| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 1 | 棒、垒球的球皮成型的制造方法 | CN201310424729.7 | 2013-09-17 | CN104339666A | 2015-02-11 | 陈锡铭 |
| 一种棒、垒球的球皮成型的制造方法，其是先将一球芯独立成型；接着，在该球芯的外表面上固定一层具一定厚度作为底材的纤维材质，并在该纤维材质层上均匀饱和地注入一层液体聚氨酯(Polyurethane)，再将该球芯放置于两半球形模体或两片8字形模体的球皮模具中；然后，加温熟成而固化成型，最后脱模形成整个球体；借此，利用在独立成型的球芯上，形成一内包裹有纤维材质的聚氨酯的复合层球皮，使在球皮成型后，具有牛皮一般的强度，经过一段时间的猛力打击后，球皮不会变形、松脱、磨损、或撕裂，借以显著地提高球体的耐用性，令使用寿命延长。 | ||||||
| 2 | 用于飞机轮胎的胎冠增强件 | CN201480060666.4 | 2014-11-06 | CN105705343A | 2016-06-22 | M·罗梅罗德拉奥萨; S·德拉克鲁瓦 |
| 本发明涉及飞机轮胎，特别涉及用于飞机轮胎的胎冠增强件。飞机轮胎(1)包括：工作增强件(2)，所述工作增强件(2)沿径向位于胎面(3)的内部并且沿径向位于胎体增强件(4)的外部。所述工作增强件(2)包括至少两个工作双层(21、22)，所述工作双层(21、22)沿径向重叠并且各自具有从第一轴向端部(I1、I2)至第二轴向端部(I’1、I’2)的轴向宽度(L1、L2)。每个工作双层(21、22)至少部分地包括两个工作层(211、212；221、222)，所述工作层(211、212；221、222)沿径向重叠并且各自由条带部分(5)的在轴向上并置制成。具有轴向宽度W的所述条带(5)沿着周期性曲线(6)周向地延伸，所述周期性曲线(6)在轮胎的赤道平面(XZ)中与轮胎的周向方向(XX’)形成非零角度A并且在其极值(7)处具有曲率半径R。本发明人的目的是通过降低工作层的轴向端部额外厚度对开裂的敏感度而改进飞机轮胎的工作增强件的耐久性。根据本发明，至少两个沿径向重叠的工作双层(21、22)的各自的轴向宽度(L1、L2)之间的差异DL至少等于2×(W+(R-W/2)×(1-cosA))。 | ||||||
| 3 | 蜡烛盒 | CN201410121348.6 | 2014-03-28 | CN104419527A | 2015-03-18 | 莉迪亚·卡勒弗曼; 安德里亚·施泰因迈尔; 莱内特·因德波森 |
| 本发明涉及一种具有多个深冲压的杯状结构的蜡烛盒，在各种情况下，该杯状结构中设置有由易燃材料和烛芯组成的蜡烛。本发明还涉及一种蜡烛、一种用于制造蜡烛或蜡烛盒的方法以及一种深冲压装置。 | ||||||
| 4 | METHOD FOR MANUFACTURING A SINGLE BELT/OVERLAY COMPONENT FOR A PNEUMATIC TIRE | US14950734 | 2015-11-24 | US20170144400A1 | 2017-05-25 | Gilles BONNET; Vaidyanathan SANKAR; Phaniraj MUTHIGI; Steven Kris Herman LAERMANS; David Ray HUBBELL; Joseph Henry LACO |
| A method in accordance with the present invention manufactures a tire with a biaxial monolayer belt component (MBC). The method comprises the steps of: winding a cord continuously about a first drum according to a pre-defined pattern to create a mesh of cords defining a single belt/overlay structure; adjusting the structure to a predetermined position on the first drum by laser lights; applying a tread component to the structure; transferring the structure and tread component to a second drum; applying the structure and tread component to a carcass component on the second drum; reducing pressure of the carcass component by a predetermined amount; and stitching the structure and tread component to the carcass component. | ||||||
| 5 | CANDLE CARTRIDGE | US14913155 | 2014-08-21 | US20160201899A1 | 2016-07-14 | Lydia KLEFFMANN; Andrea STEINMEIER; Linette INDERBIETHEN |
| A candle magazine has a multiplicity of deep-drawn cup-like structures in which there is provided in each case one candle composed of a combustible material and of a wick. A candle, method for producing a candle or a candle magazine, and a deep-drawing apparatus are also provided. | ||||||
| 6 | 航空機用タイヤのためのクラウン補強材 | JP2016530957 | 2014-11-06 | JP2016540679A | 2016-12-28 | デ ラ オサ マルク ロメロ; セルジュ ドラクロワ |
| 本発明は、航空機用タイヤに関し、より具体的には、航空機用タイヤのクラウン補強材に関する。航空機用タイヤ(1)は、トレッド(3)の半径方向内側及びカーカス補強材(4)の半径方向外側にあるワーキング補強材(2)を含む。ワーキング補強材(2)は、半径方向に重ね合わせられ、それぞれ、第1の軸方向端部(I1、I2)から第2の軸方向端部(I’1、I’2)までの軸方向幅(L1、L2)を有する、少なくとも2つのワーキングバイプライ(21、22)を含む。ワーキングバイプライ(21、22)の各々は、少なくとも部分的に、半径方向に重ね合わせられ、それぞれ、ストリップ(5)の部分の軸方向並置で構成される2つのワーキング層(211、212;221、222)を含む。軸方向幅Wのストリップ(5)は、タイヤの赤道面(XZ)において、タイヤの周方向(XX’)に対して、ゼロでない角度Aを形成し、かつ、その極値(7)において曲率半径Rを有する周期曲線(6)をなして周方向に延びる。本発明者らは、亀裂のリスクに対してあまり敏感でないワーキング層の軸方向端部厚さ付加部を作製することによって、航空機用タイヤのワーキング補強材の耐久力を改善することを目的に定める。本発明によると、少なくとも2つの半径方向に重ね合わせられたバイプライ(21、22)のそれぞれの軸方向幅(L1、L2)の間の差DLは、少なくとも2×(W+(R−W/2)×(1−cosA))に等しい。【選択図】図1 | ||||||
| 7 | Method for producing a hybrid composite component from organo sheets and a metallic reinforcing element | US14886012 | 2015-10-17 | US09914248B2 | 2018-03-13 | David Preisser |
