公开(公告)号：US20240317635A1

公开(公告)日：2024-09-26

申请号：US18186785

申请日：2023-03-20

申请人： Goodrich Corporation

发明人： Zhongfen Ding ,  Steven Poteet ,  John S. Linck ,  Xia Tang ,  Richard Wesley Jackson, III ,  Michael Miller ,  Virginia E. Collier ,  Hans L. Lehermeier

IPC分类号： C03C8/22 ,  C03C8/08 ,  C03C8/14 ,  C04B35/83 ,  C04B41/00 ,  C04B41/45 ,  C04B41/50 ,  C04B41/52 ,  C04B41/86 ,  C04B41/89

CPC分类号： C03C8/22 ,  C03C8/08 ,  C03C8/14 ,  C04B35/83 ,  C04B41/0072 ,  C04B41/4539 ,  C04B41/5022 ,  C04B41/522 ,  C04B41/86 ,  C04B41/89 ,  C03C2209/00 ,  C04B2235/422 ,  C04B2235/5248 ,  F16D2200/0039 ,  F16D2200/0052 ,  F16D2200/0078 ,  F16D2250/0046

摘要： A method for forming an oxidation protection system on a carbon-carbon composite structure can comprise applying a boron slurry to the carbon-carbon composite structure, wherein the boron slurry comprises a boron compound, a first glass mixture, a first glass former, a first glass modifier, and a first carrier fluid, the first glass mixture including a first glass compound and a second glass compound, the first glass compound having a first viscosity-temperature profile that is at least one order of magnitude below a second viscosity-temperature profile of the second glass compound; applying a silicon slurry to the carbon-carbon composite structure, wherein the silicon slurry comprises a silicon compound, a third glass compound, a second glass former, a second glass modifier, and a second carrier fluid; and heating the carbon-carbon composite structure.

公开(公告)号：US20240278499A1

公开(公告)日：2024-08-22

申请号：US18111452

申请日：2023-02-17

申请人： Lawrence Livermore National Security, LLC

发明人： James LEWICKI

IPC分类号： B29C64/30 ,  B29C64/118 ,  B33Y10/00 ,  B33Y30/00 ,  B33Y40/20 ,  C04B35/624 ,  C04B35/626 ,  C04B35/64 ,  C04B35/83

CPC分类号： B29C64/30 ,  B29C64/118 ,  B33Y10/00 ,  B33Y30/00 ,  B33Y40/20 ,  C04B35/624 ,  C04B35/6269 ,  C04B35/64 ,  C04B35/83 ,  C04B2235/422 ,  C04B2235/48 ,  C04B2235/5248 ,  C04B2235/6026

摘要： Systems for manufacturing a Stage 1 carbon-carbon (CC) part, including a resin infused with at least one of chopped fibers, milled fibers, or a continuous fiber. The resin further may include at least one UV initiator to render the resin UV gellable upon exposure to UV light. An additive manufacturing (AM) system determines and provides tool paths needed to provide an engineered characteristic to the Stage 1 CC part. A print nozzle component of the AM system extrudes the resin in accordance with the tool paths onto a sacrificial support material layer, such that the fiber(s) are deposited in desired orientations, within each layer, in a layer-by-layer printing operation. A UV light illuminates the resin after extrusion to initiate gelation of the resin as the resin is extruded onto the sacrificial material layer, to thus form a precursor part having an imparted or enhanced performance characteristic. A pyrolysis subsystem may be used for pyrolyzing the precursor part to create the Stage 1 CC part.

公开(公告)号：US12053957B2

公开(公告)日：2024-08-06

申请号：US16958558

申请日：2018-12-21

申请人： SAFRAN CERAMICS

发明人： Eric Philippe ,  Medhy Damien Bounia ,  Aurélia Clerambourg ,  Paul Carminati

IPC分类号： B32B18/00 ,  B28B1/00 ,  B28B1/24 ,  B28B1/26 ,  B28B23/00 ,  C04B35/117 ,  C04B35/14 ,  C04B35/18 ,  C04B35/185 ,  C04B35/447 ,  C04B35/488 ,  C04B35/56 ,  C04B35/565 ,  C04B35/58 ,  C04B35/584 ,  C04B35/628 ,  C04B35/64 ,  C04B35/80 ,  C04B41/45 ,  G10K11/168 ,  B28B7/00

