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1.发明授权Temperature and humidity-controlled composite material article, and methods for using such an article 有权温湿度控制复合材料制品，以及使用这种制品的方法公开(公告)号：US08324537B2
公开(公告)日：2012-12-04
申请号：US12530405
申请日：2007-08-31
CPC分类号： B64C1/12 , B32B3/08 , B32B27/04 , B32B2305/076 , B32B2305/34 , B64D15/12 , H05B3/20
摘要： An article of composite material includes a plurality of plies of material consolidated through the application of pressure and heating, in which each material ply is made by a resin matrix reinforced with fiber material. The article includes heating electrical resistance and temperature sensing devices embedded in the composite material, which are respectively placed in at least one interface zone between the material plies and are suitable to allow a temperature control of the article in service.
摘要翻译： 复合材料制品包括通过施加压力和加热而固化的多层材料，其中每个材料层由用纤维材料增强的树脂基体制成。 该制品包括加热电阻和嵌入在复合材料中的温度感测装置，其分别放置在材料层之间的至少一个界面区域中，并且适于允许制品的使用温度控制。
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2.发明申请TEMPERATURE AND HUMIDITY-CONTROLLED COMPOSITE MATERIAL ARTICLE, AND METHODS FOR USING SUCH AN ARTICLE 有权温度和湿度控制的复合材料文章和使用这些文章的方法公开(公告)号：US20100096383A1
公开(公告)日：2010-04-22
申请号：US12530405
申请日：2007-08-31
CPC分类号： B64C1/12 , B32B3/08 , B32B27/04 , B32B2305/076 , B32B2305/34 , B64D15/12 , H05B3/20
摘要： An article of composite material includes a plurality of plies of material consolidated through the application of pressure and heating, in which each material ply is made by a resin matrix reinforced with fiber material. The article includes heating electrical resistance and temperature sensing devices embedded in the composite material, which are respectively placed in at least one interface zone between the material plies and are suitable to allow a temperature control of the article in service.
摘要翻译： 复合材料制品包括通过施加压力和加热而固化的多层材料，其中每个材料层由用纤维材料增强的树脂基体制成。 该制品包括加热电阻和嵌入在复合材料中的温度感测装置，其分别放置在材料层之间的至少一个界面区域中，并且适于允许制品的使用温度控制。
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3.发明申请Wing and empennage leading edge structure made of thermoplastic material with a stiffened double shell configuration 审中-公开翼和尾翼前缘结构由热塑性材料制成，具有加强的双壳结构公开(公告)号：US20090277996A1
公开(公告)日：2009-11-12
申请号：US12387589
申请日：2009-05-05
摘要： A leading edge structure is described for wing structures and empennage, comprising an outer shell suitable to define a front portion of a airfoil. The outer shell is formed by a bent plate of fiber-reinforced thermoplastic resin composite material. The structure further comprisesan inner shell having a convex profile that is oriented in the same direction as the profile of outer shell, which is formed by a bent plate of fiber-reinforced thermoplastic resin composite material and is bonded to the outer shell at the longitudinal edges thereof, andat least one reinforcing element, transversally extending such as to connect the outer shell and inner shell to each other , which is formed by at least one piece of fiber-reinforced resin composite material and is fixed at opposite ends to the outer shell and inner shell, respectively.
摘要翻译： 描述了用于翼结构和尾翼的前缘结构，其包括适于限定翼型件的前部的外壳。 外壳由纤维增强热塑性树脂复合材料的弯曲板形成。 该结构还包括内壳，其具有与外壳轮廓相同的方向定向的凸形轮廓，外壳的轮廓由纤维增强热塑性树脂复合材料的弯曲板形成，并且在纵向上与外壳结合 边缘和至少一个加强元件，其横向延伸以将外壳和内壳彼此连接，所述外壳和内壳由至少一片纤维增强树脂复合材料形成，并且在相对端固定到外部 壳和内壳。
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4.发明授权公开(公告)号：US08481615B2
公开(公告)日：2013-07-09
申请号：US12944608
申请日：2010-11-11
申请人： Liberata Guadagno , Marialuigia Raimondo , Carlo Naddeo , Annaluisa Mariconda , Raffaele Corvino , Pasquale Longo , Vittoria Vittoria , Salvatore Russo , Generoso Iannuzzo
发明人： Liberata Guadagno , Marialuigia Raimondo , Carlo Naddeo , Annaluisa Mariconda , Raffaele Corvino , Pasquale Longo , Vittoria Vittoria , Salvatore Russo , Generoso Iannuzzo
CPC分类号： B29C73/22 , B29C73/16 , C08F283/10 , C08G59/226 , C08G59/50 , C08G59/623 , C08G59/68 , C08G59/688 , C08G59/70 , C08G61/08 , C08G2261/3324 , C08G2261/418 , C08L51/08 , C08L63/00 , C08L65/00 , C08L2205/02 , C08L2666/02
摘要： A process is for preparing a self-healing composite material including a matrix of epoxy polymer in which a catalyst of ring opening metathesis reaction and vessels containing at least one monomer able to polymerize due to a ring opening metathesis reaction are dispersed. The process includes the preliminary step of dispersing at molecular level the catalyst in a mixture containing at least one precursor of the epoxy polymer, and then the steps of dispersing, in the mixture, the vessels and a tertiary amine acting as curing agent of the precursor, and the step of curing the mixture by at least a first heating stage performed at a temperature between 70 and 90° C. for a time between 1 and 5 hours, and a second heating stage performed at a temperature between 90 and 170° C. for a time between 2 and 3 hours.
