序号 专利名 申请号 申请日 公开(公告)号 公开(公告)日 发明人
121 손 바느질 가공품을 위한 패브릭 및 상기 패브릭으로 상기 가공품을 제조하는 방법 KR20187002877 2016-06-29 KR20180033200A 2018-04-02
손바느질프로젝트를위한패브릭피스및 상기패브릭으로상기프로젝트를생성하는방법에있어서, 특정패치워크디자인(3)을생성하기위한피규어(2)를, 동일한또는다른색상, 인쇄및/또는텍스처에의해, 통합하는클로스(cloth) 피스(1)로이루어지고, 상기피규어(2)의각각은윤곽을한정하는시임라인(4) 및선택적으로미리천공되는주변경계를한정하는절단라인(5)으로표시된다. 상기방법은상기피스(1)를얻는단계, 피규어(2)를절단라인(5)을따라절단하는단계; 및이들을함께바느질하는단계를포함한다. 선택적으로패치워크디자인(3)이선택되고, 피스(1)는원하는피규어(2) 및색상, 인쇄및/또는텍스처로오더링된다.
122 헤비-듀티 체인 KR1020157012654 2013-11-18 KR1020150087228A 2015-07-29 빈케디트리히; 마리센뢸로프
본발명은, 합성중합체얀을포함하는체인-링크들을함유하는헤비-듀티체인에관한것으로서, 상기체인이본질적으로평면형표면으로적어도팽팽하게유지되는경우, 각체인-링크는상기평면형표면상에직교프로젝션을갖고, 상기프로젝션은풋 프린트영역(A)을갖되, 이때매 2개의인접링크의 A및 A로서나타내는풋 프린트영역이하기식의관계에있다: 80%A≤ A≤ 100%A상기식에서, A은상기 2개의영역중 최소의것이고, 상기프로젝션은, 풋프린트영역 A에대한풋 프린트영역 A의비가최대로되는방식으로수행된다.
123 겹조직부를 갖는 직물지의 제조방법 및 그 직물지 KR1020100101444 2010-10-18 KR101055647B1 2011-08-10 김동숙; 이수길
PURPOSE: A method for manufacturing a woven fabric is provided to prevent twisting of a fabric and to express various patterns. CONSTITUTION: A method for fabricating a woven fabric comprises: a step of crossing and weaving an upper warp(11) and an upper weft to prepare an upper surface; a step of crossing and weaving a lower warp(21) and a lower weft(22) to prepare a lower surface; a step of crossing warp and the lower weft and crossing the lower warp and the upper weft to prepare a girth; and a step of crossing the upper weft(12) and the lower warp, and the lower weft and the upper warp to prepare a pattern side.
124 그물망의 직조방법 및 그의 직조물 KR1020070089231 2007-09-04 KR1020090024312A 2009-03-09 차용철; 박상구
A weaving method for a mesh net and weaving fabric thereby are provided to improve intensity of a contact point by processing plain weaving with organization of the respective contact point of rib. A weaving method for a mesh net comprises the following steps of: picking a weft in intersection space formed by movement of leno weaves, plain weave, and heedles(201a, 201b, 201c, 201d, 201e, 201f, 201g) to up and down; picking a b weft in shed space formed by movement of plane heedles of a weaving 2 process; picking a c weft in the shed space formed by movement of plane heedles of a weaving 3 process; picking a d weft in the intersection space on a right side of a weaving 4 process; picking an e weft in the space of a weaving 5 process; and picking an f weft in the space of a weaving 6 process.
125 보호 구조의 형성을 위한 이중 직물 KR1020050114819 2005-11-29 KR1020070056320A 2007-06-04 조정문
A double cloth for forming a protection structure is provided to maintain the air at the inside during the constant time, thereby absorbing or relieving the external impact. The double cloth includes a double cloth layer(11) for forming an expansion portion. A signal cloth layer(12) forms a combination portion. A coating layer is formed at the inside, outside or middle of the double cloth layer. The strength of the double cloth layer or signal cloth layer is at least 2.0 Kgf. The coating layer is formed by coating agent of curable elastic polymer with the viscosity of 5,000 to 50,000 and the amount of coating is 120 g/m^2 to 150 g/m^2. The double cloth layer or signal cloth layer is one selected from a group consisting of polyamide 66, aromatic polyamide, polyester and polyethylene fibers.
