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1. 发明申请

WO2005056262A3 BINDERLESS PREFORM MANUFACTURING METHOD AND MOLD THEREFORE 审中-公开
标题翻译：无边界预制件制造方法和模具
公开(公告)号：WO2005056262A3
公开(公告)日：2005-12-22
申请号：PCT/US2004035660
申请日：2004-10-27
申请人： HONEYWELL INT INC , LA FOREST MARK L , FATZ ALAN E , FRYSKA SLAWOMIR T , SIEGMUND THOMAS H , SOOS BARRY P , GHARBIEH NABIL ABU , CIPRA RAYMOND J , SIMPSON ALLEN H
发明人： LA FOREST MARK L , FATZ ALAN E , FRYSKA SLAWOMIR T , SIEGMUND THOMAS H , SOOS BARRY P , GHARBIEH NABIL ABU , CIPRA RAYMOND J , SIMPSON ALLEN H
IPC分类号： B29B11/12 , B29C33/30 , B29C35/02 , B30B15/00 , B30B15/02 , C04B35/83 , F16D69/02
CPC分类号： B29B11/12 , B29C33/308 , B29C35/02 , B29K2105/0044 , B29K2105/06 , B29K2105/16 , B29L2031/7482 , B30B15/02 , C04B35/83 , C04B2235/48 , C04B2235/604 , F16D69/023
摘要： The present invention makes use of loose fibrous material (for instance, chopped fibers) as reinforcement matrix material in the manufacture of carbon-carbon composites. In accordance with this invention, a constraint fixture is provided which can be separated from the mold. The constraint fixture has an internal shape corresponding to the shape of a desired preform component, with the internal shape being defined by a bottom plate (2), an annular ejector plate (3, 3'), a inner wall (10), an outer wall (4), and an annular top plate (11, 11'). The constraint fixture is normally made of metal, porous ceramic, or carbon material. The constraint fixture of the mold holds the loose matrix materials (fibers, along with any fillers and/or additives). The mold assembly itself is segmented, so that the constraint- fixture and the loose fill materials in the fixture can be removed and subjected to further processing as a unit. Such further processing may include Chemical Vapor Deposition or resin or pitch infiltration or Resin Transfer Molding. The preform matrix may remain in the constraint fixture through such processing steps as densification and until it is removed therefrom for final machining.
摘要翻译：本发明在制造碳 - 碳复合材料时，使用松散的纤维材料（例如短切纤维）作为增强基体材料。根据本发明，提供了可以与模具分离的约束夹具。约束夹具具有对应于所需预成型件部件的形状的内部形状，其内部形状由底板（2），环形顶出板（3,3'），内壁（10），外壁（4）和环形顶板（11,11'）。约束夹具通常由金属，多孔陶瓷或碳材料制成。模具的约束夹具保持松散的基质材料（纤维，以及任何填料和/或添加剂）。模具组件本身被分段，使得夹具中的约束夹具和松散填充材料可以被去除并且作为一个单元被进一步加工。这种进一步的处理可以包括化学气相沉积或树脂或沥青渗透或树脂转移模塑。预成型体基体可以通过诸如致密化的加工步骤保持在约束夹具中，并且直到其从中移除以进行最终加工。

