| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 21 | 一种耐水航空胶合板 | CN201510868856.5 | 2015-12-01 | CN105500473A | 2016-04-20 | 李上; 王青山; 阳建新; 梁德芳; 陈润; 朗建昭; 刘波林 |
| 本发明涉及一种耐水航空胶合板，包括航空胶合板本体(1)，聚丙烯酸树脂涂层(2)和酚醛树脂涂层(3)。所述的航空胶合板本体(1)是桦木胶合板。所述聚丙烯酸树脂涂层(2)包裹于航空胶合板本体(1)周身，酚醛树脂涂层(3)包裹聚丙烯酸树脂涂层(2)。所述的聚丙烯酸树脂涂层(2)的厚度为0.1～0.3mm，酚醛树脂涂层(3)厚度为0.15～0.25mm。本发明是一种造价便宜，外观材质高贵，耐水性能好的航空胶合板。 | ||||||
| 22 | CIT实验室用耐腐蚀耐高温理化板 | CN201510968911.8 | 2015-12-17 | CN105440573A | 2016-03-30 | 盛义良 |
| 本发明公开了一种CIT实验室用耐腐蚀耐高温理化板，包括：理化基材、胶黏剂和通过胶黏剂粘合在理化基材上的理化膜；其中理化膜的原料按重量份包括：苏籽油改性酚醛树脂72～75份，丙烯酸树脂25～28份，醇酸树脂17～20份，棉纤维17～20份，碳化硼纤维3～4份，膨胀珍珠岩13～16份，滑石粉15～18份，煅烧高岭土14～17份，磷酸三甲苯酯1.7～1.9份，环氧苍耳油酸丁酯3～6份，丙烯腈-丁二烯-苯乙烯共聚物2～4份，氯化聚乙烯1～2份，氢氧化镁15～18份，微胶囊化红磷5～8份，硼酸锌7～10份，防老剂2.2～2.5份。本发明具有优异的耐腐蚀耐高温性能，而且韧性和耐水性能优秀，满足实验柜的实际需求。 | ||||||
| 23 | 稳定性好的碳膜板 | CN201510340956.0 | 2015-06-18 | CN105015093A | 2015-11-04 | 赵晶凯 |
| 稳定性好的碳膜板，本发明涉及碳膜板技术领域，它包含基板、碳膜层；基板的上部设有碳膜层；所述的基板由酚醛纸压板和树脂层构成；酚醛纸压板的外壁上设有树脂层，能够解决在使用过程中出现的微短路现象，大大降低了售后工作量，延长了其使用寿命。 | ||||||
| 24 | 碾平竹木复合集装箱底板用胶合板及其生产工艺 | CN201510237870.5 | 2015-05-11 | CN104827528A | 2015-08-12 | 廖志远 |
| 本发明公开了一种碾平竹木复合集装箱底板用胶合板，包括酚醛覆膜纸、木长中板、木短中板、长中碾平竹板、竹帘短中板；在该上端面与下端面之间沿所述上端面朝向下端面的方向上依次设置有第一块木长中板、第一块木短中板、第一块长中碾平竹板、第二块木长中板、第一块竹帘短中板、第三块木长中板、第二块木短中板、第四块木长中板、第二块长中碾平竹板、第五块木长中板、第三块木短中板、第六块木长中板、第二块竹帘短中板、第七块木长中板、第三块长中碾平竹板、第四块木短中板和第八块木长中板。本发明碾平竹木复合集装箱底板用胶合板强度高、使用寿命长。 | ||||||
| 25 | 耐燃层压板 | CN201180045486.5 | 2011-09-21 | CN103221214A | 2013-07-24 | 杰拉德·乌尔里希; 米夏埃尔·霍瓦斯; 米夏埃尔·凯泽尔; 克劳斯·弗雷德里希·戈莱奇 |
| 本发明描述了耐燃层压板，其本身特征在于根据ISO 1716，它具有≤3MJ/kg的低热值，并且得益于它特殊的多层结构而具有出色的机械特性和在气候条件变化（热/湿/冷/干）下的杰出稳定性。本发明的层压板包含几种具有不同功能性和组分的矿物纤维和玻璃纤维织物。这包括高填充织物、B-阶段粘合剂及其他添加剂。所述层压板的高度机械强度以及在气候条件变化（热/湿/冷/干）下的杰出稳定性使得可将它有效用于至今只能使用EN 438层压板的许多领域及更多领域中。 | ||||||
| 26 | 复合材料的金属镀层 | CN200780046450.2 | 2007-12-06 | CN101600817A | 2009-12-09 | 托马斯·约瑟夫·科登; 马克·雷蒙德·斯蒂尔 |
| 一种制造复合件以及将金属镀层固定到树脂基复合材料上的方法，包括在金属电镀预制件上提供咬合结构以及将咬合结构和复合材料在引起复合材料与咬合结构互锁的条件下放在一起。本发明也提供复合件(10)，其包括树脂基复合材料(12)，其表面或部分表面(16)具有金属镀层(14)，金属镀层(14)包括外部电镀预制件和内部咬合结构(20)，内部咬合结构(20)通常位于所述电镀预制件(18)和复合材料(12)之间，以提供在复合材料(12)上电镀预制件(18)的附着。 | ||||||
| 27 | Method of producing crystalline substrate having concave-convex structure | US14395151 | 2012-08-09 | US09306137B2 | 2016-04-05 | Susumu Takada; Emi Kuraseko; Motoyuki Suzuki |
| A method of producing the crystalline substrate having a concave-convex structure includes: (A) forming a transfer film by forming a concave-convex film on a support film on the surface having a concave-convex pattern thereon so that thickness of the residual film of the concave-convex film is 0.01 to 1 μm, the concave-convex pattern of the support film having concave parts with a width of 0.05 to 100 μm, a depth of 0.05 to 10 μm, and a ratio of the depth of the concave part to the width of the concave part of up to 1.5, (B) disposing the transfer film on the crystalline substrate, and transferring the concave-convex film onto the crystalline substrate to produce a crystalline substrate having the concave-convex film thereon, (C) etching the crystalline substrate having the concave-convex film thereon to form a concave-convex structure on the surface of a crystalline substrate. | ||||||
