公开(公告)号：US20170028637A1

公开(公告)日：2017-02-02

申请号：US15063347

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 ,  B29B11/00 ,  B29C70/54 ,  B29C69/00 ,  B29C70/38 ,  B29C70/16

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 ,  B29C48/02 ,  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 system (700) for additively manufacturing a composite part (102) comprises a delivery guide (112), movable relative to a surface (114). The delivery guide (112) is configured to deposit at least 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 thermosetting-resin component (110). The thermosetting-resin component (110) comprises a first part (253) and a second part (255). The non-resin component (108) comprises a first element (271) and a second element (273). The system (700) further comprises a first resin-part applicator (236), configured to apply the first part (253) to the first element (271), and a second resin-part applicator (237), configured to apply the second part (255) to the second element (273). The system (700) also comprises a feed mechanism (104), configured to pull the first element (271) through the first resin-part applicator (236), to pull the second element (273) through the second resin-part applicator (237), and to push the continuous flexible line (106) out of the delivery guide (112).

Abstract translation: 用于相加地制造复合部件（102）的系统（700）包括可相对于表面（114）移动的输送引导件（112）。 输送引导件（112）被配置成沿着打印路径（122）沉积连续柔性线（106）的至少一段（120）。 连续柔性管线（106）包括非树脂部件（108）和热固性树脂部件（110）。 热固性树脂组分（110）包括第一部分（253）和第二部分（255）。 非树脂部件（108）包括第一元件（271）和第二元件（273）。 所述系统（700）还包括构造成将第一部分（253）施加到第一元件（271）的第一树脂部分施加器（236）和第二树脂部分施加器（237），其被配置为施加第二部分 部分（255）到第二元素（273）。 系统（700）还包括进给机构（104），其构造成通过第一树脂部分施加器（236）拉动第一元件（271），以将第二元件（273）拉过第二树脂部分施加器 并且将连续柔性线（106）推出输出导向件（112）。

公开(公告)号：US20170028636A1

公开(公告)日：2017-02-02

申请号：US14995620

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 ,  B29C69/00 ,  B29C70/54 ,  B29C70/38 ,  B29C70/16

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) is disclosed. The method (300) 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 thermosetting resin component (110) that is not fully cured. The method (300) further comprises, while advancing the continuous flexible line (106) toward the print path (122), 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 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: 公开了一种叠加制造复合部件（102）的方法（300）。 方法（300）包括沿着打印路径（122）沉积连续柔性线（106）的段（120）。 连续柔性管线（106）包括未完全固化的非树脂部件（108）和热固性树脂部件（110）。 所述方法（300）还包括在将连续柔性管线（106）朝向打印路径（122）推进的同时，将至少预定或主动确定量的固化能量（118）输送到所述段的一部分（124） 在所述连续柔性管线（106）的段（120）沿着所述打印路径（122）沉积以至少部分地固化所述连续柔性管线（106）的所述部分（124）的部分 所述连续柔性线（106）的所述段（120）。

公开(公告)号：US20150290852A1

公开(公告)日：2015-10-15

申请号：US14441442

申请日：2013-09-19

Applicant: PANASONIC CORPORATION

Inventor： Takashi Nakagawa ,  Mitsuhiro Yoshinaga

IPC: B29C45/14 ,  B29B11/00 ,  B29C45/72

CPC classification number: B29C45/14827 ,  B29B11/00 ,  B29C45/14262 ,  B29C45/14811 ,  B29C45/7207 ,  B29K2101/00 ,  B29K2703/00 ,  B29K2715/006 ,  B29K2995/002 ,  B29K2995/0087 ,  B29L2009/00 ,  B29L2031/30 ,  B29L2031/762

Abstract: An in-mold molding method of the present invention is a method including: placing an in-mold transfer film in the cavity of an injection molding mold, the in-mold transfer film having a hard coating layer and a transfer section of a printed layer; and peeling, from the base material film of the in-mold transfer film, the transfer section transferred to a molding resin when a molding molded by injecting the molding resin into the cavity is removed by mold opening. The hard coating layer is ruptured in a mold opening process while the in-mold transfer film has a necessary elongation of A % on the side of the molding and the hard coating layer has a rupture elongation of at least A %+2% and less than A %+40% on the side of the molding. With this configuration, the in-mold transfer film can be stably peeled during in-mold molding.

