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公开(公告)号：EP1482163A3
公开(公告)日：2008-08-06
申请号：EP04253094.9
申请日：2004-05-26
发明人： Garrettson, Brook
CPC分类号： C09K21/14 , C08G77/04 , C08L83/04 , C08L97/007 , C09D5/18 , F02K9/34 , F02K9/974 , F05D2300/42 , F05D2300/614 , Y10T428/249924 , C08L2666/26 , C08L83/00
摘要： An insulation material suitable for use on rocket motor cases and airframe surfaces is provided. The insulation material is formed from a mixture of cork particulate, a plurality of fibers, and a siloxane based binder. The cork particulate, the binder, and the fibers are present in a mass ratio of 10-100 parts binder to 0.1-50 parts fiber to 1-100 parts cork. The insulation material may have a homogeneous or non-homogeneous composition and may be composite in nature.
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公开(公告)号：EP2466148B1
公开(公告)日：2015-07-01
申请号：EP11191330.7
申请日：2011-11-30
发明人： Bosbach, Franz
CPC分类号： F04D29/167 , F04D29/026 , F05D2300/42 , F05D2300/43 , F05D2300/603
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3.发明公开ROCKET ASSEMBLY ABLATIVE MATERIALS FORMED FROM SOLVENT-SPUN CELLULOSIC PRECURSORS, AND METHOD OF INSULATING OR THERMALLY PROTECTING A ROCKET ASSEMBLY WITH THE SAME 有权从纤维素溶液火箭形排列烧蚀材料编织前和方法分离或热火箭PROTECTING安排
公开(公告)号：EP1144835A2
公开(公告)日：2001-10-17
申请号：EP99963836.4
申请日：1999-08-19
IPC分类号： F02K9/00
CPC分类号： F02K9/974 , C06B45/12 , C08J5/04 , D01F9/16 , F02K9/346 , F05D2300/42 , Y10T428/24612 , Y10T428/24661 , Y10T428/24669 , Y10T428/24678 , Y10T428/2913 , Y10T428/2918 , Y10T428/30 , Y10T442/2926 , Y10T442/2975 , Y10T442/2984 , Y10T442/2992
摘要： A rocket motor assembly is insulated or thermally protected with a rocket motor ablative material formed from a prepreg. The prepreg contains at least an impregnating resin matrix and, as a precursor prior to carbonization, either carded and yarn-spun solvent-spun staple cellulosic fibers, solvent-spun cellulosic filaments, or a combination thereof. When patterned and carbonized, the rocket motor ablative material can be lined or otherwise placed into a rocket motor assembly, such as between the solid propellant and case, in the bulk area of the exit nozzle liner, or at susceptible portions of a re-entry vehicle, such as the nose cone.
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4.发明公开
公开(公告)号：EP3121440A1
公开(公告)日：2017-01-25
申请号：EP16179719.6
申请日：2016-07-15
IPC分类号： F03D1/06
CPC分类号： F03D1/0675 , B29C66/7392 , B29C66/7394 , F03D1/0658 , F05D2300/42 , F05D2300/433 , F05D2300/436 , F05D2300/603 , Y02E10/721 , Y02P70/523
摘要： The present disclosure is directed to a root assembly 30 for a rotor blade 16 of a wind turbine 10 and methods of manufacturing same. The root assembly 30 includes a blade root section 32 having an inner sidewall surface 40 and an outer sidewall surface 42 separated by a radial gap 44, a plurality of root inserts 46 spaced circumferentially within the radial gap 44, and a plurality of spacers 52 configured between one or more of the root inserts 46. Further, each of the root inserts 46 includes at least one bore hole 48 surrounded by a pre-cured or pre-consolidated composite material 50,54. In addition, the spacers 52 are constructed of a pre-cured or pre-consolidated composite material 50, 54.
摘要翻译： 本公开涉及用于风力涡轮机10的转子叶片16的根组件30及其制造方法。 根部组件30包括具有内侧壁表面40和由径向间隙44隔开的外侧壁表面42的叶片根部32，在径向间隙44内周向间隔开的多个根部插入件46以及多个间隔件52构造 在一个或多个根部插入件46之间。此外，每个根部插入件46包括由预固化或预固结的复合材料50,54包围的至少一个钻孔48。 此外，间隔件52由预固化或预固化复合材料50,54构成。
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5.发明公开Vorrichtung und Verfahren zur thermochemischen Umwandlung von Holz 审中-公开Vorrichtung und Verfahren zur thermhemischen Umwandlung von Holz
公开(公告)号：EP2236581A2
公开(公告)日：2010-10-06
申请号：EP10003708.4
申请日：2010-04-06
摘要： Dargestellt und beschrieben ist unter anderem eine Vorrichtung zur thermochemischen Umwandlung von Holz, mit mindestens einem kontinuierlich arbeitenden Bewegtbettreaktor, wie einem doppelwandigen Schneckenreaktor (11) od. dgl., in dem das über eine Einfüllöffnung (13) in den Schneckenreaktor (11) gelangte Holz unter Luftabschluss erwärmt, getrocknet und pyrolysiert wird, wobei der Schneckenreaktor (11) in Förderrichtung (x) vorne eine Öffnung (15) zur Entfernung des Pyrolysegases und eine Öffnung (14) zur Entfernung der Holzkohle aufweist, wobei der Schneckenreaktor mit (11) einem Ofen (18) zur im Wesentlichen vollständigen Verbrennung des Pyrolysegases verbunden ist, wobei der Ofen (18) mit einem Abgas-Luft-Wärmetauscher (20) versehen ist und wobei dem Abgas-Luft-Wärmetauscher (20) eine Einrichtung (T) zur Erzeugung von elektrischem Strom nachgeordnet ist.