| 28 | METHOD OF PRODUCING CRYSTALLINE SUBSTRATE HAVING CONCAVE-CONVEX STRUCTURE | US14395151 | 2012-08-09 | US20150097204A1 | 2015-04-09 | Susumu Takada; Emi Kuraseko; Motoyuki Suzuki |
| A method of producing the crystalline substrate having a concave-convex structure includes: (A) forming a transfer film by forming a concave-convex film on a support film on the surface having a concave-convex pattern thereon so that thickness of the residual film of the concave-convex film is 0.01 to 1 μm, the concave-convex pattern of the support film having concave parts with a width of 0.05 to 100 μm, a depth of 0.05 to 10 μm, and a ratio of the depth of the concave part to the width of the concave part of up to 1.5, (B) disposing the transfer film on the crystalline substrate, and transferring the concave-convex film onto the crystalline substrate to produce a crystalline substrate having the concave-convex film thereon, (C) etching the crystalline substrate having the concave-convex film thereon to form a concave-convex structure on the surface of a crystalline substrate. | ||||||
| 29 | Method for the production of bearing materials, bearing materials produced by said methods and use of said bearing materials | US10490923 | 2002-09-24 | US20050019490A1 | 2005-01-27 | Achim Adam; Stefan Fuchsberger; Joachim Schluter |
| A method for the production of bearing materials is disclosed, in which a strip of a metallic woven support is continuously provided with a slip layer mostly comprising polytetrafluoroethylene (PTFE), covering one side thereof. The woven support is coated on one side with a paste of the material for the slip layer, whereby the woven support runs with the lower surface thereof in full-surface contact with a roller during and directly after the coating. | ||||||
| 30 | Laminate for use as outer covering of battery and secondary battery | US10487408 | 2004-08-13 | US20040265688A1 | 2004-12-30 | Hideki Arao; Masashi Hiromitsu; Takakazu Goto; Kazuya Tanaka; Akio Shimizu; Ryoji Morita |
| The present invention relates to a laminate for battery encasement comprising aluminum foil and an inner layer, wherein a resin film layer that comprises an aminated phenol polymer (A), an acrylic polymer (B), a phosphorus compound (C), and a zirconium compound (D) lies between the aluminum foil and the inner layer. The laminate for battery encasement of the present invention is excellent in adhesiveness, gas impermeability, etc., and therefore can be suitably used as a material for encasing a secondary battery, particularly a lithium ion polymer secondary battery. | ||||||
| 31 | Ballistic resistant and fire resistant composite articles | US10287929 | 2002-11-05 | US20040086729A1 | 2004-05-06 | Huy X. Nguyen; Larry Dickson |
