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公开(公告)号：US5480678A
公开(公告)日：1996-01-02
申请号：US340677
申请日：1994-11-16
申请人： James W. Rudolph , Mark J. Purdy , Lowell D. Bok
发明人： James W. Rudolph , Mark J. Purdy , Lowell D. Bok
IPC分类号： C04B35/52 , C04B35/83 , C04B41/85 , C04B41/87 , C23C16/04 , C23C16/44 , C23C16/452 , C23C16/455 , C23C16/458 , C23C16/46 , F16D69/02 , F27B9/00 , H05B3/14 , C23C16/00
CPC分类号： C23C16/4411 , C04B35/83 , C23C16/045 , C23C16/452 , C23C16/45591 , C23C16/4583 , C23C16/46 , F16D69/023
摘要： The invention relates to apparatus for use in chemical vapor infiltration and deposition (CVI/CVD) processes. More specifically, the invention relates to a preheater for heating a reactant gas inside a CVI/CVD furnace, and a fixture for depositing a matrix within a stack of porous structures by a pressure gradient CVI/CVD process. The invention is particularly suited for the simultaneous CVI/CVD processing of large quantities (hundreds) of aircraft brake disks.
摘要翻译： 本发明涉及用于化学气相渗透和沉积（CVI / CVD）工艺的设备。 更具体地，本发明涉及一种用于加热CVI / CVD炉内的反应气体的预热器，以及用于通过压力梯度CVI / CVD工艺在多孔结构的堆叠内沉积基质的夹具。 本发明特别适用于大量（数百个）飞机制动盘的同时CVI / CVD处理。
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公开(公告)号：US6057022A
公开(公告)日：2000-05-02
申请号：US34037
申请日：1998-03-03
申请人： Mark J. Purdy , James W. Rudolph
发明人： Mark J. Purdy , James W. Rudolph
IPC分类号： C04B41/85 , C04B35/83 , C04B41/87 , C23C16/04 , C23C16/44 , C23C16/452 , C23C16/455 , C23C16/458 , C23C16/52 , F16D65/12 , F16D69/02 , B32B3/02
CPC分类号： C23C16/45561 , C04B35/83 , C23C16/045 , C23C16/452 , C23C16/45557 , C23C16/458 , C23C16/52 , F16D65/126 , F16D69/023 , C04B2235/614 , C04B2235/77 , Y10S427/10 , Y10T428/21 , Y10T428/213 , Y10T428/218 , Y10T428/249961 , Y10T428/249964 , Y10T428/249978 , Y10T428/2918 , Y10T428/30
摘要： The invention relates to the field of high temperature composites made by the chemical vapor infiltration and deposition of a binding matrix within a porous structure. More particularly, the invention relates to pressure gradient processes for forcing infiltration of a reactant gas into a porous structure, apparatus for carrying out those processes, and the resulting products. The invention is particularly suited for the simultaneous CVI/CVD processing of large quantities (hundreds) of aircraft brake disks.
摘要翻译： 本发明涉及通过化学气相渗透和在多孔结构内沉积结合基质制成的高温复合材料领域。 更具体地，本发明涉及用于迫使反应物气体渗入多孔结构的压力梯度过程，用于执行这些过程的装置以及所得到的产物。 本发明特别适用于大量（数百个）飞机制动盘的同时CVI / CVD处理。
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公开(公告)号：US5853485A
公开(公告)日：1998-12-29
申请号：US851860
申请日：1997-05-06
申请人： James W. Rudolph , Mark J. Purdy
发明人： James W. Rudolph , Mark J. Purdy
IPC分类号： C04B41/85 , C04B35/83 , C04B41/87 , C23C16/04 , C23C16/44 , C23C16/452 , C23C16/455 , C23C16/458 , C23C16/52 , F16D65/12 , F16D69/02 , C23C16/00
CPC分类号： C23C16/45561 , C04B35/83 , C23C16/045 , C23C16/452 , C23C16/45557 , C23C16/458 , C23C16/52 , F16D65/126 , F16D69/023 , C04B2235/614 , C04B2235/77 , Y10S427/10 , Y10T428/21 , Y10T428/213 , Y10T428/218 , Y10T428/249961 , Y10T428/249964 , Y10T428/249978 , Y10T428/2918 , Y10T428/30
摘要： The invention relates to the field of high temperature composites made by the chemical vapor infiltration and deposition of a binding matrix within a porous structure. More particularly, the invention relates to pressure gradient processes for forcing infiltration of a reactant gas into a porous structure, apparatus for carrying out those processes, and the resulting products. The invention is particularly suited for the simultaneous CVI/CVD processing of large quantities (hundreds) of aircraft brake disks.
