| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 41 | Thermoplastic Bonded Preforms and Thermoset Matrices Formed Therewith | US15432156 | 2017-02-14 | US20170239909A1 | 2017-08-24 | Mark Janney; Mark Mauhar |
| A thermoplastic bonded preform and method of manufacturing the preform are disclosed. The preform comprises a primary fiber comprising little or no sizing; a mechanical fiber; and a thermoplastic. | ||||||
| 42 | SYSTEMS AND METHODS FOR ADDITIVELY MANUFACTURING COMPOSITE PARTS | US15063443 | 2016-03-07 | US20170028639A1 | 2017-02-02 | Nick S. Evans; Faraón Torres; Ryan G. Ziegler; Samuel F. Harrison; Ciro J. Grijalva, III; Hayden S. Osborn |
| 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). | ||||||
| 43 | SYSTEMS AND METHODS FOR ADDITIVELY MANUFACTURING COMPOSITE PARTS | US14995620 | 2016-01-14 | US20170028636A1 | 2017-02-02 | Nick S. Evans; Faraón Torres; Ryan G. Ziegler; Samuel F. Harrison; Ciro J. Grijalva, III; Hayden S. Osborn |
| 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). | ||||||
| 44 | SYSTEMS AND METHODS FOR ADDITIVELY MANUFACTURING COMPOSITE PARTS | US14931635 | 2015-11-03 | US20170028634A1 | 2017-02-02 | Nick S. Evans; Faraón Torres; Ryan G. Ziegler; Samuel F. Harrison; Ciro J. Grijalva, III; Hayden S. Osborn |
| A method (300) of additively manufacturing a composite part (102) is disclosed. The method (300) comprises pushing a continuous flexible line (106) through a delivery guide (112). The continuous flexible line (106) comprises a non-resin component (108) and a thermosetting-epoxy-resin component (110) that is partially cured. The method (300) also comprises depositing, via the delivery guide (112), a segment (120) of the continuous flexible line (106) along a print path (122). The method (300) further comprises maintaining the thermosetting-epoxy-resin component (110) of at least the continuous flexible line (106) being pushed through the delivery guide (112) below a threshold temperature prior to depositing the segment (120) of the continuous flexible line (106) along the print path (120). | ||||||
| 45 | SYSTEMS AND METHODS FOR ADDITIVELY MANUFACTURING COMPOSITE PARTS | US14841524 | 2015-08-31 | US20170028624A1 | 2017-02-02 | Nick S. Evans; Faraón Torres; Ryan G. Ziegler; Samuel F. Harrison; Ciro J. Grijalva, III; Hayden S. Osborn |
| A method (400) of additively manufacturing a composite part (102) comprises applying a photopolymer resin (252) to a non-resin component (108) while pushing a continuous flexible line (106) through a delivery assembly (266). The continuous flexible line (106) comprises the non-resin component (108) and a photopolymer-resin component (110) that comprises at least some of the photopolymer resin (252) applied to the non-resin component (108). The method (400) also comprises depositing, via the delivery assembly (266), a segment (120) of the continuous flexible line (106) along a print path (122). The method (400) further comprises delivering curing energy (118) to at least a portion (124) of the segment (120) of the continuous flexible line (106) deposited along the print path (122). | ||||||
| 46 | SYSTEMS AND METHODS FOR ADDITIVELY MANUFACTURING COMPOSITE PARTS | US14841472 | 2015-08-31 | US20170028619A1 | 2017-02-02 | Nick S. Evans; Faraón Torres; Ryan G. Ziegler; Samuel F. Harrison; Ciro J. Grijalva, III; Hayden S. Osborn |
| 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). | ||||||
| 47 | SYSTEMS AND METHODS FOR ADDITIVELY MANUFACTURING COMPOSITE PARTS | US15063417 | 2016-03-07 | US20170028588A1 | 2017-02-02 | Nick S. Evans; Faraón Torres; Ryan G. Ziegler; Samuel F. Harrison; Ciro J. Grijalva, III; Hayden S. Osborn |
| 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). | ||||||
| 48 | IN-MOLD MOLDING METHOD, IN-MOLD TRANSFER FILM AND MANUFACTURING METHOD THEREFOR | US14441442 | 2013-09-19 | US20150290852A1 | 2015-10-15 | Takashi Nakagawa; Mitsuhiro Yoshinaga |
| 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. | ||||||
| 49 | PET PREFORM FOR A TRANSIENTLY-EXTANT DRINK BOTTLE | US12852484 | 2010-08-08 | US20120031869A1 | 2012-02-09 | Alan Bauer |
