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1. 发明授权

US5599603A Manufacture of carbon fibre preform 失效
标题翻译：碳纤维预制件的制造
公开(公告)号：US5599603A
公开(公告)日：1997-02-04
申请号：US202890
申请日：1994-02-28
申请人： Maurice J. Evans , Keith A. Williams , Ronald Fisher
发明人： Maurice J. Evans , Keith A. Williams , Ronald Fisher
IPC分类号： C04B35/83 , B32B5/02 , D04H1/4242 , D04H1/46 , D04H1/52 , F16D65/12 , F16D69/02 , B32B3/02
CPC分类号： C04B35/83 , B32B1/08 , B32B19/00 , B32B27/02 , B32B5/26 , B32B7/08 , D04H1/4242 , D04H1/46 , D04H1/52 , F16D69/023 , C04B2235/5268 , C04B2235/604 , Y10T428/21 , Y10T428/213 , Y10T428/218 , Y10T428/30 , Y10T442/682
摘要： In a method of making a carbon fibre preform such as for use in the manufacture of a friction disc a compressible body of carbon fibre or carbon fibre precursor material is acted upon by compressing means to compress the body to a required thickness and then operated upon by means such as a barbed needle-punch needle for a stitching thread which penetrates substantially the whole thickness of the body whereby the compressed preform may be removed from action by the compressing means in a free-standing and compressed state. If the method uses carbon fibre precursor material, that is then subjected to carbonization.
摘要翻译：在制造用于制造摩擦盘的碳纤维预成型件的方法中，碳纤维或碳纤维前体材料的可压缩体通过压缩装置作用，以将本体压缩至所需厚度，然后由用于缝合线的有刺刺针针的装置，其穿透主体的整个厚度，由此压缩预成型件可以通过压缩装置以独立和压缩的状态从动作中移除。如果该方法使用碳纤维前体材料，则将其进行碳化。

2. 发明授权

US5503893A Ultra-high performance carbon composites 失效
标题翻译：超高性能碳复合材料
公开(公告)号：US5503893A
公开(公告)日：1996-04-02
申请号：US246228
申请日：1994-05-18
申请人： Maurice J. Evans , Ronald Fisher , Keith A. Williams
发明人： Maurice J. Evans , Ronald Fisher , Keith A. Williams
IPC分类号： B29B11/16 , B29C70/24 , B29K105/08 , B29K307/04 , B32B5/00 , B32B5/02 , B32B5/06 , B32B5/12 , B32B7/02 , C04B35/52 , C04B35/83 , D01F9/12 , D04H1/4242 , D04H1/498 , D04H1/593 , D04H13/00 , F16D69/02 , B32B31/16 , B32B31/26 , D04H5/02
CPC分类号： D04H1/4242 , B29C70/24 , B32B7/02 , C04B35/83 , D04H1/498 , D04H1/593 , D04H13/00 , F16D69/023 , B29K2307/00 , Y10S376/904 , Y10T428/24099 , Y10T428/24107 , Y10T428/24132 , Y10T428/24942 , Y10T428/30 , Y10T442/662 , Y10T442/687
摘要： Method of fabricating a multi-ply carbon fibre fabric, preform or composite material from a layer of unidirectionally aligned carbon fibres of ultra-high modulus and a layer of low modulus carbon fibre comprising the steps of: arranging in superimposed relationship the layer of unidirectionally aligned carbon fibres of ultra-high modulus and the layer of low modulus carbon fibres so that at least a substantial number of the fibres of low modulus are disposed transversely of the fibres of the ultra-high modulus fibre layer, and connecting the two layers by interlacing fibres of the layer of low modulus fibres with those of the layer of ultra-high modulus fibres by needle-punching using felting needles orientated and configured so that their barbs snag only the low modulus fibres during passage through the layers.
摘要翻译：从超高模量的单向排列碳纤维层和低模量碳纤维层制造多层碳纤维织物，预成型件或复合材料的方法，包括以下步骤：以叠加关系布置单向对准的层超高模量的碳纤维和低模量碳纤维层，使得至少相当数量的低模量的纤维横向于超高模量纤维层的纤维设置，并且通过交织连接两层低模量纤维层的纤维与超高模量纤维层的纤维通过使用定向和构造的毡针进行针刺冲切，使得它们的倒钩在通过层期间仅阻挡低模量纤维。

