公开(公告)号：US09610756B2

公开(公告)日：2017-04-04

申请号：US13776560

申请日：2013-02-25

申请人： Larry J. Ashton ,  Craig B. Simpson ,  Rex W. Kay ,  Troy L. White ,  Mike Glen Allman

发明人： Larry J. Ashton ,  Craig B. Simpson ,  Rex W. Kay ,  Troy L. White ,  Mike Glen Allman

IPC分类号： B32B37/00 ,  B29C37/00 ,  B29C70/20 ,  B29C70/32 ,  B29C70/44 ,  B29C70/54 ,  B64C3/20 ,  D04H3/04 ,  D04H3/07 ,  D04H3/12 ,  B29C53/58 ,  B29C53/66 ,  B29C53/80 ,  B29L31/30

CPC分类号： B32B37/0038 ,  B29C37/0064 ,  B29C53/582 ,  B29C53/66 ,  B29C53/8016 ,  B29C53/8066 ,  B29C70/202 ,  B29C70/32 ,  B29C70/44 ,  B29C70/443 ,  B29C70/543 ,  B29C70/546 ,  B29L2031/3085 ,  B64C3/20 ,  D04H3/04 ,  D04H3/07 ,  D04H3/12 ,  Y02T50/43 ,  Y10T428/24116 ,  Y10T428/24994

摘要： A composite material made of multiple filament bands is disclosed. The filament bands are wound to create a composite material. The filament bands may be impregnated with a solid or semi-solid resin. The filament bands are wound in multiple orientations to form a sheet of composite material. Additionally, the composite material may be made to have a varying number of layer and fiber orientations throughout the sheet of composite material. In another embodiment, a composite component requiring multiple layers and fiber orientations may be substantially manufactured during a filament winding process.

公开(公告)号：US07445744B2

公开(公告)日：2008-11-04

申请号：US10726970

申请日：2003-12-03

申请人： Craig B. Simpson ,  Mike Glen Allman ,  Steven Taylor Tuttle ,  Larry J. Ashton

发明人： Craig B. Simpson ,  Mike Glen Allman ,  Steven Taylor Tuttle ,  Larry J. Ashton

IPC分类号： B29C44/16

CPC分类号： B64C3/20 ,  B29C37/0064 ,  B29C53/8016 ,  B29C53/8066 ,  B29C70/44 ,  B29C70/443 ,  B29C70/543 ,  B29C70/546 ,  B29L2031/3085 ,  B64C3/24 ,  Y02T50/43 ,  Y10S264/904

摘要： A single piece co-cured composite wing is disclosed. The wing has a flying surface and structural members. In one embodiment the structural members may be a plurality of spars. The spars may have various shapes to increase the buckling strength. The spars may be wave shaped, such as a sinusoidal shape. The flying surface and the structural members are co-cured in order to form a single piece, integral wing structure. A process for manufacturing a single piece co-cured wing is also disclosed. The process may include laying out composite sheets for the flying surface of the wing. Then, the composite material of the spars is arranged around a plurality of pressurizable forms. Finally, the composite material is cured in a clamshell frame.

摘要翻译： 公开了单件共固化复合翼。 机翼有飞行表面和结构构件。 在一个实施例中，结构构件可以是多个翼梁。 翼梁可以具有各种形状以增加屈曲强度。 翼梁可以是波形，例如正弦形状。 飞行表面和结构构件共同固化以形成单件，整体翼结构。 还公开了用于制造单件共固化翼的方法。 该方法可以包括为翼的飞行表面布置复合片材。 然后，翼片的复合材料围绕多个可加压的形式布置。 最后，复合材料在蛤壳框架中固化。

公开(公告)号：US07124797B2

公开(公告)日：2006-10-24

申请号：US10086685

申请日：2002-03-04

申请人： Alan H. Anderson ,  Mike Glen Allman ,  Larry Jed Ashton ,  Craig Bjarnson Simpson ,  Benko Samasoni Ta'ala ,  Troy Larry White

发明人： Alan H. Anderson ,  Mike Glen Allman ,  Larry Jed Ashton ,  Craig Bjarnson Simpson ,  Benko Samasoni Ta'ala ,  Troy Larry White

IPC分类号： B65H81/00 ,  B29C53/00

CPC分类号： B29C70/32 ,  B29C53/665 ,  B29C53/8016 ,  B29C53/8041 ,  B29C53/8066 ,  B29C70/382 ,  B29C70/384 ,  B29C70/545 ,  B29L2031/3082

摘要： The present invention relates to apparatus and methods for winding filament to create a structure. In one embodiment, the invention includes the application of filament to a rotating mandrel to create a desired shape. The invention includes the filament winding of both simple and complex shapes.

