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    Method and apparatus for automated location marking
    1.
    发明授权
    Method and apparatus for automated location marking 有权
    自动定位标记的方法和装置

    公开(公告)号：US06824628B2

    公开(公告)日：2004-11-30

    申请号：US10797693

    申请日：2004-03-09

    Applicant: Donald A. Anderson ,  Brice A. Johnson ,  James B. Andersen

    Inventor： Donald A. Anderson ,  Brice A. Johnson ,  James B. Andersen

    IPC: B05B110

    CPC classification number: B29C70/541 ,  B29C70/382

    Abstract: A compliant marking tool for attachment to a fiber placement machine that is capable of marking detail locations on a work piece positioned on the fiber placement machine. The marking tool has a flexible member that is configured and adapted to bow and twist in response to the marking tool contacting the work piece. A holder is pivotably connected to the flexible member. A marking member is positioned in the holder and is capable of moving within the holder. The flexing of the flexible member along with the pivoting of the holder and the movement of the marking member allow the marking tool to follow the contours of the work piece and mark detail locations without damaging or at least minimizing the potential of damaging the work piece.

    Abstract translation: 一种用于连接到光纤贴片机的兼容标记工具，其能够标记位于纤维铺放机上的工件上的细节位置。 标记工具具有柔性构件，其被构造和适于响应于标记工具接触工件而弯曲和扭曲。 保持器可枢转地连接到柔性构件。 标记部件定位在支架内并且能够在支架内移动。 柔性构件的弯曲以及保持器的枢转和标记构件的移动允许标记工具跟随工件的轮廓并标记细节位置，而不损害或至少最小化损坏工件的可能性。

    Method and apparatus for automated location marking
    2.
    发明授权
    Method and apparatus for automated location marking 有权

    公开(公告)号：US06736180B2

    公开(公告)日：2004-05-18

    申请号：US10012609

    申请日：2001-10-30

    Applicant: Donald A. Anderson ,  Brice A. Johnson ,  James B. Andersen

    Inventor： Donald A. Anderson ,  Brice A. Johnson ,  James B. Andersen

    IPC: B05B110

    CPC classification number: B29C70/541 ,  B29C70/382

    Abstract: A compliant marking tool for attachment to a fiber placement machine that is capable of marking detail locations on a work piece positioned on the fiber placement machine. The marking tool has a flexible member that is configured and adapted to bow and twist in response to the marking tool contacting the work piece. A holder is pivotably connected to the flexible member. A marking member is positioned in the holder and is capable of moving within the holder. The flexing of the flexible member along with the pivoting of the holder and the movement of the marking member allow the marking tool to follow the contours of the work piece and mark detail locations without damaging or at least minimizing the potential of damaging the work piece.

    Method of making composite panels for a fuselage
    3.
    发明授权
    Method of making composite panels for a fuselage 有权
    制作机身复合板的方法

    公开(公告)号：US07935289B2

    公开(公告)日：2011-05-03

    申请号：US11695561

    申请日：2007-04-02

    Applicant: Donald A. Anderson ,  Brice A. Johnson ,  Stephen S. Spoon

    Inventor： Donald A. Anderson ,  Brice A. Johnson ,  Stephen S. Spoon

    IPC: B32B37/00

    CPC classification number: B29C70/543 ,  B29C33/68 ,  B29C37/0003 ,  B29C53/60 ,  B29C53/68 ,  B29C70/30 ,  B29C70/446 ,  Y02T50/43 ,  Y10T29/49867 ,  Y10T29/49879 ,  Y10T29/49895 ,  Y10T29/49998

    Abstract: A method is provided for making a composite laminate aircraft skin for a fuselage in multiple composite panels. A resin-impregnated composite tape is placed on a lay-up surface of a mandrel tool to form the composite laminate aircraft skin as a barrel that is substantially the shape of a fuselage section. The barrel is cut into a plurality of panels on the mandrel tool, and at least one panel of the plurality of panels is transferred, individually and independently of all other of the plurality of panels, from the lay-up surface of the mandrel tool to a first cure tool of a plurality of cure tools having an aero surface tooled to an outer mold line. The at least one of the panels is cured on the first cure tool to form a cured composite panel. The first cure tool defines and controls the outer mold line of the at least one panel. The cured composite panel is removed from the first cure tool.

    Abstract translation: 提供了一种用于制造用于多个复合板中的机身的复合层压飞机皮肤的方法。 将树脂浸渍的复合带放置在心轴工具的叠置表面上，以形成基本上为机身部分形状的复合层压飞机皮肤。 将筒体切割成心轴工具上的多个面板，并且多个面板中的至少一个面板独立地且独立于多个面板中的所有其他面板从芯棒工具的叠置表面传递到 多个固化工具的第一固化工具，其具有加工到外模线的航空表面。 所述至少一个所述面板在所述第一固化工具上固化以形成固化的复合板。 第一固化工具定义和控制至少一个面板的外模线。 固化的复合板从第一固化工具移除。

    Method of transferring large uncured composite laminates
    4.
    发明授权
    Method of transferring large uncured composite laminates 有权
    转移大型未固化复合层压板的方法