摘要翻译： 一种制备自愈合复合材料的方法，其包括环状聚合物基质，其中开环复分解反应的催化剂和含有至少一种能够由开环复分解反应聚合的单体的容器被分散。 该方法包括在分子水平下将催化剂分散在含有至少一种环氧聚合物前体的混合物中的预备步骤，然后分散在混合物中的容器和作为前体固化剂的叔胺 ，以及在70至90℃之间的温度下进行至少第一加热阶段固化该混合物的步骤，持续1至5小时之间的时间，以及在90至170℃的温度下进行的第二加热阶段 在2到3小时之间的时间。
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5.发明申请PROCESS FOR MONITORING THE CURING REACTION OF A POLYMERIC MATRIX OF A COMPOSITE MATERIAL 有权用于监测复合材料的聚合物基体的固化反应的方法公开(公告)号：US20100117665A1
公开(公告)日：2010-05-13
申请号：US12615161
申请日：2009-11-09
申请人： Andrea Sorrentino , Heinrich Christoph Neitzert , Luigi Vertuccio , Liberata Guadagno , Vittoria Vittoria , Generoso Iannuzzo , Salvatore Russo , Erika Calvi
发明人： Andrea Sorrentino , Heinrich Christoph Neitzert , Luigi Vertuccio , Liberata Guadagno , Vittoria Vittoria , Generoso Iannuzzo , Salvatore Russo , Erika Calvi
IPC分类号： G01R27/08
CPC分类号： C08J3/248
摘要： The process for monitoring the curing reaction of a polymeric matrix, in which carbon nanotubes are dispersed whereby a composite material is formed, provides for: arranging an electric circuit comprising at least a generator of a substantially constant voltage, an amperemeter and two electrodes immersed into the composite material, whereby the composite material interposed between the electrodes closes the electrical circuit, and tracing the current intensity value measured by the amperemeter, which is correlated to the progress of the curing reaction of the polymeric matrix, so as to control said progress.
摘要翻译： 用于监测聚合物基体的固化反应的方法，其中分散有碳纳米管，由此形成复合材料，其提供：布置电路，该电路至少包括基本上恒定电压的发生器，安培计和两个电极浸入 复合材料，由此介于电极之间的复合材料封闭电路，并跟踪与安培计测量的电流强度值，其与聚合物基体的固化反应的进程相关，以便控制所述进展。
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6.发明申请公开(公告)号：US20110118385A1
公开(公告)日：2011-05-19
申请号：US12944608
申请日：2010-11-11
申请人： Liberata Guadagno , Marialuigia Raimondo , Carlo Naddeo , Annaluisa Mariconda , Raffaele Corvino , Pasquale Longo , Vittoria Vittoria , Salvatore Russo , Generoso Iannuzzo
发明人： Liberata Guadagno , Marialuigia Raimondo , Carlo Naddeo , Annaluisa Mariconda , Raffaele Corvino , Pasquale Longo , Vittoria Vittoria , Salvatore Russo , Generoso Iannuzzo
CPC分类号： B29C73/22 , B29C73/16 , C08F283/10 , C08G59/226 , C08G59/50 , C08G59/623 , C08G59/68 , C08G59/688 , C08G59/70 , C08G61/08 , C08G2261/3324 , C08G2261/418 , C08L51/08 , C08L63/00 , C08L65/00 , C08L2205/02 , C08L2666/02
摘要： A process is for preparing a self-healing composite material including a matrix of epoxy polymer in which a catalyst of ring opening metathesis reaction and vessels containing at least one monomer able to polymerize due to a ring opening metathesis reaction are dispersed. The process includes the preliminary step of dispersing at molecular level the catalyst in a mixture containing at least one precursor of the epoxy polymer, and then the steps of dispersing, in the mixture, the vessels and a tertiary amine acting as curing agent of the precursor, and the step of curing the mixture by at least a first heating stage performed at a temperature between 70 and 90° C. for a time between 1 and 5 hours, and a second heating stage performed at a temperature between 90 and 170° C. for a time between 2 and 3 hours.
