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公开(公告)号：US09610608B2
公开(公告)日：2017-04-04
申请号：US13860291
申请日：2013-04-10
Applicant: UT Battelle, LLC
Inventor： Minghu Pan , Miguel Fuentes-Cabrera , Petro Maksymovych , Bobby G. Sumpter , Qing Li
Abstract: The embodiments disclosed herein include all-electron control over a chemical attachment and the subsequent self-assembly of an organic molecule into a well-ordered three-dimensional monolayer on a metal surface. The ordering or assembly of the organic molecule may be through electron excitation. Hot-electron and hot-hole excitation enables tethering of the organic molecule to a metal substrate, such as an alkyne group to a gold surface. All-electron reactions may allow a direct control over the size and shape of the self-assembly, defect structures and the reverse process of molecular disassembly from single molecular level to mesoscopic scale.
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公开(公告)号：US20170090284A1
公开(公告)日：2017-03-30
申请号：US15375773
申请日：2016-12-12
Applicant: APPLIED MATERIALS, INC.
Inventor： ROBERT L. HUBBARD , IFTIKHAR AHMAD
CPC classification number: G03F7/0387 , B05D3/029 , B05D3/06 , B05D2505/50 , C08J7/123 , C08J2379/04 , C08J2379/08 , G03F7/16 , G03F7/20 , G03F7/26 , G03F7/38 , G03F7/40 , H01L21/02118 , H01L21/02337 , H01L21/311
Abstract: A method for curing photosensitive polyimide (PSPI) films includes the steps of: depositing a PSPI film on a selected substrate, and curing the film by microwave heating at a selected temperature from about 200 to 340° C. in a selected atmosphere containing an oxygen concentration from about 20 to 200,000 ppm. The process atmosphere may be static or flowing. The addition of oxygen improves the removal of acrylate residue and improves the Tg of the cured film, while the low processing temperature characteristic of the microwave process prevents the oxygen from damaging the polyimide backbone. The method may further include the steps of photopatterning and developing the PSPI film prior to curing. The process is particularly suitable for dielectric films on silicon for electronic applications.
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公开(公告)号：US20170080457A1
公开(公告)日：2017-03-23
申请号：US15267990
申请日：2016-09-16
Inventor： Joël EYMERY , Amine EL KACIMI , Olivier DELLEA , Emmanuelle PAULIAC-VAUJOUR
CPC classification number: B05D3/12 , B05D1/005 , B05D1/60 , B05D3/0254 , B05D3/06 , B05D3/107 , B82B3/0066 , B82Y40/00 , C01B32/00 , C01B32/05 , C01B32/15 , C01B32/158 , H01L21/02115 , H01L21/02118 , H01L21/02376
Abstract: A method for orienting elongated objects arranged on the surface of a substrate, the elongated objects extending according to an initial orientation, the method including depositing on the surface of the substrate at least one layer of a soft material covering at least partially a portion of the elongated objects, and applying a mechanical stress on at least one portion of the layer of soft material in such a way as to modify the orientation of at least one portion of the elongated objects.
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44.发明授权Components with micro cooled patterned coating layer and methods of manufacture 有权具有微冷却图案化涂层的组件和制造方法公开(公告)号：US09562436B2
公开(公告)日：2017-02-07
申请号：US13663989
申请日：2012-10-30
Applicant: General Electric Company
Inventor： Ronald Scott Bunker , Scott Andrew Weaver
IPC: F01D5/14 , F01D5/18 , F01D5/28 , B05D1/02 , B05D1/32 , C23C4/18 , C23C14/58 , C23C14/04 , C23C24/04 , B05D3/06 , B05D7/00
CPC classification number: F01D5/18 , B05D1/02 , B05D3/06 , B05D7/50 , C23C4/01 , C23C4/073 , C23C4/18 , C23C14/042 , C23C14/5886 , C23C24/04 , F01D5/286 , F01D5/288 , Y02T50/672 , Y02T50/676 , Y10T428/13
Abstract: A manufacturing method includes providing a substrate with an outer surface and at least one interior space, selectively deposited a coating on a portion of the substrate to form a selectively deposited coating having one or more grooves formed therein. The method further includes processing at least a portion of the surface of the selectively deposited coating to plastically deform the selectively deposited coating in the vicinity of the top of a respective groove. An additional coating is applied over at least a portion of the surface of the selectively deposited coating. A component is disclosed and includes a substrate, a selectively deposited coating disposed on at least a portion of the substrate, and defining one or more grooves therein, and an additional coating disposed over the selectively deposited coating. The substrate, the selectively deposited coating and the additional coating defining one or more channels for cooling the component.