| A method for producing a hybrid composite component from organo sheets and a metallic reinforcing element in such a way that the method may be inexpensively and simply performed and the hybrid composite component has the lowest possible weight and may absorb relatively high forces. | ||||||
| 8 | Crown Reinforcement For An Aircraft Tire | US15036608 | 2014-11-06 | US20160288576A1 | 2016-10-06 | Marc ROMERO DE LA OSA; Serge DELACROIX |
| Crown reinforcement of an aircraft tire comprises a working reinforcement (2) radially inside of tread (3) and radially outside of carcass reinforcement (4). Working reinforcement (2) comprises two working bi-plies (21, 22) radially superposed with respective axial widths (L1, L2), from first axial end (I1, I2) to second axial end (I′1, I′2). Each working bi-ply (21, 22) comprises two working layers (211, 212; 221, 222) radially superposed and respectively made up of axially juxtaposed portions of strip (5) of axial width W extending circumferentially in periodic curve (6) that forms, in the equatorial plane (XZ) of the tire and with the circumferential direction (XX′) of the tire, a non-zero angle A and has a radius of curvature R at its extrema (7). The difference DL between the respective axial widths (L1, L2) of the radially superposed working bi-plies (21, 22) is at least equal to 2×(W+(R−W/2)−(1−cos A)). | ||||||
| 9 | SHAPED PART, TRIM PART FOR VEHICLE INTERIORS, AND DEVICE AND PROCESS FOR PRODUCING THE SHAPED PART | US14969912 | 2015-12-15 | US20160167596A1 | 2016-06-16 | Guillaume BASQUIN; Valentin GEOFFROY |
| A shaped part for a trim part for vehicle interiors with a support made of a mat that contains fibers. The support includes a recess on a visible side that extends in longitudinal direction, and a protrusion on a back side that extends in longitudinal direction and corresponds with the recess on the visible side. The shaped part includes a plastic layer positioned in the area of the recess that is formed from a material other than the mat and that is firmly bonded to the recess. A device for the production of the shaped part as well as a procedure for the production of the shaped part are provided. | ||||||
| 10 | VERFAHREN ZUM HERSTELLEN EINES HYBRID-VERBUNDBAUTEILS AUS ORGANOBLECHEN UND EINEM METALLISCHEN VERSTÄRKUNGSELEMENT | EP15176972.6 | 2015-07-16 | EP3009249B1 | 2018-11-21 | PREISSER, David |
| 11 | VERFAHREN ZUM HERSTELLEN EINES HYBRID-VERBUNDBAUTEILS AUS ORGANOBLECHEN UND EINEM METALLISCHEN VERSTÄRKUNGSELEMENT | EP15176972.6 | 2015-07-16 | EP3009249A1 | 2016-04-20 | PREISSER, David |
Die Erfindung betrifft ein Verfahren zum Herstellen eines Hybrid Verbundbauteils (V2) aus ersten und zweiten Organoblechen (2a, 2b) und einem metallischen Verstärkungselement (3). Dieses soll derart weitergebildet werden, dass das Verfahren kostengünstig und einfach realisierbar, das Hybrid Verbundbauteil ein möglichst geringes Gewicht aufweist und die herzustellende Bauteilverbindung höhere Kräfte aufnehmen kann. Dies wird durch die folgenden Verfahrensschritte erreicht: a) Bereitstellen von ersten und zweiten Organoblechen (2a, 2b) sowie eines mit einer Anzahl Durchgangsbohrungen (5) versehenen metallischen Verstärkungselementes (3), b) Einlegen des ersten Organoblechs (2b) in eine erste Formhälfte (10a) einer Werkzeugform sowie Einlegen des zweiten Organoblechs (2a) in eine zweite Formhälfte (10b) der Werkzeugform, c) Einlegen des metallischen Verstärkungselements (3) auf das erste Organoblech (2b), d) Schließen der Werkzeugform unter Beaufschlagung eines Drucks, um eine stoffschlüssige Verbindung der Bereiche der Organobleche (2a, 2b) zu erreichen, die unmittelbar