126 INTEGRATED OPEN BOX-LIKE WOVEN FABRIC EP16168353.7 2016-05-04 EP3091109B1 2018-08-29 Tsai, Li-Ju
An open box-like woven fabric includes two inner walls (213) connected transversely between two outer walls (212), and a base wall (211) connected to the outer and inner walls (212, 213) oppositely of a top opening (214) formed between the outer and inner walls (212, 213). Each outer wall (212) has an outwardly extending side extension (2121), and the base wall (211) has an outwardly extending bottom extension (2111). The open box-like woven fabric is formed from a novel flattened fabric preform (20).
127 THREE-DIMENSIONAL WOVEN COMPOSITE VEHICLE COMPONENTS FOR CRASHWORTHINESS EP16770816.3 2016-09-01 EP3344809A1 2018-07-11 BAYRAKTAR, Harun, H.; STEVENSON, Michael, Brent
Described is a three-dimensional (3D) woven composites with high specific energy absorption (SEA) that significantly outperforms traditional two dimensional (2D) woven laminated composites of substantially the same weight.
128 INTEGRATED OPEN BOX-LIKE WOVEN FABRIC EP16168353.7 2016-05-04 EP3091109A3 2017-01-11 Tsai, Li-Ju

An open box-like woven fabric includes two inner walls (213) connected transversely between two outer walls (212), and a base wall (211) connected to the outer and inner walls (212, 213) oppositely of a top opening (214) formed between the outer and inner walls (212, 213). Each outer wall (212) has an outwardly extending side extension (2121), and the base wall (211) has an outwardly extending bottom extension (2111). The open box-like woven fabric is formed from a novel flattened fabric preform (20).

129 PRÉFORME FIBREUSE D'UNE AUBE DE TURBOMACHINE EN MATÉRIAU COMPOSITE À PLATE-FORME INTEGRÉE, ET SON PROCÉDÉ DE RÉALISATION EP13701834.7 2013-01-07 EP2802701B1 2016-11-16 MARCHAL, Yann; COUPE, Dominique; MAHIEU, Jean-Noël; DAMBRINE, Bruno, Jacques, Gérard
130 Method for producing a component for connecting structures and device EP12188065.2 2012-10-11 EP2581200B1 2016-07-27 Seack, Oliver; Bruns, Alexander
Producing component for connecting structures at crossing regions of the component, comprises depositing first fibers (212) and second fibers (214) on a base such that a respective first fiber with respect to a respective second fiber exhibits an offset in a longitudinal direction (306) of the first or the second fiber, connecting the first and the second fibers along an overlap region (412), in which the first and the second fibers overlaps, and pivoting the first and the second fibers with each other to form the component. Independent claims are also included for: (1) producing a structural assembly, preferably for an aircraft or spacecraft, comprising (i) providing a first structure, (ii) providing a second structure exhibiting the crossing region with the first structure, (iii) producing the component by the above method, and (iv) connecting the first and the second structures in the crossing region by the component; and (2) a device for producing the above component, comprising the base, a depositing device for depositing the first and the second fibers on the base such that the respective first fiber with respect to the respective second fiber exhibits the offset in the longitudinal direction of the first or the second fiber, a connecting device for connecting the first and the second fibers along the overlap region, in which the first and the second fibers overlap, and a pivoting device for pivoting the first and the second fibers with each other to form the component.
131 THREE-DIMENSIONAL WOVEN CORNER FITTING WITH LAP JOINT PREFORMS EP13812311.2 2013-12-04 EP2938766A1 2015-11-04 MCCLAIN, Michael; GOERING, Jonathan
A three-dimensional corner lap joint preform and a method of forming a three- dimensional corner lap joint preform including a woven flange with one or more legs that extend from the flange. The legs may include one or more independently woven portions which allow formation of a corner without darting the leg or adding additional reinforcement. The independently woven portions may include warp fibers which are not woven into the preform. The unwoven area al lows removal of a portion of the leg prior to formation of the corner, allowing the portions of the leg to overlap and form a lap joint.
132 PREFORME FIBREUSE D'UNE AUBE DE TURBOMACHINE EN MATERIAU COMPOSITE A PLATE-FORME INTEGREE, ET SON PROCEDE DE REALISATION EP13701834.7 2013-01-07 EP2802701A2 2014-11-19 MARCHAL, Yann; COUPE, Dominique; MAHIEU, Jean-Noël; DAMBRINE, Bruno, Jacques, Gérard
The invention relates to a method for producing a fibrous preform for the manufacture of a turbomachine blade made of composite material, the method involving using three-dimensional weaving to create a fibrous rough form (100) in a single piece with layers of longitudinal threads (c 1 to c 24) joined together by threads of layers of transverse threads (t 1 to t 24), and shaping the fibrous rough form to obtain a fibrous preform in a single piece having a part that forms the aerofoil preform and at least a part that forms a platform preform. During the course of the weaving process, the threads (c 5 to c 7) of a first group of longitudinal threads are led out from the fibrous rough form on the side of one of the lateral faces (110a) of the rough form to form a part (120) that corresponds to a preform of a blade platform, and threads (c 3 and c 4) of a second group of longitudinal threads are injected into the fibrous rough form with mutual criss-crossing between the threads of the first group and the threads of the second group. The invention also relates to a preform obtained using this method.