Abstract translation: 一种制造方法包括提供具有外表面和至少一个内部空间的基底，在基底的一部分上选择性地沉积涂层以形成其中形成有一个或多个凹槽的选择性沉积的涂层。 该方法还包括处理选择性沉积涂层的表面的至少一部分，使相应凹槽顶部附近的选择性沉积涂层塑性变形。 在选择性沉积的涂层的至少一部分表面上施加另外的涂层。 公开了一种组件，并且包括基板，设置在基板的至少一部分上的选择性沉积的涂层，并且在其中限定一个或多个凹槽，以及设置在选择性沉积的涂层上的附加涂层。 衬底，选择性沉积的涂层和附加涂层限定用于冷却部件的一个或多个通道。
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公开(公告)号：US20170028640A1
公开(公告)日：2017-02-02
申请号：US15087882
申请日：2016-03-31
Applicant: The Boeing Company
Inventor： Samuel F. Harrison , Faraón Torres , Ryan G. Ziegler , Nick S. Evans , Ciro J. Grijalva, III , Hayden S. Osborn
CPC classification number: B33Y70/00 , B05D1/265 , B05D1/34 , B05D3/06 , B05D3/067 , B05D3/068 , B05D3/12 , B29B11/00 , B29B11/16 , B29C35/0805 , B29C35/16 , B29C47/0002 , B29C64/106 , B29C64/129 , B29C64/135 , B29C64/25 , B29C69/001 , B29C70/16 , B29C70/28 , B29C70/38 , B29C70/545 , B29C2035/0822 , B29C2035/0827 , B29C2035/0833 , B29C2035/0838 , B29C2035/0844 , B29K2063/00 , B29K2101/10 , B29K2105/0058 , B29K2105/06 , B29K2105/0872 , B29K2105/10 , B29K2105/101 , B29K2105/12 , B29K2105/25 , B29K2105/253 , B29K2995/005 , B29L2031/00 , B29L2031/3076 , B33Y10/00 , B33Y30/00 , B33Y40/00 , B33Y50/02 , C09D5/00 , C09D201/00
Abstract: A system (100) for additively manufacturing a composite part (102) is disclosed. The system (100) comprises a housing (104) and a nozzle (107). The nozzle (107) is supported by the housing (104). The nozzle (107) comprises an outlet (110), sized to dispense a continuous flexible line (112). The continuous flexible line (112) comprises a non-resin component (114) and a photopolymer-resin component (116). The system (100) also comprises a feed mechanism (118), supported within the housing (104). The feed mechanism (118) is configured to push the continuous flexible line (112) out of the outlet (110) of the nozzle (107). The system (100) further comprises a light source (120), supported by the housing (104). The light source (120) is configured to deliver a light beam to the continuous flexible line (112) after the continuous flexible line (112) exits the outlet (110) of the nozzle (107) to at least partially cure the photopolymer-resin component (116) of the continuous flexible line (112).
Abstract translation: 公开了一种用于相加地制造复合部件（102）的系统（100）。 系统（100）包括壳体（104）和喷嘴（107）。 喷嘴（107）由壳体（104）支撑。 喷嘴（107）包括出口（110），其尺寸适于分配连续的柔性线（112）。 连续柔性线（112）包括非树脂组分（114）和光聚合物树脂组分（116）。 系统（100）还包括被支撑在壳体（104）内的进给机构（118）。 进给机构（118）构造成将连续柔性管线（112）推出喷嘴（107）的出口（110）。 系统（100）还包括由壳体（104）支撑的光源（120）。 光源（120）构造成在连续柔性管线（112）离开喷嘴（107）的出口（110）之后将光束传送到连续柔性管线（112），以至少部分地固化光聚合物树脂 连续柔性线（112）的部件（116）。
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Patent Agency Ranking
公开(公告)号：US20170028639A1
公开(公告)日：2017-02-02
申请号：US15063443
申请日：2016-03-07
Applicant: The Boeing Company
Inventor： Nick S. Evans , Faraón Torres , Ryan G. Ziegler , Samuel F. Harrison , Ciro J. Grijalva, III , Hayden S. Osborn
IPC: B29C67/00
CPC classification number: B33Y70/00 , B05D1/265 , B05D1/34 , B05D3/06 , B05D3/067 , B05D3/068 , B05D3/12 , B29B11/00 , B29B11/16 , B29C35/0805 , B29C35/16 , B29C47/0002 , B29C64/00 , B29C64/106 , B29C64/129 , B29C64/135 , B29C64/165 , B29C64/20 , B29C64/25 , B29C64/386 , B29C64/40 , B29C69/001 , B29C70/16 , B29C70/28 , B29C70/38 , B29C70/545 , B29C2035/0822 , B29C2035/0827 , B29C2035/0833 , B29C2035/0838 , B29C2035/0844 , B29K2063/00 , B29K2101/10 , B29K2105/0058 , B29K2105/06 , B29K2105/0872 , B29K2105/10 , B29K2105/101 , B29K2105/12 , B29K2105/25 , B29K2105/253 , B29K2995/005 , B29L2031/00 , B29L2031/3076 , B33Y10/00 , B33Y30/00 , B33Y40/00 , B33Y50/02 , C09D5/00 , C09D201/00