2. 发明申请

WO2005056262A8 BINDERLESS PREFORM MANUFACTURING METHOD AND MOLD THEREFORE 审中-公开
标题翻译：无粘结预制制造方法及其模具
公开(公告)号：WO2005056262A8
公开(公告)日：2005-11-24
申请号：PCT/US2004035660
申请日：2004-10-27
申请人： HONEYWELL INT INC , LA FOREST MARK L , FATZ ALAN E , FRYSKA SLAWOMIR T , SIEGMUND THOMAS H , SOOS BARRY P , GHARBIEH NABIL ABU , CIPRA RAYMOND J , SIMPSON ALLEN H
发明人： LA FOREST MARK L , FATZ ALAN E , FRYSKA SLAWOMIR T , SIEGMUND THOMAS H , SOOS BARRY P , GHARBIEH NABIL ABU , CIPRA RAYMOND J , SIMPSON ALLEN H
IPC分类号： B29B11/12 , B29C33/30 , B29C35/02 , B30B15/00 , B30B15/02 , C04B35/83 , F16D69/02 , B29C
CPC分类号： B29B11/12 , B29C33/308 , B29C35/02 , B29K2105/0044 , B29K2105/06 , B29K2105/16 , B29L2031/7482 , B30B15/02 , C04B35/83 , C04B2235/48 , C04B2235/604 , F16D69/023
摘要： The present invention makes use of loose fibrous material (for instance, chopped fibers) as reinforcement matrix material in the manufacture of carbon-carbon composites. In accordance with this invention, a constraint fixture is provided which can be separated from the mold. The constraint fixture has an internal shape corresponding to the shape of a desired preform component, with the internal shape being defined by a bottom plate (2), an annular ejector plate (3, 3'), a inner wall (10), an outer wall (4), and an annular top plate (11, 11'). The constraint fixture is normally made of metal, porous ceramic, or carbon material. The constraint fixture of the mold holds the loose matrix materials (fibers, along with any fillers and/or additives). The mold assembly itself is segmented, so that the constraint- fixture and the loose fill materials in the fixture can be removed and subjected to further processing as a unit. Such further processing may include Chemical Vapor Deposition or resin or pitch infiltration or Resin Transfer Molding. The preform matrix may remain in the constraint fixture through such processing steps as densification and until it is removed therefrom for final machining.
摘要翻译：本发明利用松散的纤维材料（例如短切纤维）作为碳 - 碳复合材料制造中的增强基体材料。根据本发明，提供了可以与模具分离的约束夹具。约束夹具具有对应于期望的预成形件部件的形状的内部形状，内部形状由底板（2），环形顶出板（3,3'），内壁（10），外壁（4）和环形顶板（11,11'）。约束夹具通常由金属，多孔陶瓷或碳材料制成。模具的约束夹具容纳松散的基体材料（纤维以及任何填料和/或添加剂）。模具组件本身是分段的，因此夹具中的约束夹具和松散填充材料可以被移除并作为一个单元进行进一步处理。这种进一步的处理可以包括化学气相沉积或树脂或沥青渗透或树脂传递模塑。预成型坯基体可以通过致密化之类的处理步骤保留在约束固定装置中，并且直到从预制坯基体中去除以进行最终加工。

3. 发明申请

WO2006039443A3 IMPROVED FORMULATION FOR THE MANUFACTURE OF CARBON-CARBON COMPOSITE MATERIALS 审中-公开
标题翻译：碳碳复合材料制造改进配方
公开(公告)号：WO2006039443A3
公开(公告)日：2006-06-22
申请号：PCT/US2005035096
申请日：2005-09-29
申请人： HONEYWELL INT INC , SIMPSON ALLEN H , SOOS BARRY P , LA FOREST MARK L , FRYSKA SLAWOMIR T
发明人： SIMPSON ALLEN H , SOOS BARRY P , LA FOREST MARK L , FRYSKA SLAWOMIR T
IPC分类号： C04B35/83
CPC分类号： C04B35/83 , C04B35/63496 , C04B2235/602 , C04B2235/604 , C04B2235/614 , C04B2235/656 , C04B2235/6567 , C04B2235/6586 , C04B2235/77 , F16D65/12 , F16D69/023 , F16D2200/0052 , Y10T428/30
摘要： Method for manufacturing a carbonized carbon-carbon composite preform, by: mixing (a) chopped carbon fiber, chopped stabilized pitch fiber, or chopped oxidized polyacrylonitrile (PAN) fiber, (b) thermoplastic pitch binder powder, and (c) activated carbon powder to form a mixture of 1560 parts by weight of chopped carbon fiber or chopped stabilized pitch fiber or chopped oxidized PAN, 28-83 parts by weight of thermoplastic pitch binder powder, and 1-12 parts by weight of activated carbon powder; depositing this mixture into a mold; pressing/heating the materials in the mold to form a preform by compaction; removing the compacted preform from the mold; and carbonizing the compacted preform. The preform is preferably configured in the form of an aircraft landing system brake disc.
摘要翻译：通过以下方法制备碳化碳 - 碳复合预成型体的方法：将（a）短切碳纤维，短切稳定沥青纤维或短切的氧化聚丙烯腈（PAN）纤维，（b）热塑性沥青粘合剂粉末和（c）活性炭粉末形成1560重量份短切碳纤维或短切稳定沥青纤维或短切氧化PAN，28-83重量份热塑性沥青粘合剂粉末和1-12重量份活性炭粉末的混合物; 将该混合物沉积到模具中; 压制/加热模具中的材料以通过压实形成预制件; 从模具中移除压实的预成型件; 并将压实的预成型件碳化。预成型件优选地以飞机着陆系统制动盘的形式配置。

