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1.发明申请公开(公告)号：US20210031395A1
公开(公告)日：2021-02-04
申请号：US17075273
申请日：2020-10-20
申请人： The Boeing Company
IPC分类号： B26D1/14 , B26D1/25 , B26D1/46 , B26D3/16 , B26D5/00 , B29C48/00 , B29C48/02 , B29C48/25 , B29C64/118 , B29C64/165 , B29C64/209 , B29C69/00 , B29C70/16 , B29C70/30 , B29C70/38 , B29C70/54 , B33Y10/00 , B33Y30/00 , B33Y40/00 , B33Y50/02 , B33Y70/00 , B26D1/143
摘要： Methods, apparatus, and systems for cutting material used in fused deposition modeling systems are provided, which comprise a ribbon including one or more perforations. Material is passed through at least one perforation and movement of the ribbon cuts the material. A further embodiment comprises a disk including one or more blade structures, each forming at least one cavity. Material is passed through at least one cavity and a rotational movement of the disk cuts the material. A further embodiment comprises a slider-crank mechanism including a slider coupled to a set of parallel rails of a guide shaft. The slider moves along a length of the rails to cut the material. Yet another embodiment comprises one or more rotatable blade structures coupled to at least one rod. The rotation of the blade structures causes the blade structures to intersect and cut extruded material during each rotation.
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2.发明授权公开(公告)号：US11529748B2
公开(公告)日：2022-12-20
申请号：US17075273
申请日：2020-10-20
申请人： The Boeing Company
IPC分类号： B29C64/118 , B26D1/14 , B29C48/00 , B29C70/38 , B29C70/54 , B26D1/143 , B26D1/46 , B33Y40/00 , B29C64/165 , B29C48/02 , B29C48/25 , B29C64/209 , B29C48/05 , B33Y10/00 , B33Y30/00 , B33Y50/02 , B33Y70/00 , B26D1/25 , B26D3/16 , B26D5/00 , B29C69/00 , B29C70/16 , B29C70/30 , B26D1/00 , B29C48/345 , B29C48/04 , B29C48/30 , B22D11/01 , B29K71/00 , B29K105/00 , B29K105/10 , B29K307/04
摘要： Methods, apparatus, and systems for cutting material used in fused deposition modeling systems are provided, which comprise a ribbon including one or more perforations. Material is passed through at least one perforation and movement of the ribbon cuts the material. A further embodiment comprises a disk including one or more blade structures, each forming at least one cavity. Material is passed through at least one cavity and a rotational movement of the disk cuts the material. A further embodiment comprises a slider-crank mechanism including a slider coupled to a set of parallel rails of a guide shaft. The slider moves along a length of the rails to cut the material. Yet another embodiment comprises one or more rotatable blade structures coupled to at least one rod. The rotation of the blade structures causes the blade structures to intersect and cut extruded material during each rotation.
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3.发明授权公开(公告)号：US10150262B2
公开(公告)日：2018-12-11
申请号：US14948057
申请日：2015-11-20
申请人： The Boeing Company
IPC分类号： B29C47/00 , B29C70/30 , B33Y10/00 , B33Y30/00 , B33Y50/02 , B33Y70/00 , B26D1/14 , B26D1/25 , B26D3/16 , B26D5/00 , B29C69/00 , B29C70/16 , B29C70/38 , B29C70/54 , B26D1/143 , B26D1/46 , B33Y40/00 , B29C64/106 , B29C64/165 , B29C64/20 , B29C64/386 , B22D11/01 , B29K71/00 , B29K105/00 , B29K105/10 , B29K307/04 , B26D1/00
摘要： Methods, apparatus, and systems for cutting material used in fused deposition modeling systems are provided, which comprise a ribbon including one or more perforations. Material is passed through at least one perforation and movement of the ribbon cuts the material. A further embodiment comprises a disk including one or more blade structures, each forming at least one cavity. Material is passed through at least one cavity and a rotational movement of the disk cuts the material. A further embodiment comprises a slider-crank mechanism including a slider coupled to a set of parallel rails of a guide shaft. The slider moves along a length of the rails to cut the material. Yet another embodiment comprises one or more rotatable blade structures coupled to at least one rod. The rotation of the blade structures causes the blade structures to intersect and cut extruded material during each rotation.