Abstract: A method (500) of additively manufacturing a composite part (102) comprises applying a first quantity of a first part (253) of a thermosetting resin (252) to a first element (271) of a non-resin component (108) by pulling the first element (271) through a first resin-part applicator (236) and applying a second quantity of a second part (255) of the thermosetting resin (252) to a second element (273) of the non-resin component (108) by pulling the second element (273) through a second resin-part applicator (237). The method (500) also comprises combining the first element (271) with the first quantity of first part (253) and the second element (273) with the second quantity of second part (255), to create a continuous flexible line (106). The method (500) additionally comprises routing the continuous flexible line (106) into a delivery guide (112) and depositing, via the delivery guide (112), a segment (120) of the continuous flexible line (106) along a print path (122).
Abstract translation: 复合部件（102）的附加制造方法（500）包括将第一量的热固性树脂（252）的第一部分（253）施加到非树脂部件（108）的第一元件（271）上，通过 通过第一树脂部分施加器（236）拉动第一元件（271）并将第二量的热固性树脂（252）的第二部分（255）施加到非树脂部件的第二元件（273）（ 108）通过第二树脂部分施加器（237）拉动第二元件（273）。 方法（500）还包括将第一元件（271）与第一数量的第一部分（253）和第二元件（273）与第二数量的第二部分（255）组合，以产生连续的柔性线（106） ）。 方法（500）还包括将连续柔性管线（106）路由到输送引导件（112）中并且经由输送引导件（112）沿着打印路径沉积连续柔性管线（106）的段（120） （122）。
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公开(公告)号：US20170028627A1
公开(公告)日：2017-02-02
申请号：US14920779
申请日：2015-10-22
Applicant: The Boeing Company
Inventor： Nick S. Evans , Faraón Torres , Ryan G. Ziegler , Samuel F. Harrison , Ciro J. Grijalva, III , Hayden S. Osborn
IPC: B29C67/00
CPC classification number: B33Y70/00 , B05D1/265 , B05D1/34 , B05D3/06 , B05D3/067 , B05D3/068 , B05D3/12 , B29B11/00 , B29B11/16 , B29C35/0805 , B29C35/16 , B29C47/0002 , B29C64/00 , B29C64/106 , B29C64/129 , B29C64/135 , B29C64/165 , B29C64/20 , B29C64/25 , B29C64/386 , B29C64/40 , B29C69/001 , B29C70/16 , B29C70/28 , B29C70/38 , B29C70/545 , B29C2035/0822 , B29C2035/0827 , B29C2035/0833 , B29C2035/0838 , B29C2035/0844 , B29K2063/00 , B29K2101/10 , B29K2105/0058 , B29K2105/06 , B29K2105/0872 , B29K2105/10 , B29K2105/101 , B29K2105/12 , B29K2105/25 , B29K2105/253 , B29K2995/005 , B29L2031/00 , B29L2031/3076 , B33Y10/00 , B33Y30/00 , B33Y40/00 , B33Y50/02 , C09D5/00 , C09D201/00
Abstract: A method (400) of additively manufacturing a composite part (102) comprises applying a liquid photopolymer resin (252) to a non-resin component (108) to create a continuous flexible line (106) by pulling the non-resin component (108) through a vessel (236), containing a volume of the liquid photopolymer resin (252). The continuous flexible line (106) comprises the non-resin component (108) and a photopolymer-resin component (110) that comprises at least some of the liquid photopolymer resin (252) applied to the non-resin component (108). The method (400) further comprises routing the continuous flexible line (106) into a delivery guide (112), pushing the continuous flexible line (106) out of the delivery guide (112), depositing, via the delivery guide (112), a segment (120) of the continuous flexible line (106) along a print path (122), and delivering curing energy (118) at least to a portion (124) of the segment (120) of the continuous flexible line (106).