摘要翻译： 本发明涉及通过化学气相渗透和在多孔结构内沉积结合基质制成的高温复合材料领域。 更具体地，本发明涉及用于迫使反应物气体渗入多孔结构的压力梯度过程，用于执行这些过程的装置以及所得到的产物。 本发明特别适用于大量（数百个）飞机制动盘的同时CVI / CVD处理。
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公开(公告)号：US06780462B2
公开(公告)日：2004-08-24
申请号：US09754829
申请日：2001-01-03
申请人： Mark J. Purdy , James W. Rudolph , Lowell D. Bok
发明人： Mark J. Purdy , James W. Rudolph , Lowell D. Bok
IPC分类号： C23C1600
CPC分类号： C23C16/45561 , C04B35/83 , C04B2235/614 , C04B2235/77 , C23C16/045 , C23C16/452 , C23C16/45557 , C23C16/458 , C23C16/52 , F16D65/126 , F16D69/023 , Y10S427/10 , Y10T428/21 , Y10T428/213 , Y10T428/218 , Y10T428/249961 , Y10T428/249964 , Y10T428/249978 , Y10T428/2918 , Y10T428/30
摘要： The invention relates to pressure gradient processes for forcing infiltration of a reactant gas into a porous structure. The process comprises the steps of partially densifying a porous structure with a pressure gradient CVI/CVD process in which a first potion of the porous structure is subjected to greater pressure than a second portion of the porous structure. The process is suited for the simultaneous CVI/CVD processing of large quantities of aircraft brake.
摘要翻译： 本发明涉及用于迫使反应气体渗入多孔结构的压力梯度方法。 该方法包括以压力梯度CVI / CVD工艺部分致密化多孔结构的步骤，其中多孔结构的第一部分经受比多孔结构的第二部分更大的压力。 该过程适用于大量飞机制动器的同时CVI / CVD处理。
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公开(公告)号：US6109209A
公开(公告)日：2000-08-29
申请号：US966612
申请日：1997-11-10
申请人： James W. Rudolph , Mark J. Purdy , Lowell D. Bok
发明人： James W. Rudolph , Mark J. Purdy , Lowell D. Bok
IPC分类号： C04B35/52 , C04B35/83 , C04B41/85 , C04B41/87 , C23C16/04 , C23C16/44 , C23C16/452 , C23C16/455 , C23C16/458 , C23C16/46 , F16D69/02 , F27B9/00 , H05B3/14 , C23C16/00
CPC分类号： C23C16/4411 , C04B35/83 , C23C16/045 , C23C16/452 , C23C16/45591 , C23C16/4583 , C23C16/46 , F16D69/023
摘要： A gas preheater for use in a CVI/CVD furnace that receives a reactant gas from a gas inlet, comprising a sealed baffle structure disposed within the furnace. The sealed baffle structure has a baffle structure inlet and baffle structure outlet. A sealed duct structure is disposed within the furnace, said sealed duct structure being sealed around the gas inlet and said baffle structure such that substantially all of the reaction gas received from the gas inlet is directed to and forced to flow through said sealed baffle structure to said baffle structure outlet.