4. 发明申请

WO2006041610A3 FIXTURE FOR HOLDING A PREFORM DURING A HEATING PROCESS 审中-公开
标题翻译：在加热过程中保持预浸料的固定
公开(公告)号：WO2006041610A3
公开(公告)日：2006-05-18
申请号：PCT/US2005032923
申请日：2005-09-15
申请人： HONEYWELL INT INC , SIMPSON ALLEN H , SOOS BARRY P , FRYSKA SLAWOMIR T , LA FOREST MARK L
发明人： SIMPSON ALLEN H , SOOS BARRY P , FRYSKA SLAWOMIR T , LA FOREST MARK L
IPC分类号： B29C33/00 , B29C37/00 , C04B35/83 , F16D69/02
CPC分类号： B29C33/0011 , B29C31/008 , B29C37/005 , B29C71/02 , B29L2031/7482
摘要： A restraint fixture (12) is disclosed that includes a preform retention region configured to limit contracting forces applied against a preform (10) in the preform retention region when the restraint fixture (12) thermally contracts. In one embodiment, the restraint fixture (12) comprises a band (12) having a first surface defining the preform retention region and a first expansion portion (26, 28, 29) adapted to deform upon application of a force to the band.
摘要翻译：公开了一种约束装置（12），其包括预制件保持区域，所述预制件保持区域构造成当所述约束装置（12）热收缩时限制在所述预制件保持区域中施加在预成型件（10）上的收缩力。在一个实施例中，约束装置（12）包括具有限定预成型件保持区域的第一表面的带（12）和适于在对带施加力时变形的第一膨胀部分（26,28,29）。

5. 发明申请

WO2005116476A3 REUSABLE CORE CARBON-CARBON COMPOSITE BRAKE DISC 审中-公开
标题翻译：可重复碳芯碳复合制动盘
公开(公告)号：WO2005116476A3
公开(公告)日：2006-01-26
申请号：PCT/US2005010997
申请日：2005-03-31
申请人： HONEYWELL INT INC , LA FOREST MARK L , JOHNSON DARRELL L , WAHLERS CHRISTOPHER S , FRYSKA SLAWOMIR T
发明人： LA FOREST MARK L , JOHNSON DARRELL L , WAHLERS CHRISTOPHER S , FRYSKA SLAWOMIR T
IPC分类号： F16D65/00 , F16D65/12 , F16D69/00 , F16D69/02 , F16D69/04
CPC分类号： C04B35/83 , C04B2235/614 , C04B2235/616 , C04B2235/75 , C04B2235/77 , F16D65/12 , F16D69/023 , F16D69/04 , F16D2069/002 , F16D2069/005 , F16D2069/0491 , Y10T29/49956 , Y10T156/10
摘要： Method of manufacturing carbon-carbon composite brake disc (5, 17, 35) comprising a dense reusable core 7, 19, 37). Preferably, the reusable core has a density of 1 .8-2.05 g/cc. The method includes: forming a dense carbon-carbon composite core; positioning the dense core in a location within a carbon-carbon composite brake disc; and fixing the dense carbon-carbon composite core in place in its location within the carbon-carbon composite brake disc. It is economically advantageous to recover the dense core from a worn brake disc prior to positioning it in the brake disc. Also, an annular carbon-carbon composite brake disc made up of a friction surface containing 15-75 weight-% carbon-containing fibers and 25-85 weight-% resin binder and a dense carbon-carbon composite core comprising 40-75 weight-% carbon-containing fibers and 25-60 weight-% resin binder.
摘要翻译：制造碳 - 碳复合制动盘（5,17,35）的方法，其包括密集的可重复使用的芯7,19,37）。优选地，可重复使用的芯的密度为1.8-2.05g / cc。该方法包括：形成致密的碳 - 碳复合芯; 将致密核心定位在碳 - 碳复合制动盘内的位置; 并将致密的碳 - 碳复合材料芯固定在碳 - 碳复合制动盘内的位置。在将其定位在制动盘中之前，从磨损的制动盘回收致密的核心在经济上是有利的。另外，由含有15-75重量％含碳纤维和25-85重量％树脂粘合剂的摩擦表面和一个含有40-75重量％的含碳纤维的密集碳 - 碳复合材料芯构成的环形碳 - 碳复合制动盘，％含碳纤维和25-60重量％树脂粘合剂。