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4.发明授权公开(公告)号：US10814511B2
公开(公告)日：2020-10-27
申请号：US16215419
申请日：2018-12-10
申请人： The Boeing Company
IPC分类号： B29C64/209 , B26D1/14 , B29C48/00 , B29C70/38 , B29C70/54 , B26D1/143 , B26D1/46 , B33Y40/00 , B29C64/165 , B29C48/02 , B29C48/25 , B29C64/118 , B33Y10/00 , B33Y30/00 , B33Y50/02 , B33Y70/00 , B26D1/25 , B26D3/16 , B26D5/00 , B29C69/00 , B29C70/16 , B29C70/30 , B26D1/00 , B29C48/30 , B29C48/345 , B22D11/01 , B29K71/00 , B29K105/00 , B29K105/10 , B29K307/04
摘要： Methods, apparatus, and systems for cutting material used in fused deposition modeling systems are provided, which comprise a ribbon including one or more perforations. Material is passed through at least one perforation and movement of the ribbon cuts the material. A further embodiment comprises a disk including one or more blade structures, each forming at least one cavity. Material is passed through at least one cavity and a rotational movement of the disk cuts the material. A further embodiment comprises a slider-crank mechanism including a slider coupled to a set of parallel rails of a guide shaft. The slider moves along a length of the rails to cut the material. Yet another embodiment comprises one or more rotatable blade structures coupled to at least one rod. The rotation of the blade structures causes the blade structures to intersect and cut extruded material during each rotation.
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5.发明申请公开(公告)号：US20190105854A1
公开(公告)日：2019-04-11
申请号：US16215419
申请日：2018-12-10
申请人： The Boeing Company
IPC分类号： B29C70/30 , B29C64/386 , B29C64/165 , B29C64/106 , B33Y40/00 , B29C64/20 , B29C70/16 , B29C69/00 , B26D5/00 , B26D3/16 , B26D1/25 , B26D1/14 , B33Y10/00 , B26D1/46 , B26D1/143 , B29C70/54 , B29C70/38 , B33Y30/00 , B33Y50/02 , B33Y70/00
摘要： Methods, apparatus, and systems for cutting material used in fused deposition modeling systems are provided, which comprise a ribbon including one or more perforations. Material is passed through at least one perforation and movement of the ribbon cuts the material. A further embodiment comprises a disk including one or more blade structures, each forming at least one cavity. Material is passed through at least one cavity and a rotational movement of the disk cuts the material. A further embodiment comprises a slider-crank mechanism including a slider coupled to a set of parallel rails of a guide shaft. The slider moves along a length of the rails to cut the material. Yet another embodiment comprises one or more rotatable blade structures coupled to at least one rod. The rotation of the blade structures causes the blade structures to intersect and cut extruded material during each rotation.
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6.发明申请公开(公告)号：US20170144375A1
公开(公告)日：2017-05-25
申请号：US14948057
申请日：2015-11-20
申请人： The Boeing Company
IPC分类号： B29C67/00 , B26D3/16 , B26D1/14 , B26D1/25 , B29C70/30 , B33Y50/02 , B29C69/00 , B33Y10/00 , B33Y70/00 , B29C70/16 , B26D5/00 , B33Y30/00
CPC分类号： B29C70/30 , B22D11/01 , B26D1/14 , B26D1/143 , B26D1/25 , B26D1/46 , B26D3/16 , B26D5/005 , B26D2001/006 , B29C47/0002 , B29C47/0066 , B29C47/0866 , B29C47/12 , B29C47/30 , B29C64/106 , B29C64/165 , B29C64/20 , B29C64/386 , B29C69/001 , B29C70/16 , B29C70/382 , B29C70/545 , B29K2071/00 , B29K2105/0067 , B29K2105/10 , B29K2307/04 , B33Y10/00 , B33Y30/00 , B33Y40/00 , B33Y50/02 , B33Y70/00
摘要： Methods, apparatus, and systems for cutting material used in fused deposition modeling systems are provided, which comprise a ribbon including one or more perforations. Material is passed through at least one perforation and movement of the ribbon cuts the material. A further embodiment comprises a disk including one or more blade structures, each forming at least one cavity. Material is passed through at least one cavity and a rotational movement of the disk cuts the material. A further embodiment comprises a slider-crank mechanism including a slider coupled to a set of parallel rails of a guide shaft. The slider moves along a length of the rails to cut the material. Yet another embodiment comprises one or more rotatable blade structures coupled to at least one rod. The rotation of the blade structures causes the blade structures to intersect and cut extruded material during each rotation.