摘要翻译： 一种制备自愈合复合材料的方法，其包括环状聚合物基质，其中开环复分解反应的催化剂和含有至少一种能够由开环复分解反应聚合的单体的容器被分散。 该方法包括在分子水平下将催化剂分散在含有至少一种环氧聚合物前体的混合物中的预备步骤，然后分散在混合物中的容器和作为前体固化剂的叔胺 ，以及在70至90℃之间的温度下进行至少第一加热阶段固化该混合物的步骤，持续1至5小时之间的时间，以及在90至170℃的温度下进行的第二加热阶段 在2到3小时之间的时间。
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公开(公告)号：US20100168280A1
公开(公告)日：2010-07-01
申请号：US12586993
申请日：2009-09-30
申请人： Liberata Guadagno , Pasquale Longo , Marialuigia Raimondo , Annaluisa Mariconda , Carlo Naddeo , Andrea Sorrentino , Vittoria Vittoria , Generoso Iannuzzo , Salvatore Russo , Erika Calvi
发明人： Liberata Guadagno , Pasquale Longo , Marialuigia Raimondo , Annaluisa Mariconda , Carlo Naddeo , Andrea Sorrentino , Vittoria Vittoria , Generoso Iannuzzo , Salvatore Russo , Erika Calvi
CPC分类号： C08F283/10 , B01J31/2208 , B01J31/2273 , B01J31/2278 , B01J2231/543 , B01J2531/821 , B29C73/163 , B29C73/22 , C08G59/4014 , C08G59/50 , C08L51/08 , C08L63/00 , C08L2666/02
摘要： The process for preparing a self-healing composite material comprising a matrix of epoxy polymer, in which a catalyst of ring opening metathesis reaction and microcapsules containing a cyclic olefin having 7 to 40 carbon atoms are dispersed, comprises the steps of: preparing a mixture of a precursor of the epoxy polymer, having at least one oxirane ring, a curing agent chosen from the group consisting of tertiary amines, a Hoveyda-Grubbs II metathesis catalyst reaction, having the formula (I), wherein Ar=aryl having at least one halogen or alkyl substituent and “R=alkyl with 1 to 20 carbon atoms, and microcapsules containing a cyclic olefin having 7 to 40 carbon atoms; and heating the mixture at a temperature comprised between 25 and 130° C. for at least 1 hour, so as to obtain such matrix of epoxy polymer due to a reaction between precursor and curing agent, which reaction does not substantially involve either said catalyst or said microcapsules.
摘要翻译： 制备包含环状聚合物基质的自愈合复合材料的方法，其中分离开环复分解反应的催化剂和含有具有7至40个碳原子的环烯烃的微胶囊包括以下步骤：制备 具有至少一个环氧乙烷环的环氧聚合物的前体，选自叔胺，具有式（I）的Hoveyda-Grubbs II复分解催化剂反应的固化剂，其中Ar =具有至少一个 卤素或烷基取代基，“R =碳原子数1〜20的烷基”，含有碳原子数为7〜40的环状烯烃的微胶囊; 并将混合物在25℃至130℃之间的温度下加热至少1小时，以便由于前体和固化剂之间的反应而获得这种环氧聚合物基质，该反应基本上不涉及所述催化剂或 所述微胶囊。
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8.发明申请ACTUATOR DEVICE BASED ON A SHAPE MEMORY ALLOY, AND A WING FLAP ASSEMBLY FITTED WITH SUCH AN ACTUATOR DEVICE 有权基于形状记忆合金的执行器装置，以及用这种执行器装置装配的翼片组件公开(公告)号：US20100019096A1
公开(公告)日：2010-01-28
申请号：US12507677
申请日：2009-07-22
申请人： Rosario Pecora , Generoso Iannuzzo , Massimo Riccio , Salvatore Russo , Erika Calvi , Leonardo Lecce , Silvestro Barbarino , Antonio Concilio , Salvatore Ameduri
发明人： Rosario Pecora , Generoso Iannuzzo , Massimo Riccio , Salvatore Russo , Erika Calvi , Leonardo Lecce , Silvestro Barbarino , Antonio Concilio , Salvatore Ameduri
摘要： A wing-flap assembly includes a flap made up of a plurality of flap sections, in which each flap section is connected to the preceding one in a rotatable manner, and one or more actuator devices adapted to control the rotation of the flap sections. Each actuator device includes an extended element made of shape memory alloy and an arch-shaped framework made of elastic material, to which the extended element is fixedly connected under tension. Each end of the extended element is fixed to a respective end of the arch-shaped framework. At least one of the actuator devices is connected at one end to the first of the flap sections, and on the other side it is adapted to be connected to a wing structure.