| Ballistically resistant and fire resistant composite articles for aircraft interiors and other applications. Composite articles are provided having a flexural modulus of at least about 80,000 lbs/sq in (552 MPa), a flexural strength at yield of at least about 800 lbs/sq. in. (5.52 MPa), an areal density of about 0.9 lb/ft2 (4.40 kg/m2) to about 1.5 lb/ft2 (5.86 kg/m2), a fire resistance meeting the requirements of null25.853 Title 14 of the United States Code, Jan. 1, 2002, and a V0 velocity of at least about 1430 ft/sec (427 m/s) when tested by United States Federal Aviation Administration Advisory Circular 25.795.2, Jan. 10, 2002, using .44 Magnum Jacketed Hollow Point (JHP) bullets of 240 grains (15.6 g) mass and using 9 mm Full Metal Jacketed, Round Nose (FMJ RN) bullets of 124 grains (8.0 g) mass. | ||||||
| 32 | Encapsulated lens retroreflective sheeting | US09824347 | 2001-04-02 | US06586067B2 | 2003-07-01 | Seth Levenstein |
| Encapsulated-lens retroreflective sheeting is described which contains an improved binder layer. The binder layer is obtained from a film-forming mixture which comprises: (A) a vinyl chloride copolymer, (B) a thermoplastic polyurethane, and (C) an aminoplast resin. Such binder layer exhibits improved adhesion to metallized beads and to a variety of cover films such as acrylic films. | ||||||
| 33 | Vacuumized plastic cap for heat insulating containers | US38974873 | 1973-08-20 | US3856172A | 1974-12-24 | WALLES W |
| Heat insulative properties of vacuum containers such as vacuum bottles are significantly improved by stoppering the container with a vacuumized plastic cap having a boundary wall of structural plastic material wherein the inner surface of the boundary wall is coated with a thin metallic layer and a layer of barrier plastic such as a vinylidene chloride copolymer and which encloses an evacuated space filled with a gas absorbing material such as activated charcoal.
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| 34 | Metal substrates bonded with thermosetting resin compositions containing fibrillated polytetrafluoroethylene | US26584872 | 1972-06-23 | US3853690A | 1974-12-10 | MCGARRY F; SUEN T |
| Various substrates are bonded together with adhesives comprising a thermosetting resin containing from about 1 percent to about 40 percent of polytetrafluoroethylene. The resultant articles exhibit excellent structural properties and find use in such areas as the aerospace industry.
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| 35 | Heat insulating container having plastic walls retaining vacuum | US30545172 | 1972-11-10 | US3828960A | 1974-08-13 | WALLES W |
| A container having a double wall construction of a structural plastic material is provided with improved thermal insulative properties by (1) metallizing at least one surface of each wall of the container with metal such as silver to provide a light reflective surface and to produce a partial barrier to atmospheric gases, (2) coating the metallized surface with a barrier plastic such as saran, (3) evacuating the space enclosed by the walls of the container, and (4) adding to the evacuated space a gas-absorbing material.