| Performs used in the preperation of a transiently-extant drink bottle is described. The drink bottle may be formed from joining two separate closable fluid holding compartments, each compartment capable of holding a unique drinking fluid. Joining of the compartments tends to allow for greater consumer choice in beverage selection as well as potential cooling of one beverage through its non-contact proximity to a second frozen beverage. PET preforms having joining elements can also aid in joining of closable fluid holding compartments to form a transiently-extant disposable drink bottle. | ||||||
| 50 | Vortex control in slurry molding applications | US11592660 | 2006-11-03 | US07678307B1 | 2010-03-16 | Ervin Geiger |
| A molding head is especially adapted for vacuum molding or forming of structures and, in particular, fibrous composite structures in an adjustable, controllable three dimensional orientation before, during and after molding. Such a molding head includes a mold plate with narrow slots in the mold surface thereof and wider channels in the back surface thereof, with such slots and channels intersecting one another. A control system of servomotors or other actuators permits movement and orientation of the mold head during forming, thereby creating the ability to vary the material properties based on gravity and particle or suspension grain, thickness and other now controllable properties. | ||||||
| 51 | Machine for shearing films of thermoplastic material | US421159 | 1982-09-22 | US4483226A | 1984-11-20 | Edoardo Costarelli |
| Machine for shearing films of thermoplastic material between a compression surface (5), joined to a piston (4) and operated hydraulically by means of a cylinder (3) from an electric motor powered pump, and the latticed bottom of a container (1). The latticed bottom has open mesh (8') along the perimeter, in which punches (6) on the compression surface (5) penetrate. The hydraulic device, the density of the cutting profiles and the cooperation of the punches (6) to expel the material through the mesh (8') reduce energy consumption to 1/10 with respect to rotation type shearing machines. | ||||||
| 52 | Method of manufacturing artificial logs | US3788919D | 1971-08-13 | US3788919A | 1974-01-29 | SUZUKI R; HOSHI H; UMEYA K |
| A SYNTHETIC RESIN SHEET, EITHER FOAMED OR NON-FOAMED, OF A SYNTHETIC RESIN MATERIAL CONTAINING A FILLER IS LAMINATED BY WINDING IT INTO THE FORM OF A ROLL TO THEREBY FORM AN ARTIFICIAL LOG. THE ARTIFICIAL LOG THUS PRODUCED HAS A GRAIN STRUCTURE CLOSELY SIMULATING THAT OF NATURAL LUMBER.
|
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| 53 | Methods for additively manufacturing composite parts | US14995742 | 2016-01-14 | US10124570B2 | 2018-11-13 | Nick S. Evans; Faraón Torres; Ryan G. Ziegler; Samuel F. Harrison; Ciro J. Grijalva, III; Hayden S. Osborn |
| A method of additively manufacturing a composite part is disclosed. The method comprises applying a thermosetting resin to a non-resin component of a continuous flexible line while pushing the non-resin component through a delivery guide and pushing the continuous flexible line out of the delivery guide. The continuous flexible line further comprises a thermosetting resin component that comprises at least some of the thermosetting resin applied to the non-resin component. The method further comprises depositing, via the delivery guide, a segment of the continuous flexible line along the print path. | ||||||
| 54 | Systems for additively manufacturing composite parts | US15087882 | 2016-03-31 | US10071545B2 | 2018-09-11 | Samuel F. Harrison; Faraón Torres; Ryan G. Ziegler; Nick S. Evans; Ciro J. Grijalva, III; Hayden S. Osborn |
| A system for additively manufacturing a composite part is disclosed. The system comprises a housing and a nozzle. The nozzle is supported by the housing. The nozzle comprises an outlet, sized to dispense a continuous flexible line. The continuous flexible line comprises a non-resin component and a photopolymer-resin component. The system also comprises a feed mechanism, supported within the housing. The feed mechanism is configured to push the continuous flexible line out of the outlet of the nozzle. The system further comprises a light source, supported by the housing. The light source is configured to deliver a light beam to the continuous flexible line after the continuous flexible line exits the outlet of the nozzle to at least partially cure the photopolymer-resin component of the continuous flexible line. | ||||||
