ,  John C. Del Ferraro

    IPC分类号： B29C73/12 ,  B29C73/32 ,  B30B5/02

    CPC分类号： B29C73/32 ,  B29C73/12 ,  B30B5/02

    摘要： A pressure applicator device for applying pressure to a repair patch of a variable contoured aircraft surface, the pressure applicator device is provided with an inflatable pressure bladder. The bladder is configured for applying pressure to the repair patch and is formed of a generally fluid tight elastic material. The pressure applicator device is further provided with at least one variable direction adjustable arm. The arm is disposed in mechanical communication with the bladder for facilitating the application of pressure by the bladder to the repair patch upon inflation of the bladder. The bladder is further provided with at least one suction device for providing suction attachment to the aircraft surface. The bladder is attachable to a respective one of the at least one variable direction adjustable arm. The arm facilitates selective attachment of the respective suction device to the variable contoured aircraft surface while maintaining the position of the bladder with respect to the repair patch.

    摘要翻译： 一种用于向可变轮廓飞行器表面的修补补片施加压力的压力施加器装置，压力施加器装置设置有可膨胀的压力囊。 囊被构造成向修补片施加压力，并且由通常是流体密封的弹性材料形成。 压力施加装置还设置有至少一个可变方向可调臂。 臂被设置成与膀胱机械连通，以便于膀胱膨胀时由膀胱施加压力至修补片。 气囊还设置有至少一个用于提供对飞机表面的吸附附件的抽吸装置。 囊状物可附接到所述至少一个可变方向可调臂中的相应一个。 臂有助于将相应的抽吸装置选择性地附接到可变轮廓飞行器表面，同时保持膀胱相对于修补补片的位置。