3. 发明授权

US5547737A Light-weight, high-strength, stiff panels 失效
标题翻译：重量轻，高强度，刚性面板
公开(公告)号：US5547737A
公开(公告)日：1996-08-20
申请号：US303671
申请日：1994-09-09
申请人： Maurice J. Evans , Sharon L. Faulkner , Ronald Fisher , Trevor C. Wells , Paul Hadlum
发明人： Maurice J. Evans , Sharon L. Faulkner , Ronald Fisher , Trevor C. Wells , Paul Hadlum
IPC分类号： B29D24/00 , B32B3/20 , B32B5/28 , B64C1/00 , C04B35/83 , E04C2/34 , B32B3/12
CPC分类号： B64C1/12 , B29D24/008 , B32B3/20 , B32B5/28 , C04B35/83 , E04C2/3405 , B64C2001/0072 , E04C2002/345 , E04C2002/3477 , Y02T50/433 , Y10T428/24661 , Y10T428/24744
摘要： A method for the manufacture of a light-weight panel, e.g. for aircraft, comprising preparing a panel preform having a pair of surface members or skins (29, 30) separated and supported by an internal core (26-28) in which spaces or interconnected pores provide vents to an edge of the panel, the wall surface members and the core comprising fibrous material, which may be carbon fibre, and using a pyrolysis process such as CVD to form a pyrolyric matrix around the fibres within the fibrous material, there being a flow of gas through the vents during the pyrolysis process.
摘要翻译：一种用于制造轻质面板的方法，例如，用于飞行器，包括制备具有一对表面构件或表皮（29,30）的面板预成型件，所述表面构件或表面（29,30）由内部芯（26-28）分隔和支撑，在所述内部芯（26-28）中空间或互连的孔向所述面板的边缘提供通风口，表面构件和包含纤维材料的芯，其可以是碳纤维，并且使用诸如CVD的热解方法在纤维材料内的纤维周围形成热解基质，在热解过程期间存在通过通气孔的气流。

4. 发明授权

US5503254A Toughened carbon composite brake discs 失效
标题翻译：增韧碳复合制动盘
公开(公告)号：US5503254A
公开(公告)日：1996-04-02
申请号：US128571
申请日：1993-09-30
申请人： Ronald Fisher , Thomas G. Fennell , Maurice J. Evans
发明人： Ronald Fisher , Thomas G. Fennell , Maurice J. Evans
IPC分类号： F16D55/00 , F16D55/36 , F16D55/40 , F16D65/12 , F16D69/00 , F16D69/02
CPC分类号： F16D55/40 , F16D55/36 , F16D65/126 , F16D69/023 , F16D2055/0058 , F16D2069/002 , F16D65/127
摘要： An aircraft disc stack (1) comprises a plurality of interleaved stator and rotor discs (3,4) keyed respectively to a torque tube (5) and a wheel hub (not shown). The stack (1) further comprises bi-functional friction/load transmitting discs in the form of end stator discs (10,13). These discs (10,13) are subject to uneven loading because the non-friction surfaces (12,15) are in use compressed on areas less than the load bearing areas of the opposing friction faces (11,14). This can lead to premature disc failure and in the past load spreader plates have been used to distribute loading over these areas to minimize the risk of failure. In this invention portions of the load bearing areas of non-friction surfaces (12,15) are toughened ie: material underlying these surfaces is toughened, to increase their resistance to deformation, fracture and/or wear thereby removing the need for additional load spreader plates which were hitherto required.
摘要翻译：飞机盘堆叠（1）包括分别键合到扭矩管（5）和轮毂（未示出）的多个交错的定子和转子盘（3,4）。堆（1）还包括端定子盘（10,13）形式的双功能摩擦/载荷传递盘。由于非摩擦表面（12,15）在比相对的摩擦面（11,14）的承载区域小的区域上被压缩，所以这些盘（10,13）承受不均匀的载荷。这可能导致过早的盘故障，并且在过去的负载中，吊具板已经用于在这些区域上分配负载以最小化故障的风险。在本发明中，非摩擦表面（12,15）的承载区域的部分是增韧的，即：这些表面下面的材料被增韧，以增加它们对变形，断裂和/或磨损的抵抗力，从而消除对额外负载撒布机的需要迄今为止所需的板材。