| 55 | PARISON FOREIGN MATTER DETECTION SYSTEM | US15760592 | 2016-07-29 | US20180250870A1 | 2018-09-06 | Masateru Takayanagi |
| Some embodiments are directed to a system for detecting foreign matter in a parison discharged successively from a discharge device, the system comprising: infrared cameras that detect infrared beams emitted from the parison; and a determination unit that determines whether foreign matter is present in the parison on the basis of the infrared beams detected by the infrared cameras. A determination area is set in the parison in a discharge direction of the parison, a storage unit is provided that stores an infrared threshold set for the determination area, and the determination unit compares the detected values from the infrared cameras with the threshold. | ||||||
| 56 | Film manufacturing method, film manufacturing device, and jig | US14648106 | 2013-11-28 | US09656410B2 | 2017-05-23 | Takashi Urabe; Hisayasu Kaneshiro; Koji Hanada |
| A film is formed by extruding a resin from a lip opening (3) of a multilayer extrusion die (1) in a state in which a rectifying jig (10) does not cover the lip opening (3) but covers a seal part (6) while being located adjacent to each end in a longer side direction of the lip opening (3). | ||||||
| 57 | SYSTEMS AND METHODS FOR ADDITIVELY MANUFACTURING COMPOSITE PARTS | US15063347 | 2016-03-07 | US20170028637A1 | 2017-02-02 | Nick S. Evans; Faraón Torres; Ryan G. Ziegler; Samuel F. Harrison; Ciro J. Grijalva, III; Hayden S. Osborn |
| 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). | ||||||
| 58 | SYSTEMS AND METHODS FOR ADDITIVELY MANUFACTURING COMPOSITE PARTS | US14995742 | 2016-01-14 | US20170028625A1 | 2017-02-02 | Nick S. Evans; Faraón Torres; Ryan G. Ziegler; Samuel F. Harrison; Ciro J. Grijalva, III; Hayden S. Osborn |
| 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). | ||||||
| 59 | SYSTEMS AND METHODS FOR ADDITIVELY MANUFACTURING COMPOSITE PARTS | US14931692 | 2015-11-03 | US20170028621A1 | 2017-02-02 | Nick S. Evans; Faraón Torres; Ryan G. Ziegler; Samuel F. Harrison; Ciro J. Grijalva, III; Hayden S. Osborn |
| A method (400) of additively manufacturing a composite part (102) is disclosed. The method (400) comprises depositing, via a delivery guide (112), 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-epoxy-resin component (110) that is partially cured. The method (400) also comprises maintaining the thermosetting-epoxy-resin component (110) of at least the continuous flexible line (106) being advanced toward the print path (122) via the delivery guide (112) below a threshold temperature. The method (400) further comprises delivering a predetermined or actively determined amount of curing energy (118) to 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) to at least partially cure the segment (120) of the continuous flexible line (106). | ||||||
| 60 | SYSTEMS AND METHODS FOR ADDITIVELY MANUFACTURING COMPOSITE PARTS | US14841500 | 2015-08-31 | US20170028620A1 | 2017-02-02 | Nick S. Evans; Faraón Torres; Ryan G. Ziegler; Samuel F. Harrison; Ciro J. Grijalva, III; Hayden S. Osborn |
| A method (400) of additively manufacturing a composite part (102) comprises pushing a continuous flexible line (106) through a delivery guide (112). The continuous flexible line comprises (106) a non-resin component (108) and a photopolymer-resin component (110) that is partially cured. The method (400) also comprises depositing, via the delivery guide (112), a segment (120) of the continuous flexible line (106) along a print path (122). Additionally, the method (400) comprises delivering curing energy (118) at least to a portion (124) of the segment (120) of the continuous flexible line (106) deposited along the print path (122). | ||||||
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