133 BALLOON WITH DIVIDING FABRIC LAYERS AND METHOD FOR BRAIDING OVER THREE-DIMENSIONAL FORMS EP07869384.3 2007-12-17 EP2101858B1 2014-07-16 SIMPSON, Charles L.
A medical balloon with a variable diameter that is reinforced with continuous fibers woven to form a fabric with a varying number of layers and fiber densities. Portions of the balloon having a relatively smaller diameter are reinforced with a fabric having a reduced fiber density and an increased number of layers to facilitate the placement of the layers. The fabric also includes a braiding pattern that facilitates the transition from a single layer fabric to a multiple layer fabric. Also described is a manufacturing method for the braiding and layering.
134 NON-KINKING SELF-WRAPPING WOVEN SLEEVE AND METHOD OF CONSTRUCTION THEREOF EP11749649.7 2011-08-16 EP2606168B1 2014-03-26 MALLOY, Cassie
135 NAHTKONSTRUKTION FUR EIN GEWEBE EP07724937.3 2007-05-07 EP2016216B1 2011-02-23 BECKER, Michael; ESCHBACH, Thomas; ENDERLEIN, Andreas
Seam construction for a woven fabric for an OPW airbag, in particular for person restraint systems, which seam construction is characterized by a weaving seam (Ia) having a single-layer region which is surrounded by an at least two-layer region (6), the individual layers of which have in each case a looser woven structure than the single-layer region.
136 BALLOON WITH DIVIDING FABRIC LAYERS AND METHOD FOR BRAIDING OVER THREE-DIMENSIONAL FORMS EP07869384.3 2007-12-17 EP2101858A2 2009-09-23 SIMPSON, Charles L.
A medical balloon with a variable diameter that is reinforced with continuous fibers woven to form a fabric with a varying number of layers and fiber densities. Portions of the balloon having a relatively smaller diameter are reinforced with a fabric having a reduced fiber density and an increased number of layers to facilitate the placement of the layers. The fabric also includes a braiding pattern that facilitates the transition from a single layer fabric to a multiple layer fabric. Also described is a manufacturing method for the braiding and layering.
137 NAHTKONSTRUKTION FUR EIN GEWEBE EP07724937.3 2007-05-07 EP2016216A1 2009-01-21 BECKER, Michael; ESCHBACH, Thomas; ENDERLEIN, Andreas
Seam construction for a woven fabric for an OPW airbag, in particular for person restraint systems, which seam construction is characterized by a weaving seam (Ia) having a single-layer region which is surrounded by an at least two-layer region (6), the individual layers of which have in each case a looser woven structure than the single-layer region.
138 Design tape EP03252340.9 2003-04-11 EP1354989B1 2007-03-21 Arai, Shintaro
139 TISSU CHAINE ET TRAME A BASE DE FILS TECHNIQUES MULTIFILAMENTS A PREDOMINANCE SANS TORSION ET PROCEDE D'OBTENTION EP94900890.0 1993-11-30 EP0670921A1 1995-09-13 AUCAGNE, Jean Pierre-Blanche; BOMPARD, Bruno; BRUYERE, Alain; DEBAILLE, Christian; GERMAIN, Bertrand; LAMARIE, Jean-Paul; MARTINET, Laurent; PERRET, Franck; VEAUVILLE, Jean-François
A warp and weft fabric based on multifilament yarn. At least 80 wt % of the yarn has a combination of the following features: (a) the yarn count, for a given fabric substance, is greater than the conventional yarn count; (b) the yarn twist is no greater than the original twist of the yarn prior to weaving, which yarn, in an equal proportion, has 0 twists per metre; (c) the yarn width over the whole yarn length is at least as great as the original yarn width prior to weaving. Said yarn constitutes all the yarn in the direction comprising the majority by weight of the yarn when the weight ratio of weft yarn to warp yarn is at least 80/20, and all the fabric yarn when said ratio is below 80/20, and the fibre volume ratio is substantially constant in the fabric and at least as high as the volume ratio in a conventional fabric based on yarn with the same or a lower count.
140 Three dimensional woven fabric connector EP86106650.4 1986-05-15 EP0245533B1 1990-10-10 Abildskov, Dale
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