5. 发明授权

US5360500A Method of producing light-weight high-strength stiff panels 失效
标题翻译：生产轻质高强度强板的方法
公开(公告)号：US5360500A
公开(公告)日：1994-11-01
申请号：US190615
申请日：1994-02-02
申请人： Maurice J. Evans , Sharon L. Faulkner , Ronald Fisher , Trevor C. Wells , Paul Hadlum
发明人： Maurice J. Evans , Sharon L. Faulkner , Ronald Fisher , Trevor C. Wells , Paul Hadlum
IPC分类号： B29D24/00 , B32B3/20 , B32B5/28 , B64C1/00 , C04B35/83 , E04C2/34 , C23C16/26 , C23C16/44
CPC分类号： B64C1/12 , B29D24/008 , B32B3/20 , B32B5/28 , C04B35/83 , E04C2/3405 , B64C2001/0072 , E04C2002/345 , E04C2002/3477 , Y02T50/433 , Y10T428/24661 , Y10T428/24744
摘要： A method for the manufacture of a light-weight panel, e.g. for aircraft, comprising preparing a panel preform having a pair of surface members or skins separated and supported by an internal core in which spaces or interconnected pores provide vents to an edge of the panel, the wall surface members and the core comprising fibrous material, which may be carbon fiber, and using a pyrolysis process such as CVD to form a pyrolytic matrix around the fibers within the fibrous material, there being a flow of gas through the vents during the pyrolysis process.
摘要翻译：一种用于制造轻质面板的方法，例如，用于飞机，包括制备具有一对表面构件或表皮的面板预成型件，所述表面构件或表皮由内部芯部分隔并支撑，其中空间或互连的孔向所述面板的边缘提供通风口，所述壁表面构件和所述芯包括纤维材料，可以是碳纤维，并且使用诸如CVD的热解方法在纤维材料内的纤维周围形成热解基质，在热解过程期间存在通过通气孔的气流。

6. 发明授权

US4029829A Friction member 失效
标题翻译：摩擦件
公开(公告)号：US4029829A
公开(公告)日：1977-06-14
申请号：US544575
申请日：1975-01-27
申请人： John Victor Weaver , Ronald Fisher
发明人： John Victor Weaver , Ronald Fisher
IPC分类号： F16C33/18 , C04B35/52 , C04B35/83 , C08J5/14 , C09K3/14 , C10M103/02 , C10N20/06 , C10N40/00 , C10N40/02 , C10N50/08 , C10N70/00 , F16C33/12 , F16D65/12 , F16D69/00 , F16D69/02 , C01B31/04 , B32B5/02 , C23C11/10
CPC分类号： C04B35/83 , F16D69/023 , F16D65/126 , Y10S428/902 , Y10T428/24992 , Y10T428/292 , Y10T428/30 , Y10T428/31
摘要： The invention provides a more economical carbon-fiber-reinforced carbon surfaced friction member, such as a brake disc, by replacing a disc which is of fiber-reinforced carbon throughout its thickness by a disc in which a fiber-reinforced surface layer is bonded to a base of a less expensive material, such as bulk graphite. A textile may be applied to the base and carbonized and carbon deposited on the textile layer by the multiple impregnation process or the chemical vapor deposition process. In the latter process the base is preferably heated above the temperature of the textile layer, e.g. by electrical induction or resistance, to obtain carbon deposition from the base outward through the textile layer.
摘要翻译：本发明提供了一种更经济的碳纤维增强碳表面摩擦件，例如制动盘，通过用纤维增强表面层粘合到其上的盘来替换纤维增强碳的整个厚度的盘一种较便宜的材料的基体，例如体积石墨。纺织品可以通过多次浸渍方法或化学气相沉积工艺施加到基底上并且碳化和沉积在织物层上的碳。在后一种方法中，优选将基底加热到高于织物层的温度，例如通过电感应或电阻，从基底向外通过织物层获得碳沉积。

7. 发明授权

US4212906A Method for the production of carbon/carbon composite material 失效
标题翻译：生产碳/碳复合材料的方法
公开(公告)号：US4212906A
公开(公告)日：1980-07-15
申请号：US943854
申请日：1978-09-19
申请人： Ronald Fisher , Norman Smith
发明人： Ronald Fisher , Norman Smith
IPC分类号： C23C16/04 , C23C16/455 , D01F11/10 , D01F11/12 , B05D3/12
CPC分类号： D01F11/125 , C23C16/045 , C23C16/455 , D01F11/10
摘要： In the production of all-carbon composite articles by the cracking of a hydrocarbon gas to deposit carbon on a fibrous carbon substrate the substrate is held in the furnace by a ram movable in the furnace to engage the substrate. The gas is introduced inside the annular substrate and evacuated at a position spaced laterally from the substrate so that the gas is forced to disperse through the substrate wall.
摘要翻译：在通过裂解碳氢化合物气体以将碳沉积在纤维状碳基体上的全碳复合制品的生产中，基板通过可在炉中移动的柱塞保持在炉中，从而与基板接合。将气体引入到环形基板的内部并且在与衬底横向间隔开的位置处抽空，使得气体被迫分散通过衬底壁。