Abstract translation: 复合部件（102）的附加制造方法（400）包括：向非树脂部件（108）施加液体光聚合物树脂（252），以通过拉动非树脂部件（108）来形成连续柔性线（106） ）通过容纳液体光聚合物树脂（252）的容器（236）。 连续柔性线（106）包括非树脂组分（108）和包含施加到非树脂组分（108）的至少一些液体光聚合物树脂（252）的光聚合物树脂组分（110）。 方法（400）还包括将连续柔性管线（106）引导到输送引导件（112）中，将连续柔性管线（106）推出输送引导件（112），经由输送引导件（112） 连续柔性管线（106）沿着打印路径（122）的段（120），并且至少向连续柔性管线（106）的段（120）的部分（124）递送固化能量（118） 。
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公开(公告)号：US20170028625A1
公开(公告)日：2017-02-02
申请号：US14995742
申请日：2016-01-14
Applicant: The Boeing Company
Inventor： Nick S. Evans , Faraón Torres , Ryan G. Ziegler , Samuel F. Harrison , Ciro J. Grijalva, III , Hayden S. Osborn
CPC classification number: B33Y70/00 , B05D1/265 , B05D1/34 , B05D3/06 , B05D3/067 , B05D3/068 , B05D3/12 , B29B11/00 , B29B11/16 , B29C35/0805 , B29C35/16 , B29C47/0002 , B29C64/00 , B29C64/106 , B29C64/129 , B29C64/135 , B29C64/165 , B29C64/20 , B29C64/25 , B29C64/386 , B29C64/40 , B29C69/001 , B29C70/16 , B29C70/28 , B29C70/38 , B29C70/545 , B29C2035/0822 , B29C2035/0827 , B29C2035/0833 , B29C2035/0838 , B29C2035/0844 , B29K2063/00 , B29K2101/10 , B29K2105/0058 , B29K2105/06 , B29K2105/0872 , B29K2105/10 , B29K2105/101 , B29K2105/12 , B29K2105/25 , B29K2105/253 , B29K2995/005 , B29L2031/00 , B29L2031/3076 , B33Y10/00 , B33Y30/00 , B33Y40/00 , B33Y50/02 , C09D5/00 , C09D201/00
Abstract: A method (400) of additively manufacturing a composite part (102) is disclosed. The method (400) comprises applying a thermosetting resin (252) to a non-resin component (108) of a continuous flexible line (106) while pushing the non-resin component (108) through a delivery guide (112) and pushing the continuous flexible line (106) out of the delivery guide (112). The continuous flexible line (106) further comprises a thermosetting resin component (110) that comprises at least some of the thermosetting resin (252) applied to the non-resin component (108). The method (400) further comprises depositing, via the delivery guide (112), a segment (120) of the continuous flexible line (106) along the print path (122).
Abstract translation: 公开了一种加法制造复合部件（102）的方法（400）。 方法（400）包括将热固性树脂（252）施加到连续柔性管线（106）的非树脂部件（108）上，同时将非树脂部件（108）推动通过输送引导件（112）并将 连续的柔性管线（106）从输送引导件（112）中取出。 连续柔性线（106）还包括热固性树脂组分（110），其包含施加到非树脂组分（108）上的至少一些热固性树脂（252）。 方法（400）还包括沿着打印路径（122）经由输送引导件（112）沉积连续柔性管线（106）的段（120）。
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公开(公告)号：US20170028619A1
公开(公告)日：2017-02-02
申请号：US14841472
申请日：2015-08-31
Applicant: The Boeing Company
Inventor： Nick S. Evans , Faraón Torres , Ryan G. Ziegler , Samuel F. Harrison , Ciro J. Grijalva, III , Hayden S. Osborn
CPC classification number: B33Y70/00 , B05D1/265 , B05D1/34 , B05D3/06 , B05D3/067 , B05D3/068 , B05D3/12 , B29B11/00 , B29B11/16 , B29C35/0805 , B29C35/16 , B29C47/0002 , B29C64/00 , B29C64/106 , B29C64/129 , B29C64/135 , B29C64/165 , B29C64/20 , B29C64/25 , B29C64/386 , B29C64/40 , B29C69/001 , B29C70/16 , B29C70/28 , B29C70/38 , B29C70/545 , B29C2035/0822 , B29C2035/0827 , B29C2035/0833 , B29C2035/0838 , B29C2035/0844 , B29K2063/00 , B29K2101/10 , B29K2105/0058 , B29K2105/06 , B29K2105/0872 , B29K2105/10 , B29K2105/101 , B29K2105/12 , B29K2105/25 , B29K2105/253 , B29K2995/005 , B29L2031/00 , B29L2031/3076 , B33Y10/00 , B33Y30/00 , B33Y40/00 , B33Y50/02 , C09D5/00 , C09D201/00
Abstract: A method (300) of additively manufacturing a composite part (102) comprises depositing a segment (120) of a continuous flexible line (106) along a print path (122). The continuous flexible line (106) comprises a non-resin component (108) and a photopolymer-resin component (110) that is partially cured. The method (300) also comprises delivering a predetermined or actively determined amount of curing energy (118) at least to a portion (124) of the segment (120) of the continuous flexible line (106) at a controlled rate while advancing the continuous flexible line (106) toward the print path (122) and after the segment (120) of the continuous flexible line (106) is deposited along the print path (122) to at least partially cure at least the portion (124) of the segment (120) of the continuous flexible line (106).