    公开(公告)号：US07228611B2

    公开(公告)日：2007-06-12

    申请号：US10717030

    申请日：2003-11-18

    Applicant: Donald A. Anderson ,  Brice A. Johnson ,  Stephen S. Spoon

    Inventor： Donald A. Anderson ,  Brice A. Johnson ,  Stephen S. Spoon

    IPC: B23P11/02 ,  B29C65/00 ,  B64C1/00

    CPC classification number: B29C70/543 ,  B29C33/68 ,  B29C37/0003 ,  B29C53/60 ,  B29C53/68 ,  B29C70/30 ,  B29C70/446 ,  Y02T50/43 ,  Y10T29/49867 ,  Y10T29/49879 ,  Y10T29/49895 ,  Y10T29/49998

    Abstract: A method of transferring an uncured composite laminate skin from a lay-up surface of a male mandrel tool to a female cure tool includes defining multiple vacuum zones on the lay-up surface, each zone corresponding to one of a multiple of portions into which the skin is to be separated. For example, to separate the skin into two portions, a low profile seal of a first membrane to the lay-up surface is formed at a first vacuum zone and a second low profile seal for a second membrane is formed at a second vacuum zone. The method further includes laying up a composite laminate skin over all the vacuum zones; separating the composite laminate skin into portions, for example, a first portion over the first vacuum zone and a second portion over the second vacuum zone; and releasing the portions individually into cure tools having an outside mold line surface.

    Abstract translation: 将未固化的复合层合物表皮从阳性心轴工具的铺叠表面转移到阴性固化工具的方法包括在铺设表面上限定多个真空区，每个区对应于多个部分中的一个， 皮肤是分开的。 例如，为了将皮肤分成两部分，在第一真空区域形成第一膜至叠层表面的低轮廓密封，并且在第二真空区域形成用于第二膜的第二低轮廓密封。 该方法还包括在所有真空区域上铺设复合层压体皮肤; 将复合层压板表皮分离成例如第一真空区上的第一部分和第二真空区上的第二部分; 并且将这些部分单独地释放到具有外部模具线表面的固化工具中。

    CASSETTE APPARATUS AND PROCESS
    6.
    发明申请
    CASSETTE APPARATUS AND PROCESS 有权
    CASSETTE设备和过程

    公开(公告)号：US20080290208A1

    公开(公告)日：2008-11-27

    申请号：US11829536

    申请日：2007-07-27

    Applicant: Donald A. Anderson ,  Gary E. Pfitzner ,  Ronald E. Anderson

    Inventor： Donald A. Anderson ,  Gary E. Pfitzner ,  Ronald E. Anderson

    IPC: B65H35/00

    CPC classification number: B65H18/103 ,  B65H2301/5111 ,  B65H2301/5151 ,  B65H2301/5152 ,  B65H2301/543 ,  B65H2701/377 ,  Y10T156/1052 ,  Y10T156/108 ,  Y10T156/1174 ,  Y10T156/1195 ,  Y10T156/12 ,  Y10T156/195 ,  Y10T156/1956 ,  Y10T156/1978 ,  Y10T156/1983 ,  Y10T156/1994

    Abstract: In one embodiment, an apparatus is provided for preparing a cassette spool. The apparatus includes: a supply reel for supplying and unrolling tape material on original backing paper; at least one cutting member for cutting unrolled tape material while on original backing paper; a cutting surface defined in a plane; a pivoting path member adapted to move from a first position aligned in the plane to a second position aligned at least partially out of the plane; at least one removing member for removing uncut unrolled tape material from original backing paper; and a cassette spool for rolling up unrolled cut tape material on original backing paper. In further embodiments, methods are provided for preparing a cassette spool with cut tape material on original backing paper.

    Abstract translation: 在一个实施例中，提供了一种用于准备盒式卷轴的装置。 该设备包括：用于在原始背纸上提供和展开胶带材料的供带盘; 至少一个用于在原始背纸上切割展开的带材的切割构件; 在平面中限定的切割表面; 枢转路径构件，其适于从在所述平面中对准的第一位置移动到至少部分地离开所述平面的第二位置; 至少一个去除构件，用于从原始背衬纸去除未切割的未卷曲的带材料; 以及用于在原始背纸上卷起展开的切割胶带材料的盒式卷轴。 在另外的实施例中，提供了用于在原始背衬纸上制备具有切割带材料的盒式卷轴的方法。

    Convolutely lined and wrapped composite tubes
    8.
    发明授权
    Convolutely lined and wrapped composite tubes 失效
    缠绕式复合管