Abstract translation: 本发明的模内成型方法是将模内转印膜配置在注射成型模具的型腔内的方式，具有硬涂层和印刷层的转印部的模内转印膜 ; 并且通过模具开口去除通过将模制树脂注入到模腔中而成型的模制树脂时，从模内转印膜的基材膜剥离转印部。 模内转印膜在模制品侧具有必要的A％伸长率，硬质涂层在开模过程中破裂，硬涂层的断裂伸长率至少为A％+ 2％以下 比成型品侧面的A％+ 40％。 通过这种构造，可以在模内成型时稳定地剥离模内转印膜。

公开(公告)号：US20150283730A1

公开(公告)日：2015-10-08

申请号：US14438802

申请日：2013-10-30

Applicant: MITSUBISHI RAYON CO., LTD.

Inventor： Yoshihide Kakimoto

IPC: B29B11/12 ,  B29B11/16

CPC classification number: B29B11/12 ,  B29B11/00 ,  B29B11/16 ,  B29C33/0016 ,  B29C33/306 ,  B29C51/082 ,  B29C51/14 ,  B29C51/16 ,  B29C51/28 ,  B29C51/421 ,  B29C70/44 ,  B29C70/46 ,  B29C70/56 ,  B29C2035/0822 ,  B29K2063/00 ,  B29K2101/10 ,  B29K2307/04 ,  B29K2995/0002 ,  B29K2995/0015

Abstract: A method of producing a preform, having a step for preparing a sheet-shaped prepreg and a preform mold having a forming surface and a separable portion constituting at least a portion of the forming surface, forming the prepreg using the preform mold, and then removing the preform together with the separable portion from the preform mold.

Abstract translation: 一种制造预成型体的方法，具有制备片状预浸料坯的步骤和具有构成至少一部分成形表面的成形表面和可分离部分的预成型模具，使用预成型模具形成预浸料，然后除去 预成型件与预成型模具的可分离部分一起。

公开(公告)号：US07544127B2

公开(公告)日：2009-06-09

申请号：US11395567

申请日：2006-03-31

Applicant: Chad Allen Dow ,  Merle Ray Gerber

Inventor： Chad Allen Dow ,  Merle Ray Gerber

IPC: A01F12/40

CPC classification number: B29B11/00 ,  A01F12/40 ,  G01B11/0675

Abstract: A straw chopper for an agricultural harvesting machine includes a housing, a rotor carried by the housing, and a stationary knife bank. The rotor includes a plurality of pendulously mounted knife blades. The stationary knife bank includes a plurality of stationary knife blades adjustably movable toward and away from the rotor. The stationary knife bank includes a tension rod extending longitudinally through the stationary knife bank and having a threaded end, and at least one wing nut threadingly engaged with the threaded end.

Abstract translation: 用于农业收割机的秸秆切碎机包括壳体，由壳体承载的转子和固定刀库。 转子包括多个下摆式的刀片。 固定刀库包括能够朝向和远离转子可调节地移动的多个固定刀片。 固定刀库包括纵向延伸通过固定刀库并具有螺纹端的拉杆，以及与螺纹端螺纹接合的至少一个翼螺母。

公开(公告)号：US3106441A

公开(公告)日：1963-10-08

申请号：US40660

申请日：1960-01-04

Applicant: GRACE W R & CO

Inventor： HARRISON JOHN W ,  LOWRY ROBERT D ,  BAIRD JR WILLIAM G ,  SHAVER ROBERT G

IPC: B29B11/00

CPC classification number: B29B11/00 ,  B29B2911/14593 ,  Y10S215/90 ,  Y10T156/1043 ,  Y10T156/1085

公开(公告)号：US2761176A

公开(公告)日：1956-09-04

申请号：US42139254

申请日：1954-04-06

Applicant: KENRO CORP

Inventor： WELCH KENNETH B ,  SACIA ROGER R

IPC: B29B11/00 ,  B29B13/10 ,  B44F5/00 ,  B44F9/04

CPC classification number: B29B13/10 ,  B29B11/00 ,  B44F5/00 ,  B44F9/04 ,  Y10T428/252