6. 发明申请

WO2006101799A3 CARBON FIBER CONTAINING CERAMIC PARTICLES 审中-公开
标题翻译：碳纤维含有陶瓷颗粒
公开(公告)号：WO2006101799A3
公开(公告)日：2006-12-07
申请号：PCT/US2006008878
申请日：2006-03-13
申请人： HONEYWELL INT INC , FRYSKA SLAWOMIR T , SIMPSON ALLEN H , LAFOREST MARK L
发明人： FRYSKA SLAWOMIR T , SIMPSON ALLEN H , LAFOREST MARK L
IPC分类号： C04B35/83 , D01F1/10 , D01F9/12
CPC分类号： D06M11/74 , C04B35/6286 , C04B35/62863 , C04B35/62892 , C04B35/83 , C04B2235/3826 , C04B2235/3843 , C04B2235/48 , C04B2235/5248 , C04B2235/5264 , C04B2235/5436 , D06M23/08 , D06M2101/40 , D06M2200/40 , F16D69/023 , F16D2200/0065 , Y10T428/213 , Y10T428/249928 , Y10T428/292 , Y10T428/30
摘要： Small ceramic particles (e.g., of TiC) are incorporated into fibers. The ceramic particles enhance the friction and/or wear properties of a carbon-carbon composite article made with the impregnated or coated f ibers. The impregnated fibers can be, e.g., polyacrylonitrile (PAN) fibers, pitch f ibers, and other such fibers as are commonly employed in the manufacture of C-C friction materials. The impregnated f ibers can be used to make woven, nonwoven, or random fiber preforms or in other known preform types. Preferred products are brake discs and other components of braking systems. The particles may be included in the fibers by mixing them with the resin employed to make the fibers and/or by applying them to the surfaces of the fibers in a binder.
摘要翻译：将小的陶瓷颗粒（例如TiC）掺入纤维中。陶瓷颗粒增强了用浸渍或涂布的织物制成的碳 - 碳复合制品的摩擦和/或耐磨性能。浸渍的纤维可以是例如聚丙烯腈（PAN）纤维，沥青纤维，以及其他通常用于制造C-C摩擦材料的纤维。浸渍的纤维可用于制造编织物，无纺布或无规纤维预制件或其它已知的预型件。优选的产品是制动盘和制动系统的其他部件。通过将它们与用于制造纤维的树脂混合，和/或通过将其施加到纤维的粘合剂表面中，将颗粒包含在纤维中。

7. 发明申请

WO2006101799A8 CARBON FIBER CONTAINING CERAMIC PARTICLES 审中-公开
标题翻译：碳纤维含有陶瓷颗粒
公开(公告)号：WO2006101799A8
公开(公告)日：2007-05-24
申请号：PCT/US2006008878
申请日：2006-03-13
申请人： HONEYWELL INT INC , FRYSKA SLAWOMIR T , SIMPSON ALLEN H , LAFOREST MARK L
发明人： FRYSKA SLAWOMIR T , SIMPSON ALLEN H , LAFOREST MARK L
IPC分类号： C04B35/83 , D01F1/10 , D01F9/12
CPC分类号： D06M11/74 , C04B35/6286 , C04B35/62863 , C04B35/62892 , C04B35/83 , C04B2235/3826 , C04B2235/3843 , C04B2235/48 , C04B2235/5248 , C04B2235/5264 , C04B2235/5436 , D06M23/08 , D06M2101/40 , D06M2200/40 , F16D69/023 , F16D2200/0065 , Y10T428/213 , Y10T428/249928 , Y10T428/292 , Y10T428/30
摘要： Small ceramic particles (e.g., of TiC) are incorporated into fibers. The ceramic particles enhance the friction and/or wear properties of a carbon-carbon composite article made with the impregnated or coated f ibers. The impregnated fibers can be, e.g., polyacrylonitrile (PAN) fibers, pitch f ibers, and other such fibers as are commonly employed in the manufacture of C-C friction materials. The impregnated f ibers can be used to make woven, nonwoven, or random fiber preforms or in other known preform types. Preferred products are brake discs and other components of braking systems. The particles may be included in the fibers by mixing them with the resin employed to make the fibers and/or by applying them to the surfaces of the fibers in a binder.
摘要翻译：将小的陶瓷颗粒（例如TiC）掺入纤维中。陶瓷颗粒增强了用浸渍或涂布的织物制成的碳 - 碳复合制品的摩擦和/或耐磨性能。浸渍的纤维可以是例如聚丙烯腈（PAN）纤维，沥青纤维，以及其他通常用于制造C-C摩擦材料的纤维。浸渍的纤维可用于制造编织物，无纺布或无规纤维预制件或其它已知的预型件。优选的产品是制动盘和制动系统的其他部件。通过将它们与用于制造纤维的树脂混合，和/或通过将其施加到纤维的粘合剂表面中，将颗粒包含在纤维中。