aufeinanderliegen, e) Einspritzen eines thermoplastischen Kunststoffmaterials (6) in einen zwischen einem Organoblech (2b) und zugeordneter Formhälfte (10b) freigehaltenen Formspalt, wobei das Kunststoffmaterial (6) ein Anschmelzen des Organoblechs in dem Formspalt zugewandten Oberflächenbereich sowie ein Durchströmen der Organobleche 2a, 2b im Bereich der Anzahl Durchgangsbohrungen (5) und ein Befüllen der Anzahl Durchgangsbohrungen (5) des metallischen Verstärkungselements (3) bewirkt, wobei eine stoffschlüssige Verbindung zwischen dem Kunststoffmaterial (6) und den Organoblechen (2a, 2b) und eine formschlüssige Verbindung zwischen Kunststoffmaterial (6) den Organoblechen 2a, 2b und dem metallischen Verstärkungselement (3) bewirkt wird; und f) Öffnen der Werkzeugform und Herausnehmen des Hybrid Verbundbauteils (V2).
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| 12 | ARMATURE DE SOMMET POUR PNEUMATIQUE D'AVION | EP14798749.9 | 2014-11-06 | EP3068633B1 | 2018-03-28 | ROMERO DE LA OSA, Marc; DELACROIX, Serge |
| 13 | ARMATURE DE SOMMET POUR PNEUMATIQUE D'AVION | EP14798749.9 | 2014-11-06 | EP3068633A1 | 2016-09-21 | ROMERO DE LA OSA, Marc; DELACROIX, Serge |
| The present invention relates to an aircraft tyre, and in particular the crown reinforcement for an aircraft tyre. An aircraft tyre (1) comprises a working reinforcement (2) radially inside a tread (3) and radially outside a carcass reinforcement (4). The working reinforcement (2) comprises at least two working bilayers (21, 22), which are radially superimposed and respectively have an axial width (L 1, L 2) from a first axial end (I1, I2) to a second axial end (I'1, I'2). Each working bilayer (21, 22) at least partially comprises two working layers (211, 212; 221, 222), which are radially superimposed and respectively made up of an axial juxtaposition of band portions (5). The band (5), with axial width W, extends circumferentially along a periodic curve (6), forming a non-zero angle A in the equatorial plane (XZ) of the tyre and with the circumferential direction of the tyre (XX') and having a radius of curvature R at its extrema (7). The inventors' aim was to improve the endurance of the working reinforcement of an aircraft tyre by making the axial end overthicknesses of the working layers less sensitive to cracking. According to the invention, the difference DL between the respective axial widths (L 1, L 2) of the at least two radially superimposed working bilayers (21, 22) is at least equal to 2*(W+(R-W/2)*(1-cosA)). | ||||||
| 14 | Shaped part, trim part for vehicle interiors, and device and process for producing the shaped part | US14969912 | 2015-12-15 | US10035474B2 | 2018-07-31 | Guillaume Basquin; Valentin Geoffroy |
| A shaped part for a trim part for vehicle interiors with a support made of a mat that contains fibers. The support includes a recess on a visible side that extends in longitudinal direction, and a protrusion on a back side that extends in longitudinal direction and corresponds with the recess on the visible side. The shaped part includes a plastic layer positioned in the area of the recess that is formed from a material other than the mat and that is firmly bonded to the recess. A device for the production of the shaped part as well as a procedure for the production of the shaped part are provided. | ||||||
| 15 | STITCHLESS BULK BAG WITH HEAT FUSED SEAMS AND METHOD OF PRODUCTION | US15807272 | 2017-11-08 | US20180126661A1 | 2018-05-10 | Clifford DUNLAP; Daniel R. SCHNAARS, SR.; Brody Alan VIATOR; Daniel SCHNAARS, JR. |