Die Besonderheit besteht darin, dass die Einrichtung zur Erzeugung von elektrischem Strom eine Heißluftturbine (T) umfasst, dass der Abgas-Luft-Wärmetauscher (20) mit der Heißluftturbine (T) verbunden ist, um die dem Abgas-Luft-Wärmetauscher (20) zugeführte und von dem Abgas-Luft-Wärmetauscher (20) erwärmte Luft zu der Heißluftturbine (T) zu leiten und dass die Heißluftturbine (T) mit dem Ofen (19) verbunden ist, um zumindest einen Teil der Abluft der Heißluftturbine (T) einer Brennkammer (17) des Ofens (18) zuzuführen.摘要翻译： 装置包括连续操作的移动床反应器，如双壁螺杆式反应器（11），其中木材被加热，干燥和热解。 螺杆式反应器具有用于除去木炭的输送方向（x）的前开口（15）和用于除去木炭的另一开口（14）。 螺杆式反应器与烘箱（18）连接，用于热解气体的完全燃烧。 烘箱设置有排气 - 空气 - 热交换器（20），其中从属于排气 - 空气 - 热交换器的装置（T）用于产生电流。 装置包括连续操作的移动床反应器，如双壁螺杆式反应器，其中木材被加热，干燥并通过空气密封热解。 螺杆式反应器具有用于除去木炭的输送方向的前开口和用于除去木炭的另一开口。 螺杆式反应器与烘箱连接，用于完全燃烧热解气体。 烘箱设有排气 - 空气 - 热交换器，其中设备从属于排气 - 空气 - 热交换器以产生电流。 该装置包括用于产生电流的热空气涡轮机。 排气 - 空气 - 热交换器与热空气涡轮机连接以引导排气 - 热交换器并将空气引导到热空气涡轮机。 热风涡轮机与烘箱（19）连接，以供应炉的燃烧室（17）的一部分排气或热空气涡轮机。 还包括用于木材热化学转化的方法的独立权利要求，其涉及向与废气 - 空气 - 热交换器相关联的烘箱中供应空气。
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6.发明授权ROCKET ASSEMBLY ABLATIVE MATERIALS FORMED FROM SOLVENT-SPUN CELLULOSIC PRECURSORS, AND METHOD OF INSULATING OR THERMALLY PROTECTING A ROCKET ASSEMBLY WITH THE SAME 有权从纤维素溶液火箭形排列烧蚀材料编织前和方法分离或热火箭PROTECTING安排
公开(公告)号：EP1144835B1
公开(公告)日：2003-07-16
申请号：EP99963836.4
申请日：1999-08-19
IPC分类号： F02K9/00
CPC分类号： F02K9/974 , C06B45/12 , C08J5/04 , D01F9/16 , F02K9/346 , F05D2300/42 , Y10T428/24612 , Y10T428/24661 , Y10T428/24669 , Y10T428/24678 , Y10T428/2913 , Y10T428/2918 , Y10T428/30 , Y10T442/2926 , Y10T442/2975 , Y10T442/2984 , Y10T442/2992
摘要： A rocket motor assembly is insulated or thermally protected with a rocket motor ablative material formed from a prepreg. The prepreg contains at least an impregnating resin matrix and, as a precursor prior to carbonization, either carded and yarn-spun solvent-spun staple cellulosic fibers, solvent-spun cellulosic filaments, or a combination thereof. When patterned and carbonized, the rocket motor ablative material can be lined or otherwise placed into a rocket motor assembly, such as between the solid propellant and case, in the bulk area of the exit nozzle liner, or at susceptible portions of a re-entry vehicle, such as the nose cone.