8. 发明专利

ES2283559T3 DISCOS DE FRICCION DE MATERIAL COMPUESTO CON UN NUCLEO ESTRUCTURAL Y ELEMENTOS DE CAMISA RESTAURABLES. 未知
公开(公告)号：ES2283559T3
公开(公告)日：2007-11-01
申请号：ES02734615
申请日：2002-06-04
申请人： HONEYWELL INT INC
发明人： FRYSKA SLAWOMIR T , SCELSI ANTHONY
IPC分类号： F16D65/12 , F16D69/00 , F16D69/04
摘要： Un disco de fricción para un conjunto de freno que comprende: un núcleo estructural anular (40) que tiene al menos una superficie (41) de montaje con forma sinusoidal, y al menos un elemento (30) de camisa de fricción que tiene una superficie (31) de montaje con forma sinusoidal y una superficie (32) de desgaste, relativamente plana, axialmente opuesta a dicha superficie (31) de montaje de forma sinusoidal; aplicándose de forma acoplable dicha superficie (31) de montaje de cada elemento (30) de camisa de fricción a dicha superficie (41) de dicho núcleo estructural (40).

9. 发明专利

DE60219465D1 未知
公开(公告)号：DE60219465D1
公开(公告)日：2007-05-24
申请号：DE60219465
申请日：2002-06-04
申请人： HONEYWELL INT INC
发明人： FRYSKA SLAWOMIR T , SCELSI ANTHONY
IPC分类号： F16D65/12 , F16D69/00 , F16D69/04
摘要： A friction disc assembly having an annular structural core ( 40 ) and at least one friction lining disc ( 30 ). The annular structural core ( 40 ) is made from a strength-optimized carbon carbon composite and the friction lining discs ( 30 ) from a friction-optimized carbon carbon composite. Each friction lining disc ( 30 ) is provided with a mounting surface ( 31 ) and a wear surface ( 32 ). The structural core ( 40 ) includes at least one mounting surface ( 41 ). The mounting surfaces ( 31,41 ) may include corresponding sinusoidally-shaped wave patterns for increasing the surface area of a contact zone between the friction lining discs ( 30 ) and a reusable structural core ( 40 ).

10. 发明专利

DE602007003819D1 未知
公开(公告)号：DE602007003819D1
公开(公告)日：2010-01-28
申请号：DE602007003819
申请日：2007-03-27
申请人： HONEYWELL INT INC
发明人： SIMPSON ALLAN H , FRYSKA SLAWOMIR T , LA FOREST MARK L , MUKASYAN ALEXANDER
IPC分类号： C04B37/00 , B32B18/00 , C04B35/83 , F16D69/02
摘要： Method of joining carbon-carbon composite pieces together, e.g. in the refurbishment of aircraft brake discs. The method includes the steps of: providing a first carbon-carbon composite piece and a second carbon-carbon composite piece, wherein the second carbon-carbon composite piece has a surface that is complementary to a surface of said first carbon-carbon composite piece; providing a layer of a mixture of titanium powder and carbon powder on the first complementary mating surface; arranging the second carbon-carbon composite piece on the powder layer such that the second complementary mating surface is matched to the first complementary mating surface, thereby forming a construct of the first carbon-carbon composite piece, the powder layer, and the second carbon-carbon composite piece; placing the construct into a press and applying pressure to the construct to press together the two pieces joined at their complementary surfaces; and applying an electrical current to the powder in the construct to initiate an oxidation-reduction reaction, thereby bonding the carbon-carbon composite pieces together.

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