    公开(公告)号：US5077106A

    公开(公告)日：1991-12-31

    申请号：US416650

    申请日：1989-10-03

    Applicant: Harry W. Dursch ,  Donald A. Anderson ,  Robert F. Collins

    Inventor： Harry W. Dursch ,  Donald A. Anderson ,  Robert F. Collins

    IPC: B29C31/00 ,  B29C53/42 ,  B29C63/00 ,  B29C63/14 ,  B29C63/30 ,  B29C65/78 ,  F16L57/06

    CPC classification number: B29C31/002 ,  B29C53/42 ,  B29C63/0047 ,  B29C63/14 ,  B29C63/30 ,  B29C65/78 ,  B29C66/4322 ,  B29C66/45 ,  B29C66/49 ,  B29C66/71 ,  B29C66/7212 ,  B29C66/7394 ,  F16L57/06 ,  Y10T428/1359

    Abstract: Methods are provided for lining and wrapping both interior and exterior surfaces of tubular structures with materials that protect the underlying structures from adverse environmental conditions, provide a thermal control coating and prevent exchanging moisture with the surrounding environments. The methods use adhesives to securely position the lining or wrapping material inside or around the exterior of the tubular structure. The adhesives prevent the formation of discontinuities in the protective layer provided by the lining or wrapping material by holding the protective materials in place during the fabrication process. The wrapping materials are sealed by an ultrasonically welded seam to prevent environmental attack through the seam to the underlying tubular structure.

    Abstract translation: 提供了用于将管状结构的内表面和外表面衬里和包裹的材料与保护下面的结构免受恶劣环境条件的材料，提供热控制涂层并防止与周围环境交换湿气的方法。 该方法使用粘合剂将衬里或包裹材料牢固地定位在管状结构的外部或周围。 粘合剂通过在制造过程中将保护材料保持在适当位置，防止在由衬里或包裹材料提供的保护层中形成不连续性。 包裹材料通过超声波焊缝密封，以防止通过接缝到下面的管状结构的环境侵蚀。

    Golf club head
    9.
    发明授权
    Golf club head 失效
    高尔夫球杆头

    公开(公告)号：US5024437A

    公开(公告)日：1991-06-18

    申请号：US492973

    申请日：1990-03-13

    Applicant: Donald A. Anderson

    Inventor： Donald A. Anderson

    IPC: A63B53/04 ,  C22C9/00 ,  C22C14/00 ,  C22C25/00

    CPC classification number: A63B53/04 ,  A63B53/0466 ,  A63B53/047 ,  A63B2053/0416 ,  A63B2053/0458

    Abstract: A golf club head has a main body portion formed by investment casting of material such as stainless steel, beryllium copper, titanium, or aluminum. The face plate of the head is formed of a forged metal such as forged carbon steel, this plate being welded to the face portion of the casting to form an integral assembly therewith. The forged metal faceplate affords a more solid impact and feel to the club which provides better control.

    Abstract translation: 高尔夫球杆头具有通过不锈钢，铍铜，钛或铝等材料的熔模铸造而形成的主体部。 头部的面板由诸如锻造碳钢的锻造金属形成，该板被焊接到铸件的面部以形成与其一体的组件。 锻造的金属面板为俱乐部提供了更加坚实的冲击和感觉，从而提供更好的控制。

    Convolutely lined and wrapped composite tubes
    10.
    发明授权
    Convolutely lined and wrapped composite tubes 失效
    缠绕式复合管

    公开(公告)号：US4900383A

    公开(公告)日：1990-02-13

    申请号：US183680

    申请日：1988-04-19

    Applicant: Harry W. Dursch ,  Donald A. Anderson ,  Robert F. Collins

    Inventor： Harry W. Dursch ,  Donald A. Anderson ,  Robert F. Collins

    IPC: B29C31/00 ,  B29C53/42 ,  B29C63/00 ,  B29C63/14 ,  B29C63/30 ,  B29C65/78 ,  F16L57/06

    CPC classification number: F16L57/06 ,  B29C31/002 ,  B29C53/42 ,  B29C63/0047 ,  B29C63/14 ,  B29C63/30 ,  B29C65/78 ,  B29C66/4322 ,  B29C66/49 ,  B29C66/71 ,  B29C66/7212 ,  B29C66/7394 ,  Y10S138/10 ,  Y10T156/1038 ,  Y10T428/1359

    Abstract: Methods are provided for lining and wrapping both interior and exterior surfaces of tubular structures with materials that protect the underlying structures from adverse environmental conditions, provide a thermal control coating and prevent exchanging moisture with the surrounding environments. The methods use adhesives to securely position the lining or wrapping material inside or around the exterior of the tubular structure. The adhesives prevent the formation of discontinuities in the protective layer provided by the lining or wrapping material by holding the protective materials in place during the fabrication process. The wrapping materials are sealed by an ultrasonically welded seam to prevent environmental attack through the seam to the underlying tubular structure.

    Abstract translation: 提供了用于将管状结构的内表面和外表面衬里和包裹的材料与保护下面的结构免受恶劣环境条件的材料，提供热控制涂层并防止与周围环境交换湿气的方法。 该方法使用粘合剂将衬里或包裹材料牢固地定位在管状结构的外部或周围。 粘合剂通过在制造过程中将保护材料保持在适当位置，防止在由衬里或包裹材料提供的保护层中形成不连续性。 包裹材料通过超声波焊缝密封，以防止通过接缝到下面的管状结构的环境侵蚀。

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