CPC分类号： B32B18/00 ,  B28B1/002 ,  B28B1/24 ,  B28B1/265 ,  B28B23/0006 ,  C04B35/117 ,  C04B35/14 ,  C04B35/18 ,  C04B35/185 ,  C04B35/447 ,  C04B35/488 ,  C04B35/56 ,  C04B35/565 ,  C04B35/5805 ,  C04B35/58071 ,  C04B35/58092 ,  C04B35/584 ,  C04B35/62886 ,  C04B35/64 ,  C04B35/80 ,  C04B41/4584 ,  B28B7/0058 ,  C04B2235/3217 ,  C04B2235/3244 ,  C04B2235/3418 ,  C04B2235/3463 ,  C04B2235/3804 ,  C04B2235/3817 ,  C04B2235/3852 ,  C04B2235/3891 ,  C04B2235/447 ,  C04B2235/5224 ,  C04B2235/5228 ,  C04B2235/5232 ,  C04B2235/5244 ,  C04B2235/5248 ,  C04B2235/616 ,  G10K11/168 ,  C04B38/0074 ,  C04B35/80 ,  C04B38/0054

摘要： A process for manufacturing a composite material part includes formation of a fibrous texture from refractory ceramic fibres, placement of the fibrous texture in a mould with interposition of a filtration layer between the fibrous texture and a discharge port, the filtration layer including a partially densified fibrous structure, pressure injection of a slurry containing a powder of refractory ceramic particles into the fibrous texture, drainage by the filtration layer of the slurry solvent having passed through the fibrous texture and retention of the powder of refractory ceramic particles within the texture by the filtration layer to obtain a fibrous preform including the fibrous texture filled with refractory ceramic particles and the filtration layer, heat treatment of the refractory ceramic particles present in the fibrous texture of the preform to form a composite material part including the fibrous texture densified by a refractory ceramic matrix and the filtration layer.

公开(公告)号：US20240239713A1

公开(公告)日：2024-07-18

申请号：US18153871

申请日：2023-01-12

申请人： Honeywell International Inc.

发明人： Mehrad Mehr ,  Bahram Jadidian

IPC分类号： C04B35/628 ,  C04B35/565 ,  C04B41/45

CPC分类号： C04B35/62844 ,  C04B35/565 ,  C04B41/4515 ,  C04B2235/5244 ,  C04B2235/5248 ,  C04B2235/5264

摘要： The disclosure describes vacuum processing of a fiber tow. In some examples, the disclosure describes generating a metal carbide fiber tow by applying metal to a carbon fiber tow and vacuum processing the carbon fiber tow to convert at least a portion of the carbon fiber tow to a metal carbide fiber tow.

公开(公告)号：US12017961B2

公开(公告)日：2024-06-25

申请号：US16614263

申请日：2018-05-16

申请人： Cornell University

发明人： Yong Lak Joo ,  Ling Fei ,  Seung Wan Kim

IPC分类号： C04B35/622 ,  C01B32/16 ,  C04B35/83 ,  D01D5/00

CPC分类号： C04B35/62277 ,  C01B32/16 ,  C04B35/83 ,  D01D5/0046 ,  C04B2235/5248 ,  C04B2235/526 ,  C04B2235/5264 ,  C04B2235/96

摘要： Provided in certain embodiments are high performance graphene fibers and yarns, including components and precursors thereof, and composites comprising the same. Also provided herein are methods of manufacturing such fibers, yarns, composites, and components/precursors thereof.

公开(公告)号：US20240140879A1

公开(公告)日：2024-05-02

申请号：US17977781

申请日：2022-10-31

申请人： Rohr, Inc.

发明人： Katherine E. Waugh ,  Christopher C. Koroly ,  Vijay V. Pujar ,  John S. Linck ,  Kyle Rosenbrock

IPC分类号： C04B35/83

CPC分类号： C04B35/83 ,  C04B2235/5248 ,  C04B2235/5256 ,  C04B2235/604

摘要： A shape forming tool for pre-carbonization compression of a fibrous preform includes a female forming tool comprising a die recess, a support structure moveable with respect to the female forming tool, and at least one bladder coupled to the support structure and configured to be received into the die recess. The support structure is configured to move the bladder(s) with respect to the female forming tool. The bladder(s) is/are configured to be inflated to apply a compressive force to compress and form a fibrous preform between the bladder(s) and the female forming tool.