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7.发明申请UNITIZED ASSEMBLY INCLUDING SUBSTRUCTURE ELEMENT INTEGRAL WITH FIBER METAL LAMINATE 有权独特的组件，其中包括与光纤金属层压板结合的元件公开(公告)号：US20140220372A1
公开(公告)日：2014-08-07
申请号：US14172721
申请日：2014-02-04
申请人： The Boeing Company
发明人： David P. Heck , Loren J. Strahm
CPC分类号： B64C1/12 , B23K20/12 , B23K2101/001 , B29C65/06 , B32B3/08 , B32B3/30 , B32B5/22 , B32B5/26 , B32B7/02 , B32B7/12 , B32B15/043 , B32B15/14 , B32B15/20 , B32B2262/101 , B32B2262/106 , B32B2307/30 , B32B2307/50 , B32B2307/558 , B32B2307/718 , B32B2605/00 , B64C2001/0072 , Y10T428/12347 , Y10T428/12375 , Y10T428/1241 , Y10T428/12444 , Y10T428/31678
摘要： A unitized assembly may comprise a fiber metal laminate and at least one additive layer. The fiber metal laminate may have non-metallic plies bonded to metallic plies and may include an innermost metallic ply. The at least one additive layer may be deposited onto the innermost metallic ply by friction stir welding.
摘要翻译： 组合组件可以包括纤维金属层压体和至少一个添加剂层。 纤维金属层压板可以具有非金属层粘合到金属层，并且可以包括最内层的金属层。 可以通过摩擦搅拌焊接将至少一个添加剂层沉积到最内层的金属层上。
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公开(公告)号：US10201940B2
公开(公告)日：2019-02-12
申请号：US14939336
申请日：2015-11-12
申请人： The Boeing Company
IPC分类号： B29C67/00 , G05B19/4099 , B33Y50/02 , G06F17/50
摘要： A computer implemented apparatus and method for receiving tool paths that a dispensing head follows to deposit roads of material for successively building object layers of a 3D object during an additive manufacturing process, generating simulated object layers of a simulated 3D object from the tool paths, wherein the simulated object layers represent an interior geometry of each one of the object layers, determining a contact surface area between adjacent ones of the simulated object layers, and determining a predicted mechanical property of the 3D object from the contact surface area and a material property of the material.
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9.发明申请公开(公告)号：US20170136703A1
公开(公告)日：2017-05-18
申请号：US14939336
申请日：2015-11-12
申请人： The Boeing Company
IPC分类号： B29C67/00 , G05B19/4099
CPC分类号： B29C67/0088 , B29C64/386 , B33Y50/00 , B33Y50/02 , G05B19/4099 , G05B2219/35134 , G05B2219/49007 , G06F17/5009 , G06F2217/12
摘要： A computer implemented apparatus and method for receiving tool paths that a dispensing head follows to deposit roads of material for successively building object layers of a 3D object during an additive manufacturing process, generating simulated object layers of a simulated 3D object from the tool paths, wherein the simulated object layers represent an interior geometry of each one of the object layers, determining a contact surface area between adjacent ones of the simulated object layers, and determining a predicted mechanical property of the 3D object from the contact surface area and a material property of the material.
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10.发明授权Unitized assembly including substructure element integral with fiber metal laminate 有权单元组件，包括与纤维金属层压板成一体的子结构元件公开(公告)号：US09027820B2
公开(公告)日：2015-05-12
申请号：US14172721
申请日：2014-02-04
申请人： The Boeing Company
发明人： David P. Heck , Loren J. Strahm
CPC分类号： B64C1/12 , B23K20/12 , B23K2101/001 , B29C65/06 , B32B3/08 , B32B3/30 , B32B5/22 , B32B5/26 , B32B7/02 , B32B7/12 , B32B15/043 , B32B15/14 , B32B15/20 , B32B2262/101 , B32B2262/106 , B32B2307/30 , B32B2307/50 , B32B2307/558 , B32B2307/718 , B32B2605/00 , B64C2001/0072 , Y10T428/12347 , Y10T428/12375 , Y10T428/1241 , Y10T428/12444 , Y10T428/31678
摘要： A unitized assembly may comprise a fiber metal laminate and at least one additive layer. The fiber metal laminate may have non-metallic plies bonded to metallic plies and may include an innermost metallic ply. The at least one additive layer may be deposited onto the innermost metallic ply by friction stir welding.
摘要翻译： 组合组件可以包括纤维金属层压体和至少一个添加剂层。 纤维金属层压板可以具有非金属层粘合到金属层，并且可以包括最内层的金属层。 可以通过摩擦搅拌焊接将至少一个添加剂层沉积到最内层的金属层上。
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