| A stitchless highly oriented polypropylene fabric bulk bag of the type that can hold 500 to 5000 pounds (226.7 to 2268 kilograms) of bulk material includes a highly oriented polypropylene fabric top, body and bottom, with a heat fused joint providing an air tight connection between the top and body, and another air tight heat fused joint connecting the body and bottom. A fill spout and discharge tube may also be provided with an air tight heat fused joint connecting the fill spout to the top and another air tight heat fused joint connecting the discharge spout to the bottom. Heat sealing machinery include heat seal bar assemblies that can self-align during heat-sealing to apply even pressure to all areas being heat sealed. A heating element is of single piece construction and can include end coupler portions as part of the single piece construction. Carrier plates used in a heat-sealing assembly line guide parts placement, provide quality checks for parts placement, and tooling set-up for machinery. | ||||||
| 16 | Deflecting Member for Making Fibrous Structures | US15795339 | 2017-10-27 | US20180119351A1 | 2018-05-03 | John Leslie Brent, JR.; James Michael Singer; John Allen Manifold; Eric James Watkins; Mario Castillo |
| A deflection member that includes a reinforcing member that includes a resin coating, and at least one tile fastened to the resin coating. | ||||||
| 17 | Deflecting Member for Making Fibrous Structures | US15795329 | 2017-10-27 | US20180119350A1 | 2018-05-03 | John Leslie Brent, JR.; James Michael Singer; John Allen Manifold; Eric James Watkins; Mario Castillo |
| A deflection member that includes a reinforcing member and a plurality of tiles fastened to the reinforcing member. | ||||||
| 18 | PROTECTIVE COVERING FOR WOOD PRODUCTS | US15342644 | 2016-11-03 | US20170120503A1 | 2017-05-04 | Trevor Arthurs |
| Protective coverings herein have a coated woven material with a first edge parallel with a warp direction and a second edge opposite the first edge, and have a first edge band proximate the first edge and a second edge band proximate the second edge. The coated woven material has a woven scrim made of a plurality of weft tapes and a plurality of warp tapes, but the warp tapes positioned in the first and second edge bands are high-shrinkage warp tapes and the warp tapes positioned in between the first and second edge bands have a shrinkage that is less than a shrinkage of the high-shrinkage warp tapes, and has a coating on at least one major surface of the woven scrim. The plurality of high-shrinkage warp tapes shrink upon application of heat. Methods of covering a load, such as stacked lumber, with the protective covering are also disclosed. | ||||||
| 19 | METHOD FOR PRODUCING A HYBRID COMPOSITE COMPONENT FROM ORGANO SHEETS AND A METALLIC REINFORCING ELEMENT | US14886012 | 2015-10-17 | US20160107348A1 | 2016-04-21 | David PREISSER |
| A method for producing a hybrid composite component from organo sheets and a metallic reinforcing element in such a way that the method may be inexpensively and simply performed and the hybrid composite component has the lowest possible weight and may absorb relatively high forces. | ||||||
| 20 | CANDLE MAGAZINE | US14227513 | 2014-03-27 | US20150056562A1 | 2015-02-26 | Lydia KLEFFMANN; Andrea STEINMEIER; Linette INDERBIETHEN |
| A candle magazine has a multiplicity of deep-drawn cup-like structures in which there is provided in each case one candle composed of a combustible material and of a wick. A candle, a method for producing a candle or a candle magazine, and a deep-drawing apparatus are also provided. | ||||||
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