公开(公告)号：US07748424B2

公开(公告)日：2010-07-06

申请号：US11508870

申请日：2006-08-24

申请人： Alan H. Anderson ,  Mike Glen Allman ,  Larry Jed Ashton ,  Craig Bjamson Simpson ,  Benko Samasoni Ta'ala ,  Troy Larry White

发明人： Alan H. Anderson ,  Mike Glen Allman ,  Larry Jed Ashton ,  Craig Bjamson Simpson ,  Benko Samasoni Ta'ala ,  Troy Larry White

IPC分类号： B65H81/00 ,  B29C53/00

CPC分类号： B29C70/32 ,  B29C53/665 ,  B29C53/8016 ,  B29C53/8041 ,  B29C53/8066 ,  B29C70/382 ,  B29C70/384 ,  B29C70/545 ,  B29L2031/3082

摘要： The present invention relates to apparatus and methods for winding filament to create a structure. In one embodiment, the invention includes the application of filament to a rotating mandrel to create a desired shape. The invention includes the filament winding of both simple and complex shapes.

摘要翻译： 本发明涉及用于缠绕丝以产生结构的装置和方法。 在一个实施例中，本发明包括将丝应用于旋转心轴以产生期望的形状。 本发明包括简单和复杂形状的细丝缠绕。

公开(公告)号：US20130164491A1

公开(公告)日：2013-06-27

申请号：US13776560

申请日：2013-02-25

申请人： Larry J. Ashton ,  Craig B. Simpson ,  Rex W. Kay ,  Troy L. White ,  Mike Glen Allman

发明人： Larry J. Ashton ,  Craig B. Simpson ,  Rex W. Kay ,  Troy L. White ,  Mike Glen Allman

IPC分类号： B32B37/00

CPC分类号： B32B37/0038 ,  B29C37/0064 ,  B29C53/582 ,  B29C53/66 ,  B29C53/8016 ,  B29C53/8066 ,  B29C70/202 ,  B29C70/32 ,  B29C70/44 ,  B29C70/443 ,  B29C70/543 ,  B29C70/546 ,  B29L2031/3085 ,  B64C3/20 ,  D04H3/04 ,  D04H3/07 ,  D04H3/12 ,  Y02T50/43 ,  Y10T428/24116 ,  Y10T428/24994

摘要： A composite material made of multiple filament bands is disclosed. The filament bands are wound to create a composite material. The filament bands may be impregnated with a solid or semi-solid resin. The filament bands are wound in multiple orientations to form a sheet of composite material. Additionally, the composite material may be made to have a varying number of layer and fiber orientations throughout the sheet of composite material. In another embodiment, a composite component requiring multiple layers and fiber orientations may be substantially manufactured during a filament winding process.

摘要翻译： 公开了一种由多根丝带制成的复合材料。 缠绕丝带以产生复合材料。 丝带可以用固体或半固体树脂浸渍。 丝束带以多个取向缠绕以形成复合材料片。 另外，复合材料可以制成在整个复合材料片材上具有不同数量的层和纤维取向。 在另一个实施例中，可以在丝缠绕过程中基本上制造需要多层和纤维取向的复合部件。

公开(公告)号：US06889937B2

公开(公告)日：2005-05-10

申请号：US10175722

申请日：2002-06-20

申请人： Craig B. Simpson ,  Mike Glen Allman ,  Steven Taylor Tuttle ,  Larry J. Ashton

发明人： Craig B. Simpson ,  Mike Glen Allman ,  Steven Taylor Tuttle ,  Larry J. Ashton

IPC分类号： B29C37/00 ,  B29C53/80 ,  B29C70/44 ,  B29C70/54 ,  B64C3/20 ,  B64C3/24 ,  B64C1/00

CPC分类号： B64C3/20 ,  B29C37/0064 ,  B29C53/8016 ,  B29C53/8066 ,  B29C70/44 ,  B29C70/443 ,  B29C70/543 ,  B29C70/546 ,  B29L2031/3085 ,  B64C3/24 ,  Y02T50/43 ,  Y10S264/904

摘要： A single piece co-cured composite wing is disclosed. The wing has a flying surface and structural members. In one embodiment the structural members may be a plurality of spars. The spars may have various shapes to increase the buckling strength. The spars may be wave shaped, such as a sinusoidal shape. The flying surface and the structural members are co-cured in order to form a single piece, integral wing structure. A process for manufacturing a single piece co-cured wing is also disclosed. The process may include laying out composite sheets for the flying surface of the wing. Then, the composite material of the spars is arranged around a plurality of pressurizable forms. Finally, the composite material is cured in a clamshell frame.

摘要翻译： 公开了单件共固化复合翼。 机翼有飞行表面和结构构件。 在一个实施例中，结构构件可以是多个翼梁。 翼梁可以具有各种形状以增加屈曲强度。 翼梁可以是波形，例如正弦形状。 飞行表面和结构构件共同固化以形成单件，整体翼结构。 还公开了用于制造单件共固化翼的方法。 该方法可以包括为机翼的飞行表面布置复合片材。 然后，翼片的复合材料围绕多个可加压的形式布置。 最后，复合材料在蛤壳框架中固化。