公开(公告)号：US20150217599A1

公开(公告)日：2015-08-06

申请号：US14613736

申请日：2015-02-04

申请人： Craig M. Zehnder ,  Greg Peer ,  James Burg ,  Stephen Leonard ,  Henry Sklyut ,  John Cobes ,  Anton Rovito ,  Gabriele Ciccola ,  Kelly Weiler ,  Michael Kulak ,  James Black ,  Glenn Jarvis ,  Wilson Lee ,  Grant DeGeorge

发明人： Craig M. Zehnder ,  Greg Peer ,  James Burg ,  Stephen Leonard ,  Henry Sklyut ,  John Cobes ,  Anton Rovito ,  Gabriele Ciccola ,  Kelly Weiler ,  Michael Kulak ,  James Black ,  Glenn Jarvis ,  Wilson Lee ,  Grant DeGeorge

IPC分类号： B60B25/12 ,  B60B23/08

CPC分类号： B60B25/12 ,  B60B3/02 ,  B60B11/02 ,  B60B25/18 ,  B60B25/20 ,  B60B2360/104

摘要： A wheel for a pneumatic tire has a rim with one monolithic bead seat and a removable beat seat. The removable bead seat has two halves that embrace the rim and engage a groove to retain the tire. The removable bead seat may have a second lip either monolithically formed or as a part of a separate retainer that bolts to the bead seat. The wheel may be made from aluminum alloy.

摘要翻译： 用于充气轮胎的车轮具有带有一个整体式胎圈座和可拆卸节拍座的轮辋。 可拆卸的胎圈座具有包围轮辋的两个半部，并与槽啮合以保持轮胎。 可拆卸的胎圈座可以具有一个第一唇形或者一个单独的保持器的一部分，该保持器螺栓连接到胎圈座上。 车轮可以由铝合金制成。

公开(公告)号：US20100043939A1

公开(公告)日：2010-02-25

申请号：US12299708

申请日：2007-05-15

申请人： Markus B. Heinimann ,  Michael Kulak ,  Edmund W. Chu ,  John T. Siemon

发明人： Markus B. Heinimann ,  Michael Kulak ,  Edmund W. Chu ,  John T. Siemon

IPC分类号： B32B37/00

CPC分类号： B32B37/1018 ,  B32B2305/08 ,  B32B2311/00 ,  B32B2605/18 ,  Y10T156/10

摘要： The present invention discloses a method for producing a wing structure comprising producing a machined metallic bottom skin by pre-machinmg, preforming or combinations thereof, finishing the skin which serves as a mold, placing a plurality of straps on top of the skin, arranging a monolithic, fiber metal laminate, or non-reinforced metallic laminate skin on top of the plurality of straps to form a module, and curing the module, wherein the bottom skin is the load carrying element in the wing The present invention also discloses a method for producing a wing structure comprising providing a mold, placing a first monolithic, fiber metal laminate, or non-reinforced metallic laminate skin on a lay-up mold, placing a plurality of straps on top of the skin, arranging a second monolithic, fiber metal laminate, or non-reinforced metallic laminate skin on top of the plurality of straps to form a module, and curing the module.

摘要翻译： 本发明公开了一种翼型结构的制造方法，其特征在于，包括通过预先加工，预成型或组合来制造加工后的金属底层皮肤，整理作为模具的皮肤，将多个皮带放置在皮肤的顶部， 整体式，纤维金属层压体或非强化金属层压板表层，以形成模块，并固化模块，其中底层皮肤是机翼中的承载元件本发明还公开了一种用于 制造机翼结构，包括提供模具，将第一整体，纤维金属层压板或非增强金属层压板表层放置在铺层模具上，将多个带放置在皮肤的顶部上，布置第二整体的纤维金属 层压体或非增强金属层压板表层，以形成模块，并固化模块。

公开(公告)号：US20070128463A1

公开(公告)日：2007-06-07

申请号：US11558265

申请日：2006-11-09

申请人： Gwendolyn Dixon ,  Robert Pahl ,  Michael Kulak ,  Markus Heinimann ,  Brandon Bodily

发明人： Gwendolyn Dixon ,  Robert Pahl ,  Michael Kulak ,  Markus Heinimann ,  Brandon Bodily