摘要翻译： 翼片组件包括由多个翼片部分构成的翼片，其中每个翼片部分以可旋转的方式连接到前一个翼片部分，以及适于控制翼片部分的旋转的一个或多个致动器装置。 每个致动器装置包括由形状记忆合金制成的延伸元件和由弹性材料制成的拱形框架，延伸元件在张力下固定连接到该延伸元件上。 延伸元件的每个端部固定到拱形框架的相应端部。 致动器装置中的至少一个在一端连接到第一翼片部分，并且另一侧适于连接到机翼结构。
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9.发明授权Process for monitoring the curing reaction of a polymeric matrix of a composite material 有权用于监测复合材料的聚合物基质的固化反应的方法公开(公告)号：US08382975B2
公开(公告)日：2013-02-26
申请号：US12615161
申请日：2009-11-09
申请人： Andrea Sorrentino , Heinrich Christoph Neitzert , Luigi Vertuccio , Liberata Guadagno , Vittoria Vittoria , Generoso Iannuzzo , Salvatore Russo , Erika Calvi
发明人： Andrea Sorrentino , Heinrich Christoph Neitzert , Luigi Vertuccio , Liberata Guadagno , Vittoria Vittoria , Generoso Iannuzzo , Salvatore Russo , Erika Calvi
IPC分类号： B32B37/14
CPC分类号： C08J3/248
摘要： The process for monitoring the curing reaction of a polymeric matrix, in which carbon nanotubes are dispersed whereby a composite material is formed, provides for: arranging an electric circuit comprising at least a generator of a substantially constant voltage, an amperemeter and two electrodes immersed into the composite material, whereby the composite material interposed between the electrodes closes the electrical circuit, and tracing the current intensity value measured by the amperemeter, which is correlated to the progress of the curing reaction of the polymeric matrix, so as to control said progress.
摘要翻译： 用于监测聚合物基体的固化反应的方法，其中分散有碳纳米管，由此形成复合材料，其提供：布置电路，该电路至少包括基本上恒定电压的发生器，安培计和两个电极浸入 复合材料，由此介于电极之间的复合材料封闭电路，并跟踪与安培计测量的电流强度值，其与聚合物基体的固化反应的进程相关，以便控制所述进展。
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10.发明授权Actuator device based on a shape memory alloy, and a wing flap assembly fitted with such an actuator device 有权基于形状记忆合金的致动器装置和装配有这种致动器装置的翼片组件公开(公告)号：US08348201B2
公开(公告)日：2013-01-08
申请号：US12507677
申请日：2009-07-22
申请人： Rosario Pecora , Generoso Iannuzzo , Massimo Riccio , Salvatore Russo , Erika Calvi , Leonardo Lecce , Silvestro Barbarino , Antonio Concilio , Salvatore Ameduri
发明人： Rosario Pecora , Generoso Iannuzzo , Massimo Riccio , Salvatore Russo , Erika Calvi , Leonardo Lecce , Silvestro Barbarino , Antonio Concilio , Salvatore Ameduri
IPC分类号： B64C3/58
摘要： A wing-flap assembly includes a flap made up of a plurality of flap sections, in which each flap section is connected to the preceding one in a rotatable manner, and one or more actuator devices adapted to control the rotation of the flap sections. Each actuator device includes an extended element made of shape memory alloy and an arch-shaped framework made of elastic material, to which the extended element is fixedly connected under tension. Each end of the extended element is fixed to a respective end of the arch-shaped framework. At least one of the actuator devices is connected at one end to the first of the flap sections, and on the other side it is adapted to be connected to a wing structure.
摘要翻译： 翼片组件包括由多个翼片部分构成的翼片，其中每个翼片部分以可旋转的方式连接到前一个翼片部分，以及适于控制翼片部分的旋转的一个或多个致动器装置。 每个致动器装置包括由形状记忆合金制成的延伸元件和由弹性材料制成的拱形框架，延伸元件在张力下固定连接到该延伸元件。 延伸元件的每个端部固定到拱形框架的相应端部。 致动器装置中的至少一个在一端连接到第一翼片部分，并且另一侧适于连接到机翼结构。
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