Abstract translation: 叠加制造复合部件（102）的方法（300）包括沿着打印路径（122）沉积连续柔性管线（106）的段（120）。 连续柔性管线（106）包括部分固化的非树脂部件（108）和光聚合物树脂部件（110）。 方法（300）还包括以可控制的速率将至少预定或主动确定量的固化能量（118）输送到连续柔性管线（106）的段（120）的一部分（124） 柔性线（106）朝向打印路径（122）并且在连续柔性线（106）的段（120）之后沿着打印路径（122）沉积以至少部分地固化至少部分（124）的部分 所述连续柔性管线（106）的段（120）。
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公开(公告)号：US20170028588A1
公开(公告)日：2017-02-02
申请号：US15063417
申请日：2016-03-07
Applicant: The Boeing Company
Inventor： Nick S. Evans , Faraón Torres , Ryan G. Ziegler , Samuel F. Harrison , Ciro J. Grijalva, III , Hayden S. Osborn
IPC: B29B11/16 , B33Y70/00 , B29C67/00 , C09D201/00 , C09D5/00
CPC classification number: B33Y70/00 , B05D1/265 , B05D1/34 , B05D3/06 , B05D3/067 , B05D3/068 , B05D3/12 , B29B11/00 , B29B11/16 , B29C35/0805 , B29C35/16 , B29C47/0002 , B29C64/00 , B29C64/106 , B29C64/129 , B29C64/135 , B29C64/165 , B29C64/20 , B29C64/25 , B29C64/386 , B29C64/40 , B29C69/001 , B29C70/16 , B29C70/28 , B29C70/38 , B29C70/545 , B29C2035/0822 , B29C2035/0827 , B29C2035/0833 , B29C2035/0838 , B29C2035/0844 , B29K2063/00 , B29K2101/10 , B29K2105/0058 , B29K2105/06 , B29K2105/0872 , B29K2105/10 , B29K2105/101 , B29K2105/12 , B29K2105/25 , B29K2105/253 , B29K2995/005 , B29L2031/00 , B29L2031/3076 , B33Y10/00 , B33Y30/00 , B33Y40/00 , B33Y50/02 , C09D5/00 , C09D201/00
Abstract: A method (400) of additively manufacturing a composite part (102) comprises applying a thermosetting resin (252) to a non-resin component (108) to create a continuous flexible line (106) by pulling a non-resin component (108) through a first resin-part applicator (236), in which a first quantity of a first part (253) of the thermosetting resin (252) is applied to the non-resin component (108), and by pulling a non-resin component (108) through a second resin-part applicator (237), in which a second quantity of a second part (255) of the thermosetting resin (252) is applied to at least a portion of the first quantity of the first part (253) of the thermosetting resin (252), applied to the non-resin component (108). The method (400) further comprises routing the continuous flexible line (106) into a delivery guide (112) and depositing, via the delivery guide (112), a segment (120) of the continuous flexible line (106) along a print path (122).
Abstract translation: 复合部件（102）的附加制造方法（400）包括通过拉动非树脂部件（108）将热固性树脂（252）施加到非树脂部件（108）以形成连续柔性线（106） 通过第一树脂部分施加器（236），其中将第一量的热固性树脂（252）的第一部分（253）施加到非树脂部件（108）上，并且通过拉动非树脂部件 （108）通过第二树脂部分施加器（237），其中将第二量的热固性树脂（252）的第二部分（255）施加到第一部分（253）的至少一部分 ）的热固化性树脂（252），涂布在非树脂成分（108）上。 所述方法（400）还包括将所述连续柔性管线（106）路由到输送引导件（112）中并且经由所述输送引导件（112）沿着打印路径沉积所述连续柔性管线（106）的段（120） （122）。
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