摘要翻译： 一种用于CVI / CVD炉的气体预热器，其接收来自气体入口的反应气体，包括设置在炉内的密封挡板结构。 密封挡板结构具有挡板结构入口和挡板结构出口。 密封的管道结构设置在炉内，所述密封管道结构围绕气体入口和所述挡板结构密封，使得从气体入口接收的基本上所有的反应气体被引导并被迫流过所述密封的挡板结构， 所述挡板结构出口。
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公开(公告)号：US5900297A
公开(公告)日：1999-05-04
申请号：US966819
申请日：1997-11-10
申请人： James W. Rudolph , Mark J. Purdy
发明人： James W. Rudolph , Mark J. Purdy
IPC分类号： C04B41/85 , C04B35/83 , C04B41/87 , C23C16/04 , C23C16/44 , C23C16/452 , C23C16/455 , C23C16/458 , C23C16/52 , F16D65/12 , F16D69/02 , B32B3/02
CPC分类号： C23C16/45561 , C04B35/83 , C23C16/045 , C23C16/452 , C23C16/45557 , C23C16/458 , C23C16/52 , F16D65/126 , F16D69/023 , C04B2235/614 , C04B2235/77 , Y10S427/10 , Y10T428/21 , Y10T428/213 , Y10T428/218 , Y10T428/249961 , Y10T428/249964 , Y10T428/249978 , Y10T428/2918 , Y10T428/30
摘要： The invention relates to the field of high temperature composites made by the chemical vapor infiltration and deposition of a binding matrix within a porous structure. More particularly, the invention relates to pressure gradient processes for forcing infiltration of a reactant gas into a porous structure, apparatus for carrying out those processes, and the resulting products. The invention is particularly suited for the simultaneous CVI/CVD processing of large quantities (hundreds) of aircraft brake disks.
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公开(公告)号：US5298311A
公开(公告)日：1994-03-29
申请号：US450145
申请日：1989-12-13
CPC分类号： C04B41/009 , C04B35/806 , C04B41/52 , C04B41/89 , Y10T428/24942 , Y10T428/2495 , Y10T428/24975 , Y10T428/249957 , Y10T428/24999 , Y10T428/25 , Y10T428/258 , Y10T428/30
摘要： Carbon/carbon composites including those structures formed from a fibrous reinforcement itself formed principally from carbon in a carbon matrix are protected against oxidation by multi-layer sealant system preferably including a multi-layer paint including in its carbonized binder refactory granules and inhibitor particles that form a moisture resistant, viscosity-stabilized borate glass when exposed to a high-temperature, oxidizing environment, and an outer ceramic shell formed by CVI/CVD in situ formation of boron carbide followed by silicon carbide. The paint is prepared by mixing finely divided powders of borate precursor compounds or borate glass frit and refractory granules with a carbon char yielding precursor binder such as phenolic resin or pitch which preferably produces a highly porous structure upon carbonization.
摘要翻译： 包括由主要由碳基体中的碳形成的纤维增强本身形成的那些结构的碳/碳复合材料通过多层密封剂系统被保护以防止氧化，优选地包括多层涂料，其包括在其碳化粘合剂的重构颗粒和形成 当暴露于高温氧化环境时，防潮，粘度稳定的硼酸盐玻璃，以及通过CVI / CVD形成的外部陶瓷壳体原位形成碳化硼，然后碳化硅。 通过将硼酸盐前体化合物或硼酸盐玻璃料和耐火颗粒的细碎粉末与碳炭产生前体粘合剂如酚醛树脂或沥青混合来制备涂料，其优选在碳化时产生高度多孔的结构。
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公开(公告)号：US5127783A
公开(公告)日：1992-07-07
申请号：US356815
申请日：1989-05-25
申请人： Sharad R. Moghe , Mark J. Purdy , Wei-Teh Shih , James A. Tallon
发明人： Sharad R. Moghe , Mark J. Purdy , Wei-Teh Shih , James A. Tallon
CPC分类号： D04C1/06 , B29C70/222 , B29D1/005 , C04B35/806 , C04B35/83 , D04B9/44 , D04C3/48 , D07B5/005 , F16B33/006 , B29K2105/0827 , D07B2201/2086 , D07B2201/209 , F16B2001/0085 , Y10S411/901 , Y10S411/908
摘要： A carbon and/or ceramic fiber reinforced carbon and/or ceramic matrix composite threaded member including a core, a fiber containing thread-defining element bonded to the exterior of the core and a reinforcing fabric layer securing the thread-defining element to the core. The thread-defining element may be an integral part of a tubular braided reinforcing fabric or applied to the core prior to application of a reinforcing fabric layer. Externally and internally threaded members and methods for their manufacture are described.
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