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1. 发明授权

US06346304B1 Densification of a porous structure (II) 失效
标题翻译：多孔结构的致密化（II）
公开(公告)号：US06346304B1
公开(公告)日：2002-02-12
申请号：US09202692
申请日：1998-12-21
申请人： Ronald Fisher , Keith Williams
发明人： Ronald Fisher , Keith Williams
IPC分类号： C23C1600
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： At least one layer of fibers of a material susceptible to heating by electromagnetic radiation is incorporated in a porous structure. The structure is subjected to the radiation to heat up the body which is contacted with hydrocarbon gas to cause the gas to deposit carbon within the porous structure and thereby cause densification.
摘要翻译：通过电磁辐射加热的材料的至少一层纤维被并入多孔结构中。该结构经受辐射以加热与烃气体接触的主体，以使气体将碳沉积在多孔结构内，从而导致致密化。

2. 发明授权

US06180223B2 Densification of a porous structure 失效
标题翻译：多孔结构的致密化
公开(公告)号：US06180223B2
公开(公告)日：2001-01-30
申请号：US09202720
申请日：1998-12-21
申请人： Ronald Fisher , Keith Williams
发明人： Ronald Fisher , Keith Williams
IPC分类号： B32B522
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 a porous structure comprises providing the structure with a body of material (13, 14) which includes a susceptor element foil (14) which is more susceptible to heating by electromagnetic radiation than the other material (13) of the body, exposing said porous structure to hydrocarbon gas and simultaneously applying an electromagnetic field to said porous structure whereby said susceptor element (14) at least in part causes heating of the porous structure to a temperature at which the gas infiltrating the porous structure deposits carbon within the porous structure.
摘要翻译：用于致密化多孔结构的方法包括为所述结构提供材料体（13,14），所述材料体包括感受器元件箔（14），所述感受体元件箔（14）比电磁辐射的其它材料（13）更容易被电磁辐射加热将所述多孔结构暴露于烃气体并同时向所述多孔结构施加电磁场，由此所述基座元件（14）至少部分地使所述多孔结构的加热导致渗透所述多孔结构的气体沉积碳的温度多孔结构。

3. 发明授权

US5782320A Toughened carbon composite brake discs 失效
标题翻译：增韧碳复合制动盘
公开(公告)号：US5782320A
公开(公告)日：1998-07-21
申请号：US882958
申请日：1997-06-26
申请人： Ronald Fisher , Thomas Gerard Fennell , Maurice James Evans
发明人： Ronald Fisher , Thomas Gerard Fennell , Maurice James Evans
IPC分类号： F16D55/00 , F16D55/36 , F16D55/40 , F16D65/12 , F16D69/00 , F16D69/02 , B00T1/06
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，负载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，从而消除了对附加负载撒布机的需要迄今为止所需的板材。

4. 发明授权

US4526616A Load-bearing thermal insulator 失效
标题翻译：承重热绝缘子
公开(公告)号：US4526616A
公开(公告)日：1985-07-02
申请号：US513090
申请日：1983-07-12
申请人： Thomas G. Fennell , Ronald Fisher
发明人： Thomas G. Fennell , Ronald Fisher
IPC分类号： F16D65/14 , F16D65/18 , F16D65/84 , F16L59/02 , C07C29/00
CPC分类号： F16L59/028 , F16D65/84 , F16D2065/785 , F16D2125/06 , Y10T428/251 , Y10T428/2911
摘要： A load-bearing thermal insulator, for example a brake piston thrust transmission element, which comprises platelets or flakes of thermally insulating material dispersed in a metal matrix and oriented normal to the direction of heat flow so as to impede the flow of heat through the matrix in one direction.
摘要翻译：承载热绝缘体，例如制动活塞推力传动元件，其包括分散在金属基体中并且垂直于热流方向定向的绝热材料的薄片或薄片，以阻止热通过基体的热量在一个方向。

5. 发明授权

US07219449B1 Adaptively controlled footwear 失效
标题翻译：适应性强的鞋类
公开(公告)号：US07219449B1
公开(公告)日：2007-05-22
申请号：US10870194
申请日：2004-06-17
申请人： Steven M. Hoffberg , Ronald Fisher
发明人： Steven M. Hoffberg , Ronald Fisher
IPC分类号： A43B7/14
CPC分类号： A43B7/02 , A43B1/0054 , A43B3/0005 , A43B3/0015 , A43B3/0026 , A43B7/04 , A43B7/06 , A43B7/14 , A43B7/1415 , A43B13/14 , A43B13/181 , A43B13/189
摘要： A method for controlling footwear, comprising cushioning a transient force during use of the footwear at a first period of a gait cycle, storing energy from said cushioning, and releasing the stored energy during use of the footwear at a second period of the gait cycle, and after said transient force has subsided. The control can be electronic, mechanical or hydraulic, and is preferably dependent on a sensed gait cycle phase. The control may be adaptive to the user or the use of the footwear. The stored energy can be used to assist in locomotion, to generate electrical energy, to drive a heat pump, or simply dissipated.
摘要翻译：一种用于控制鞋类的方法，包括在步态周期的第一阶段缓冲使用鞋类期间的瞬时力，存储来自所述缓冲的能量，以及在所述步态周期的第二周期期间释放所述鞋类使用期间的储存能量，之后瞬态力已经消退。控制可以是电子的，机械的或液压的，并且优选地依赖于感测的步态循环阶段。控制可以适应用户或使用鞋类。存储的能量可以用于帮助运动，产生电能，驱动热泵或简单消散。

6. 发明授权

US5634535A Composite brake disc 失效
标题翻译：复合制动盘
公开(公告)号：US5634535A
公开(公告)日：1997-06-03
申请号：US613122
申请日：1996-03-08
申请人： Thomas G. Fennell , Ronald Fisher , David C. Johnson , Lynda M. Perks
发明人： Thomas G. Fennell , Ronald Fisher , David C. Johnson , Lynda M. Perks
IPC分类号： F16D65/12 , F16D69/02 , F16D55/36
CPC分类号： F16D69/023 , F16D65/126
摘要： In a composite brake disc such as a carbon composite brake disc having reinforcement provided by layers of carbon fibre material, the drive region is provided with additional reinforcement to that of the friction region by laying or otherwise providing additional fibre reinforcement material substantially uniformly in the drive region.
摘要翻译：在具有由碳纤维材料层提供的加强件的碳复合制动盘的复合制动盘中，通过在驱动器中基本上均匀地铺设或以其它方式提供额外的纤维增强材料，驱动区域被提供到摩擦区域的附加加强件地区。

7. 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。

8. 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。

9. 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。

10. 发明授权

US4134360A Apparatus for vapor deposition on tubular substrate 失效
标题翻译：用于蒸气沉积在管状基底上的装置
公开(公告)号：US4134360A
公开(公告)日：1979-01-16
申请号：US822824
申请日：1977-08-08
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 , C23C13/08
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。

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