公开(公告)号：US20230242454A1

公开(公告)日：2023-08-03

申请号：US17591013

申请日：2022-02-02

申请人： GOODRICH CORPORATION

发明人： Jean-Francois LeCOSTAOUEC

IPC分类号： C04B35/83 ,  C04B35/628 ,  C04B35/64

CPC分类号： C04B35/83 ,  C04B35/62873 ,  C04B35/62849 ,  C04B35/62886 ,  C04B35/64 ,  C04B2235/5248 ,  C04B2235/3869 ,  C04B2235/424 ,  C04B2235/483

摘要： A method of making a carbon-carbon composite may comprise forming a Silicon-Aluminum-Oxygen-Nitrogen (SiAlON) precursor suspension and infiltrating a fibrous preform with the SiAlON precursor suspension. A SiAlON forming heating treatment may be performed on the fibrous preform to form SiAlON particles. The fibrous preform may be densified using chemical vapor infiltration to form a densified fibrous preform.

公开(公告)号：US11713281B2

公开(公告)日：2023-08-01

申请号：US17557902

申请日：2021-12-21

申请人： GOODRICH CORPORATION

发明人： Ying She ,  Naveen Menon ,  Gavin Charles Richards ,  Zissis A. Dardas ,  Thomas P. Filburn

IPC分类号： C04B35/80 ,  C23C16/455 ,  C23C16/44 ,  C04B35/565 ,  C23C16/32 ,  C23C16/04

CPC分类号： C04B35/80 ,  C04B35/565 ,  C23C16/045 ,  C23C16/325 ,  C23C16/4412 ,  C23C16/45517 ,  C04B2235/46 ,  C04B2235/5244 ,  C04B2235/5248 ,  C04B2235/614

摘要： Systems for and methods of manufacturing a ceramic matrix composite include introducing a gaseous precursor into an inlet portion of a reaction furnace having a chamber comprising the inlet portion and an outlet portion that is downstream of the inlet portion, and delivering a mitigation agent, such as water vapor or ammonia, into an exhaust conduit in fluid communication with and downstream of the outlet portion of the reaction chamber so as to control chemical reactions occurring with the exhaust chamber. Introducing the gaseous precursor densifies a porous preform, and introducing the mitigation agent shifts the reaction equilibrium to disfavor the formation of harmful and/or pyrophoric byproduct deposits within the exhaust conduit.

公开(公告)号：US20230227369A1

公开(公告)日：2023-07-20

申请号：US18176639

申请日：2023-03-01

申请人： Arkema France

发明人： Robert BARSOTTI ,  Krysten MINNICI ,  Stephen G DIPIETRO ,  Mary CALVIN ,  Roderick REBER

IPC分类号： C04B35/83 ,  C04B35/64 ,  C04B35/628

CPC分类号： C04B35/83 ,  C04B35/64 ,  C04B35/62886 ,  C04B35/62873 ,  C04B2235/48 ,  C04B2235/422 ,  C04B2235/5248 ,  C04B2235/5252 ,  C04B2235/6562 ,  C04B2235/616

摘要： A method for making a high temperature composite, which is a carbon carbon composite, carbon fiber reinforced ceramic matrix composite, ceramic fiber reinforced ceramic matrix composite, or a carbon silica composite, including: a) providing a precursor part including a resin comprising a poly(aryl ether ketone) (PAEK) and at least one reinforcing material, wherein the resin has a degree of crystallinity of 10% or more; b) pyrolyzing the precursor part to a pyrolyzed part; c) infusing a liquid second resin into the pyrolyzed part to make an infused part; and d) pyrolyzing the infused part to make the carbon carbon composite carbon fiber reinforced ceramic matrix composite, ceramic fiber reinforced ceramic matrix composite, or the carbon silica composite, optionally repeating steps c. through d. Also, a carbon carbon composite, carbon fiber reinforced ceramic matrix composite, ceramic fiber reinforced ceramic matrix composite, or carbon silica composite made by the method.

公开(公告)号：US20230183141A1

公开(公告)日：2023-06-15

申请号：US18107189

申请日：2023-02-08

申请人： United States of America as Represented by the Secretary of Agriculture

发明人： Zhiyong Cai ,  Qiangu Yan

IPC分类号： C04B35/83 ,  C04B38/00

CPC分类号： C04B35/83 ,  C04B38/0022 ,  C04B2235/614 ,  C04B2235/5248

摘要： Methods of forming a carbon fiber reinforced carbon foam are provided. Such a method may comprise heating a porous body composed of a solid material comprising covalently bound carbon atoms and heteroatoms and having a surface defining pores distributed throughout the solid material, in the presence of an added source of gaseous hydrocarbons. The heating generates free radicals in the porous body from the heteroatoms and induces reactions between the free radicals and the gaseous hydrocarbons to form covalently bound carbon nanofibers extending from the surface of the solid material and a network of entangled carbon microfibers within the pores the porous body, thereby forming a carbon fiber reinforced carbon foam. Carbon fiber reinforced carbon foams and ballistic barriers incorporating the foams are also provided.