公开(公告)号：US10166753B2

公开(公告)日：2019-01-01

申请号：US14920767

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 ,  B33Y70/00 ,  B29C69/00 ,  B29C70/28 ,  B05D1/26 ,  B05D1/34 ,  B05D3/06 ,  B05D3/12 ,  B29C35/16 ,  B29C70/16 ,  B29C70/38 ,  B29C70/54 ,  C09D5/00 ,  B29B11/00 ,  B29B11/16 ,  C09D201/00 ,  B29C47/00 ,  B29C64/106 ,  B29K105/00 ,  B33Y10/00 ,  B29L31/30 ,  B29L31/00 ,  B33Y30/00 ,  B33Y40/00 ,  B29K63/00 ,  B29K105/08 ,  B29K105/10 ,  B33Y50/02 ,  B29K101/10 ,  B29K105/12 ,  B29C35/08 ,  B29K105/06 ,  B29C64/135 ,  B29C64/129 ,  B29C64/25

Abstract: A method of additively manufacturing composite part comprises depositing a segment of a continuous flexible line along a print path. The continuous flexible line comprises a non-resin component and further comprises a photopolymer-resin component that is uncured. The method further comprises delivering a predetermined or actively determined amount of curing energy at least to a portion of the segment of the continuous flexible line at a controlled rate while advancing the continuous flexible line toward the print path and after the segment of the continuous flexible line is deposited along the print path to at least partially cure at least the portion of the segment of the continuous flexible line.

公开(公告)号：US20180320569A1

公开(公告)日：2018-11-08

申请号：US15586344

申请日：2017-05-04

Applicant: THE BOEING COMPANY

Inventor： Nassar D. Rwashdeh ,  Ivan F. Trivino ,  Ryan Hinds ,  Hayden S. Osborn ,  Khalid Salih Alshobber ,  Rita Jeannine Ann Taitano Johnson ,  Genesis Marvin Supnet Pilarca ,  Michael Joseph Jelmini

IPC: F01M11/04 ,  F01D25/18

CPC classification number: F01M11/04 ,  F01D25/18

Abstract: An oil filling assembly is configured to couple to an intake port of an engine to fill an oil tank connected to the intake port. The intake port is located behind an access door of the engine. The oil filling assembly includes a hopper defining an oil retention chamber that is configured to receive oil, and a coupler extending from the hopper. The coupler includes a neck defining an oil outlet fluidly connected to the oil retention chamber. The coupler is configured to removably mount to the intake port of the engine.

公开(公告)号：US10112380B2

公开(公告)日：2018-10-30

申请号：US14841500

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

IPC: B33Y30/00 ,  B33Y70/00 ,  B29C69/00 ,  B29C70/28 ,  B05D1/26 ,  B05D1/34 ,  B05D3/06 ,  B05D3/12 ,  B29C35/16 ,  B29C70/16 ,  B29C70/38 ,  B29C70/54 ,  C09D5/00 ,  B29B11/00 ,  B29B11/16 ,  C09D201/00 ,  B29C47/00 ,  B29C64/106 ,  B29C64/135 ,  B29C64/129 ,  B29C64/386 ,  B29C64/20 ,  B29C64/00 ,  B29C64/40 ,  B29C64/165 ,  B29K105/00 ,  B33Y10/00 ,  B29L31/30 ,  B29L31/00 ,  B33Y40/00 ,  B29K63/00 ,  B29K105/08 ,  B29K105/10 ,  B33Y50/02 ,  B29K101/10 ,  B29K105/12 ,  B29C35/08 ,  B29K105/06 ,  B29C64/25

Abstract: A method of additively manufacturing a composite part comprises pushing a continuous flexible line through a delivery guide. The continuous flexible line comprises a non-resin component and a photopolymer-resin component that is partially cured. The method also comprises depositing, via the delivery guide, a segment of the continuous flexible line along a print path. Additionally, the method comprises delivering curing energy at least to a portion of the segment of the continuous flexible line deposited along the print path.

公开(公告)号：US20180245613A1

公开(公告)日：2018-08-30

申请号：US15966855

申请日：2018-04-30

Applicant: The Boeing Company

Inventor： Karina R. Nipper ,  Hayden S. Osborn

IPC: F16B5/01 ,  B32B7/08 ,  F16B5/02

CPC classification number: F16B5/01 ,  B32B7/08 ,  B32B2250/40 ,  B32B2605/18 ,  F16B5/02

Abstract: A threaded adjustable-height insert may be installed in a bore of a sandwich panel, such that the insert may be configured to transfer a load to the sandwich panel. The threaded adjustable-height insert may include a first insert part and a second insert part that may be selectively operatively positioned with respect to each other. The overall height of the threaded adjustable-height insert may be adjusted by longitudinally sliding the second insert part with respect to the first insert part and rotating the second insert part with respect to the first insert part. Presently disclosed threaded adjustable-height inserts may be configured for flush installation in a sandwich panel. Methods of installing such threaded adjustable-height inserts and adjusting the height of the same are also disclosed.

公开(公告)号：US20170028644A1

公开(公告)日：2017-02-02

申请号：US14841470

申请日：2015-08-31

Applicant: The Boeing Company

Inventor： Nick S. Evans ,  Faraon Torres ,  Ryan G. Ziegler ,  Samuel F. Harrison ,  Ciro J. Grijalva, III ,  Hayden S. Osborn

IPC: B29C67/00

CPC classification number: B29C64/165 ,  B29B15/122 ,  B29C64/106 ,  B29C64/386 ,  B29C70/384 ,  B29C70/524 ,  B33Y30/00

Abstract: A system (100) for additively manufacturing a composite part (102) comprises a delivery assembly (266), a feed mechanism (104), and a source (116) of curing energy (118). The delivery assembly (266) comprises a delivery guide (112) movable relative to a surface (114) and is configured to deposit a continuous flexible line (106) along a print path (122). The delivery assembly (266) further comprises a first inlet (170), configured to receive a non-resin component (108), and a second inlet (250), configured to receive a photopolymer resin (252). The delivery assembly (266) applies the photopolymer resin (252) to the non-resin component (108). The feed mechanism (104) pushes the continuous flexible line (106) out of the delivery guide (112). The source (116) of the curing energy (118) delivers the curing energy (118) to a portion (124) of the continuous flexible line (106) after it exits the delivery guide (112).

Abstract translation: 用于相加地制造复合部件（102）的系统（100）包括输送组件（266），进料机构（104）和固化能量源（118）。 输送组件（266）包括相对于表面（114）可移动的输送引导件（112），并且构造成沿着打印路径（122）沉积连续的柔性线（106）。 输送组件（266）还包括构造成接收非树脂组分（108）的第一入口（170）和构造成接收光聚合物树脂（252）的第二入口（250）。 输送组件（266）将光聚合物树脂（252）施加到非树脂组分（108）。 进给机构（104）将连续的柔性管线（106）推出输出引导件（112）。 固化能量（118）的源（116）在其离开输送引导件（112）之后将固化能量（118）输送到连续柔性管线（106）的一部分（124）。

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

IPC: B29C67/00 ,  B29C47/00

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 ,  B29C64/106 ,  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）。

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）。

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） 。

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

IPC: B29C67/00 ,  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) 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）。

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

IPC: B29C67/00 ,  B29C69/00 ,  B29C70/28 ,  B29C69/02

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）。