公开(公告)号：US20180088263A1

公开(公告)日：2018-03-29

申请号：US15688815

申请日：2017-08-28

Applicant: Murray Kendall Wilson ,  Yuichi Ogawa

Inventor： Murray Kendall Wilson ,  Yuichi Ogawa

IPC: G02B5/30 ,  G02B1/08 ,  G02C7/12

CPC classification number: G02B5/3016 ,  B29B11/00 ,  B29C51/082 ,  B29C69/00 ,  B29D11/00 ,  B29D11/00009 ,  B29D11/00644 ,  B32B37/00 ,  G02B1/08 ,  G02C7/12

Abstract: Described herein are improved thermoformed liquid crystal polarized wafers and methods of creating, and more specifically the utilization of an improved printed polarized crystal technology and wafer adhesion technology which enables the production of a polarized wafer capable of being thermoformed without a loss of alignment precision.

公开(公告)号：US09925704B2

公开(公告)日：2018-03-27

申请号：US14441442

申请日：2013-09-19

Applicant: Panasonic Intellectual Property Management Co., Ltd.

Inventor： Takashi Nakagawa ,  Mitsuhiro Yoshinaga

IPC: B29C45/14 ,  B29B11/00 ,  B29C45/72 ,  B29K101/00 ,  B29K703/00 ,  B29L9/00 ,  B29L31/30 ,  B29L31/00

CPC classification number: B29C45/14827 ,  B29B11/00 ,  B29C45/14262 ,  B29C45/14811 ,  B29C45/7207 ,  B29K2101/00 ,  B29K2703/00 ,  B29K2715/006 ,  B29K2995/002 ,  B29K2995/0087 ,  B29L2009/00 ,  B29L2031/30 ,  B29L2031/762

Abstract: An in-mold molding method of the present invention is a method including: placing an in-mold transfer film in the cavity of an injection molding mold, the in-mold transfer film having a hard coating layer and a transfer section of a printed layer; and peeling, from the base material film of the in-mold transfer film, the transfer section transferred to a molding resin when a molding molded by injecting the molding resin into the cavity is removed by mold opening. The hard coating layer is ruptured in a mold opening process while the in-mold transfer film has a necessary elongation of A % on the side of the molding and the hard coating layer has a rupture elongation of at least A %+2% and less than A %+40% on the side of the molding. With this configuration, the in-mold transfer film can be stably peeled during in-mold molding.

公开(公告)号：US20170266882A1

公开(公告)日：2017-09-21

申请号：US15615795

申请日：2017-06-06

Applicant: Huazhong University of Science and Technology

Inventor： Chunze YAN ,  Wei ZHU ,  Yusheng SHI ,  Jie LIU

IPC: B29C67/00 ,  B33Y10/00 ,  B29B11/14 ,  B29C67/04 ,  B29C51/02

CPC classification number: B29C67/04 ,  B29B11/00 ,  B29B11/14 ,  B29B11/16 ,  B29C51/02 ,  B29C64/153 ,  B29C67/00 ,  B29C70/12 ,  B29C2035/0838 ,  B29C2059/027 ,  B29K2101/10 ,  B33Y10/00 ,  B33Y70/00 ,  B33Y80/00 ,  C08G18/244 ,  C08G18/302 ,  C08G18/3281 ,  C08G18/48 ,  C08G18/6688 ,  C08G18/7664 ,  C08L63/00 ,  C08L75/08 ,  C08L77/02 ,  C08K7/06 ,  C08K7/14 ,  C08K7/04 ,  C08L61/06

Abstract: A method for manufacturing a composite product, including: 1) preparing a composite powder including 10-50 v. % of a polymer adhesive and 50-90 v. % of a chopped fiber; 2) shaping the composite powder by using a selective laser sintering technology to yield a preform including pores; 3) preparing a liquid thermosetting resin precursor, immersing the preform into the liquid thermosetting resin precursor, allowing a liquid thermosetting resin of the liquid thermosetting resin precursor to infiltrate into the pores of the preform, and exposing the upper end of the preform out of the liquid surface of the liquid thermosetting resin precursor to discharge gas out of the pores of the preform; 4) collecting the preform from the liquid thermosetting resin precursor and curing the preform; and 5) polishing the preform obtained in 4) to yield a composite product.