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| 36 | Flame resistant laminate | US13820818 | 2011-09-21 | US09650783B2 | 2017-05-16 | Gerald Ullrich; Michael Horvath; Michael Ketzer; Klaus Friedrich Gleich |
| A flame resistant laminate is described, which distinguishes itself by its low heating value ≦3 MJ/kg according to ISO 1716 and thanks to its special multilayer structure has excellent mechanical characteristics and an extraordinarily good stability under changing climatic conditions (hot/humid/cold/dry). The laminate according to the invention comprises several mineral and glass fiber non-woven fabrics with different functionalities and components. This includes high-filled non-woven fabrics, B-stage binders and other additives. Its great mechanical strength as well as the extraordinarily good stability under changing climatic conditions (hot/humid/cold/dry) allow its reasonable use in many areas where until now exclusively laminates according to EN 438 are used and beyond. | ||||||
| 37 | FLAME RESISTANT LAMINATE | US13820818 | 2011-09-21 | US20130323497A1 | 2013-12-05 | Gerald Ullrich; Michael Horvath; Michael Ketzer; Klaus Friedrich Gleich |
| A fire-resistant laminate is described, which distinguishes itself by its low heating value ≦3 MJ/kg according to ISO 1716 and thanks to its special multilayer structure has excellent mechanical characteristics and a very good stability under changing climatic conditions (hot/humid/cold/dry). The laminate according to the invention comprises several mineral and glass non-woven fabrics with different functionalities and components. This includes high-filled non-woven fabrics, B-stage binders and other additives.Its great mechanical strength as well as the very good stability under changing climatic conditions (hot/humid/cold/dry) allow its reasonable use in many areas where until now exclusively laminates according to EN 438 are used and furthermore. | ||||||
| 38 | METALLIC COATING OF COMPOSITE MATERIALS | US12518523 | 2007-12-06 | US20100151262A1 | 2010-06-17 | Thomas Joseph Corden; Mark Raymond Steele |
| A method of manufacturing a composite and of securing a metallic coating to a resin-based composite material, comprising the provision of a keying structure on a metallic electroplated preform and bringing the keying structure and the composite material together under conditions to cause the composite material and the keying structure to interlock. The invention also provides a composite comprising a resin-based composite material with a metallic coating on a surface, or part surface thereof, the metallic coating comprising an outer electroplated preform, and an inner keying structure which is located generally between said electroplated preform and the composite material to provide attachment of the electroplated preform on the composite material. | ||||||
| 39 | Laminate for use as outer covering of battery and secondary battery | US10487408 | 2002-08-30 | US07485393B2 | 2009-02-03 | Hideki Arao; Masashi Hiromitsu; Takakazu Goto; Kazuya Tanaka; Akio Shimizu; Ryoji Morita |
| The present invention relates to a laminate for battery encasement comprising aluminum foil and an inner layer, wherein a resin film layer that comprises an aminated phenol polymer (A), an acrylic polymer (B), a phosphorus compound (C), and a zirconium compound (D) lies between the aluminum foil and the inner layer. The laminate for battery encasement of the present invention is excellent in adhesiveness, gas impermeability, etc., and therefore can be suitably used as a material for encasing a secondary battery, particularly a lithium ion polymer secondary battery. | ||||||
| 40 | Phenolic lamination process for hot gas components | US10897499 | 2004-07-23 | US20060016551A1 | 2006-01-26 | Donald Christensen; Jason Gratton |
| A method is provided for fabricating a missile component having a flow path therein. The resulting component is a phenolic laminate constructed of layers having cavities formed therein. The method includes bonding a plurality of phenolic laminates to one another in a predetermined order and in a predetermined configuration, each phenolic laminate having a cavity formed therein, wherein the bonded phenolic laminates form the missile component and the cavities define the flow path. | ||||||
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