8. 发明授权

US06416824B2 Densification 失效
标题翻译：致密化
公开(公告)号：US06416824B2
公开(公告)日：2002-07-09
申请号：US09737730
申请日：2000-12-15
申请人： Ronald Fisher , Alan Frank Tibbatts
发明人： Ronald Fisher , Alan Frank Tibbatts
IPC分类号： H05B602
CPC分类号： H05B6/105 , C04B35/571 , C04B35/806 , C04B35/83 , C23C16/045 , F16D69/023
摘要： A method of deposing a carbon-containing substance in the pores of a porous body comprises establishing an open varying magnetic field flux loop and placing the body such that a magnetic field flux generated by the open magnetic field flux loop passes through a region of said body and heats that region, creating a thermal gradient across the body and bringing a thermally decomposable carbon-containing gas into contact with the heated region, thereby depositing a carbon-containing substance in the pores if said heated region.
摘要翻译：在多孔体的孔中含有碳物质的方法包括：建立开放变化的磁场通量回路并放置体，使得由开放磁场通量环产生的磁场通量通过所述体的区域并加热该区域，在身体上产生热梯度并使可热分解的含碳气体与加热区域接触，从而如果所述加热区域在孔中沉积含碳物质。

9. 发明授权

US06177146B1 Densification of a porous structure (III) 失效
标题翻译：多孔结构（III）的致密化
公开(公告)号：US06177146B1
公开(公告)日：2001-01-23
申请号：US09202691
申请日：1998-12-21
申请人： Ronald Fisher , Keith Williams
发明人： Ronald Fisher , Keith Williams
IPC分类号： G23C1626
CPC分类号： F16D69/023 , C04B35/83 , C23C16/045 , C23C16/26 , C23C16/46 , Y10T428/213 , Y10T428/24322 , Y10T428/249928 , Y10T428/249931 , Y10T428/249986 , Y10T428/24999 , Y10T428/30
摘要： A method for the densification of an annular body having a porous structure and comprising layers of fabric, which includes locating a susceptor element within the porous body, the amount of the susceptor element occupying less than 5% of the volume of the porous body, the susceptor element being in the form of a layer comprising one of a foil and a fiber and having plural holes therein through which adjacent layers of fabric of the porous body contact each other, said susceptor element being made of a material which is more susceptible to heating by electromagnetic radiation than the material of the porous body, and exposing the porous body to hydrocarbon gas and simultaneously applying an electromagnetic field to the porous body, the susceptor element within the porous body at least in part causing heating of the porous body to a temperature at which the gas infiltrating the porous body deposits carbon within the porous body.
摘要翻译：一种用于致密化具有多孔结构并且包括织物层的环形体的方法，其包括将基座元件定位在多孔体内，基座元件的量占多孔体的体积的5％以下，感受元件为包括箔和纤维之一的层的形式，并且具有多个孔，多孔体的相邻层彼此接触，所述基座元件由更容易加热的材料制成通过电磁辐射而不是多孔体的材料，并且将多孔体暴露于烃气体并同时向多孔体施加电磁场，多孔体内的基座元件至少部分地导致多孔体的加热至温度渗透多孔体的气体在多孔体内沉积碳。

10. 发明授权

US5230946A Carbon-carbon composite materials 失效
标题翻译：碳碳复合材料
公开(公告)号：US5230946A
公开(公告)日：1993-07-27
申请号：US417484
申请日：1989-10-05
申请人： Ronald Fisher
发明人： Ronald Fisher
IPC分类号： B32B5/08 , F16D65/12 , F16D69/02
CPC分类号： B32B5/08 , F16D65/126 , F16D69/023 , F16D65/127 , Y10T428/24124 , Y10T428/24132 , Y10T428/24942 , Y10T428/30
摘要： A coated carbon-carbon composite of the kind incorporating carbon fibres in a carbon matrix also incorporates in at least a region (2) thereof other fibres of a different axial coefficient of thermal expansion from that of the carbon fibres, the other fibres being arranged in relation to adjacent carbon fibres so as to provide in combination with the carbon matrix a coefficient of thermal expansion of that region (2) of the composite which is compatible with that of an anti-oxidation coating (1) on the surface of that region.
摘要翻译：在碳基体中并入碳纤维的涂层碳 - 碳复合材料也至少在其中具有不同于碳纤维轴向热膨胀系数的其它纤维的区域（2）中，其它纤维被布置在与相邻的碳纤维相关联，以便与碳基体组合提供与该区域的表面上的抗氧化涂层（1）相适应的复合材料区域（2）的热膨胀系数。

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