IPC分类号： C22F1/04 ,  B32B15/20

CPC分类号： B21C23/22 ,  B21C23/08 ,  B21C33/004 ,  B23K26/32 ,  B23K31/12 ,  B23K2103/10 ,  B32B15/016 ,  C22F1/04 ,  Y10T428/12764

摘要： The present invention provides a structural member of a multi-alloy monolithic extrusion comprising a first aluminum alloy and a second aluminum alloy; wherein the first aluminum alloy is metallurgically fused to the second aluminum alloy. In another aspect of the present invention, an extrusion method is provided including the steps of providing a first billet and at least a second billet; machining the first billet to form a first substantially flat surface; machining the second billet to form a second flat surface; positioning the first flat surface of the first billet adjacent to the second flat surface of the second billet; welding at least a portion of the first billet to the second billet to form a third billet; and extruding the third billet to form a monolithic multi-alloy structural member.

摘要翻译： 本发明提供了包括第一铝合金和第二铝合金的多合金整体式挤压件的结构件; 其中所述第一铝合金与所述第二铝合金冶金熔合。 在本发明的另一方面，提供挤压方法，包括提供第一坯料和至少第二坯料的步骤; 加工第一坯料以形成第一基本平坦的表面; 加工第二坯料以形成第二平坦表面; 将第一坯料的第一平坦表面邻近第二坯料的第二平坦表面定位; 将第一坯料的至少一部分焊接到第二坯料以形成第三坯料; 并挤出第三坯料以形成整体式多合金结构构件。

公开(公告)号：US20090211697A1

公开(公告)日：2009-08-27

申请号：US11749027

申请日：2007-05-15

申请人： Markus B. Heinimann ,  Michael Kulak ,  Edmund W. Chu ,  John T. Siemon

发明人： Markus B. Heinimann ,  Michael Kulak ,  Edmund W. Chu ,  John T. Siemon

IPC分类号： B29C65/00

CPC分类号： B64C3/26 ,  B29K2105/06 ,  B29K2305/00 ,  Y10T156/1028

摘要： The present invention discloses a method for producing an aircraft wing hybrid structure comprising the steps of producing a machined metallic bottom skin by either (i) pre-machining, (ii) preforming or (iii) combinations thereof, finishing the machined metallic bottom skin, providing a finished machined metallic bottom skin that serves as a lay-up mold, placing a plurality of core straps on top of the finished machined metallic bottom skin, arranging a skin that is selected from the group consisting of a monolithic skin, a fiber metal laminate skin and a non-reinforced metallic laminate skin on top of the plurality of cores strap to form a module, and curing the module, wherein the finished machined metallic bottom skin is the load carrying element in the aircraft wing hybrid structure. In another embodiment, the present invention discloses a method for producing an aircraft wing hybrid structure comprising the steps of providing a lay-up mold, placing a first skin that is selected from the group consisting of a monolithic skin, a fiber metal laminate skin and a non-reinforced metallic laminate skin on a lay-up mold, placing a plurality of core straps on top of the skin, arranging a second skin that is selected from the group consisting of a monolithic skin, a fiber metal laminate skin and a non-reinforced metallic laminate skin on top of the plurality of cores strap to form a module, and curing the module.

摘要翻译： 本发明公开了一种用于制造飞机机翼混合结构的方法，包括以下步骤：（i）预加工，（ii）预成型或（iii）其组合，完成机加工金属底皮， 提供用作叠层模具的成品加工的金属底部皮肤，将多个芯带放置在成品加工的金属底部皮肤的顶部上，布置从由单片皮，纤维金属 层叠皮肤和非强化金属层压皮肤，以形成模块，并固化模块，其中成品加工的金属底部皮肤是飞机机翼混合结构中的承载元件。 在另一个实施方案中，本发明公开了一种用于生产飞机机翼混合结构的方法，包括以下步骤：提供铺层模具，放置选自下列组的第一皮肤：整体式皮肤，纤维金属层压体皮肤和 在叠层模具上的非增强金属层压体皮肤，将多个芯皮带放置在皮肤的顶部上，布置第二皮肤，所述第二皮肤选自单片皮肤，纤维金属层压体皮肤和非皮肤组织 - 在多个芯带的顶部上加强金属层压体表层以形成模块，并固化模块。