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7.发明公开ROCKET ASSEMBLY ABLATIVE MATERIALS FORMED FROM SOLVENT-SPUN CELLULOSIC PRECURSORS, AND METHOD OF INSULATING OR THERMALLY PROTECTING A ROCKET ASSEMBLY WITH THE SAME 有权从纤维素溶液火箭形排列烧蚀材料编织前和方法分离或热火箭PROTECTING安排
公开(公告)号：EP1144835A3
公开(公告)日：2002-12-18
申请号：EP99963836.4
申请日：1999-08-19
IPC分类号： F02K9/00
CPC分类号： F02K9/974 , C06B45/12 , C08J5/04 , D01F9/16 , F02K9/346 , F05D2300/42 , Y10T428/24612 , Y10T428/24661 , Y10T428/24669 , Y10T428/24678 , Y10T428/2913 , Y10T428/2918 , Y10T428/30 , Y10T442/2926 , Y10T442/2975 , Y10T442/2984 , Y10T442/2992
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8.发明公开
公开(公告)号：EP1105636A1
公开(公告)日：2001-06-13
申请号：EP99942262.9
申请日：1999-08-19
CPC分类号： C08J5/04 , C06B45/12 , D01F9/16 , F02K9/346 , F02K9/974 , F05D2300/42 , Y10S428/92 , Y10T428/1314 , Y10T428/1362 , Y10T428/24992 , Y10T428/2843 , Y10T428/2924 , Y10T428/2982 , Y10T428/30 , Y10T442/56 , Y10T442/637
摘要： A rocket motor assembly is insulated or thermally protected with a rocket motor ablative material formed from a prepreg. The prepreg contains at least an impregnating resin matrix and, as a precursor prior to carbonization, carded and spun staple cellulosic fibers. When patterned and carbonized, the rocket motor ablative material can be lined or otherwise placed into a rocket motor assembly, such as between the solid propellant and case, in the bulk area of the exit nozzle liner, or at susceptible portions of a re-entry vehicle, such as the nose cone.
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公开(公告)号：EP3313657A1
公开(公告)日：2018-05-02
申请号：EP16738062.5
申请日：2016-06-24
申请人： Patentco ApS
发明人： IBSEN, Ditte Hofman
CPC分类号： C09J7/255 , B32B3/02 , B32B3/266 , B32B5/02 , B32B5/022 , B32B5/024 , B32B5/08 , B32B5/26 , B32B7/06 , B32B7/12 , B32B27/06 , B32B27/12 , B32B27/40 , B32B2255/02 , B32B2255/26 , B32B2255/28 , B32B2262/0261 , B32B2262/0269 , B32B2262/0276 , B32B2262/065 , B32B2262/101 , B32B2262/106 , B32B2262/108 , B32B2262/14 , B32B2307/748 , B32B2419/00 , B32B2603/00 , B32B2605/18 , F01D5/288 , F03B17/061 , F03D1/0675 , F03D13/25 , F05B2230/90 , F05B2280/6011 , F05D2230/90 , F05D2300/224 , F05D2300/30 , F05D2300/42 , F05D2300/43 , F05D2300/611 , Y02E10/721 , Y02T50/673
摘要： Coating system (1) for coating a surface (3) of a substrate (5), the coating system (1) comprising; a coating (7), and an adhesive layer (9), that is disposed between the substrate (5) and the coating (7), wherein the adhesive layer (9) comprises a first adhesive layer portion (13) adjacent the substrate (5) and a second adhesive layer portion (15) adjacent the coating (7) and a carrier (11) placed between said first and second adhesive layer portions (13, 5), wherein the first adhesive layer portion (13) is composed of a first adhesive layer material, wherein the second adhesive layer portion (15) is composed of a second adhesive layer material, wherein the first adhesive layer material and the second adhesive layer material is having an adhesive or bond strength to the surface (3) of the substrate (5) and to the coating (7) respectively that exceeds their respective cohesive or tensile strength, wherein the first and second adhesive layer materials and carrier (11) combination is configured for having an adhesive strength that is less than their respective cohesive or tensile strength, wherein the carrier (11) is configured with grab tensile properties such that the carrier (11) in combination with the second adhesive layer portion (15) and the coating (7) will separate from the first adhesive layer portion (13) under the action of a peeling force.
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公开(公告)号：EP2466148A1
公开(公告)日：2012-06-20
申请号：EP11191330.7
申请日：2011-11-30
发明人： Bosbach, Franz
CPC分类号： F04D29/167 , F04D29/026 , F05D2300/42 , F05D2300/43 , F05D2300/603
摘要： Vorrichtung aus einem Verbundwerkstoff zur Einhaltung kleinster Spaltweiten zwischen Rotor und Gehäuse einer Strömungsarbeitsmaschine, insbesondere einer Kreiselpumpe, wobei die Vorrichtung aus mindestens zwei unterschiedlichen Werkstoffen besteht, wobei mindestens ein Werkstoff (2) die geometrische Gestalt der Vorrichtung vorgibt und erfindungsgemäß mindestens ein Werkstoff (5) bei Kontakt mit Förderfluid quellende Eigenschaften aufweist.
摘要翻译： 该环具有复合材料，该复合材料包括形成为成形稳定组分的材料组分（2）。 复合材料的另一材料成分形成为在水分影响下确定体积变化的源材料（5）。 源材料在空间上改变环的间隙限制壁表面，并且前一材料部件包括几何形状。 源材料形成有间隙宽度变化特性，并且材料成分包括不同的溶胀特性和/或不同的流体渗透性。 源材料选自生物源材料，木材或热处理木材。 包括材料组分的复合材料选自基于可再生原料的聚合材料。 还包括用于构造用于观察流体流动机器的转子和壳体之间的最小间隙宽度的装置的方法的独立权利要求。
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