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公开(公告)号:US20240140875A1
公开(公告)日:2024-05-02
申请号:US18468903
申请日:2023-09-18
Applicant: SK enpulse Co., Ltd.
Inventor: Kyung yeol MIN , Yongsoo CHOI , SungSic HWANG , Kyung In KIM , Jung Kun KANG , Su Man CHAE
IPC: C04B35/563 , C04B35/626 , C04B35/634 , C04B35/64 , H01J37/32
CPC classification number: C04B35/563 , C04B35/6261 , C04B35/6264 , C04B35/62655 , C04B35/62695 , C04B35/63424 , C04B35/63476 , C04B35/64 , H01J37/32642 , C04B2235/3821 , C04B2235/422 , C04B2235/606 , C04B2235/6562 , C04B2235/6565 , C04B2235/6567 , C04B2235/661 , C04B2235/723 , C04B2235/728 , C04B2235/782 , C04B2235/786 , C04B2235/9607 , C04B2235/9669 , H01J2237/334
Abstract: The sintered body including boron carbide, wherein the sintered body includes a zone, in which a volume ratio of grains having a grain size of greater than 30 μm and 60 μm or less is in a range of 50% to 70% based on a total volume of grains, as observed on a surface of the sintered body, is disclosed.
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公开(公告)号:US20240051878A1
公开(公告)日:2024-02-15
申请号:US17887228
申请日:2022-08-12
Applicant: Goodrich Corporation
Inventor: CHRISTOPHER T. KIRKPATRICK
IPC: C04B35/622 , C04B35/563 , C04B41/45 , C04B41/50 , C04B35/83 , C04B41/91
CPC classification number: C04B35/62222 , C04B35/563 , C04B41/457 , C04B41/5096 , C04B35/83 , C04B41/91 , C04B2235/616 , C04B2235/3821 , C04B2235/5248 , C04B2235/428 , C04B2235/422
Abstract: A method of fabricating a composite component, includes forming a fibrous preform by forming a first ceramic particle layer over a first textile layer, the first ceramic particle layer having a first group of ceramic particles, disposing a second textile layer over the first ceramic particle layer, forming a second ceramic particle layer over the second textile layer, the second ceramic particle layer having a second group of ceramic particles, and disposing a third textile layer over the second ceramic particle layer. The method further includes densifying the fibrous preform.
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公开(公告)号:US11885182B2
公开(公告)日:2024-01-30
申请号:US17662871
申请日:2022-05-11
Applicant: Baker Hughes Holdings LLC
Inventor: Wanjun Cao , Marc W. Bird
IPC: E21B10/573 , C04B35/528 , C04B35/56 , C04B35/565 , C04B35/563 , B24D18/00 , E21B10/567 , C22C26/00 , E21B10/54
CPC classification number: E21B10/5735 , B24D18/0009 , C04B35/528 , C04B35/56 , C04B35/563 , C04B35/565 , C04B35/5607 , C04B35/5611 , C04B35/5615 , C04B35/5618 , C04B35/5622 , C22C26/00 , E21B10/5673 , C22C2026/006 , E21B10/54
Abstract: A cutting element comprises a supporting substrate, and a cutting table attached to an end of the supporting substrate. The cutting table comprises inter-bonded diamond particles, and a thermally stable material within interstitial spaces between the inter-bonded diamond particles. The thermally stable material comprises a carbide precipitate having the general chemical formula, A3XZn-1, where A comprises one or more of Sc, Ti, V, Cr, Mn, Fe, Co, Ni, Cu, Zn, Y, Zr, Nb, Mo, Tc, Ru, Rh, Pd, Ag, Cd, Hf, Ta, W, Re, Os, Ir, Pt, Au, Hg, La, Ce, Pr, Nd, Pm, Sm, Eu, Gd, Tb, Dy, Ho, Er, Tm, Yb, Lu, Ac, Th, Pa, and U; X comprises one or more of Al, Ga, Sn, Be, Bi, Te, Sb, Se, As, Ge, Si, B, and P; Z comprises C; and n is greater than or equal to 0 and less than or equal to 0.75. A method of forming a cutting element, an earth-boring tool, a supporting substrate, and a method of forming a supporting substrate are also described.
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公开(公告)号:US20230373868A1
公开(公告)日:2023-11-23
申请号:US17747816
申请日:2022-05-18
Applicant: GOODRICH CORPORATION
Inventor: Steven Poteet
IPC: C04B35/5831 , C04B35/563 , C04B35/565 , C04B35/58 , C04B35/14
CPC classification number: C04B35/5831 , C04B35/563 , C04B35/565 , C04B35/58085 , C04B35/14
Abstract: Systems and methods for forming an oxidation protection system on a composite structure are provided. In various embodiments, the oxidation protection system comprises a boron-glass layer formed on the composite substrate and a silicon-glass layer formed over the boron-glass layer. Each of the boron-glass layer and the silicon-glass layer include a glass former and a glass modifier. The boron-glass layer includes a boron compound comprising a mixture of boron carbide (B4C) powder and cubic boron nitride (BN) powder.
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公开(公告)号:US20230257308A1
公开(公告)日:2023-08-17
申请号:US18107224
申请日:2023-02-08
Applicant: The Government of the United States of America, as represented by the Secretary of the Navy
Inventor: Ramasis Goswami , Syed B. Qadri
IPC: C04B35/563 , C04B35/626 , C04B41/00
CPC classification number: C04B35/563 , C04B35/62615 , C04B35/62695 , C04B41/0081 , C04B2235/401 , C04B2235/402 , C04B2235/61 , C04B2235/5445 , C04B2235/3821
Abstract: A method of making an Al—B4C composite with Mg addition comprising providing a first mixture of B4C, Al and Mg powder, producing a powder mixture, adding Mg to the powder mixture, forming pellets, creating a composite, annealing the composite, and forming an Al—Mg—B4C composite. An Al—B4C composite with Mg addition comprising Al, Mg comprising 4 wt. %, and B4C comprising 8 wt. %. An Al—B4C composite with Mg addition made from the steps comprising providing a first mixture of B4C, Al and Mg powder, producing a powder mixture, adding Mg to the powder mixture, forming pellets, creating a composite, annealing the composite, and forming an Al—Mg—B4C composite.
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公开(公告)号:US20230117106A1
公开(公告)日:2023-04-20
申请号:US18082053
申请日:2022-12-15
Applicant: Ossiform ApS
Inventor: Morten Østergaard Andersen , Martin Bonde Jensen , Casper Slots
IPC: A61C13/00 , C04B35/563 , C04B28/00 , C04B35/468 , C04B35/583 , C04B35/01 , C04B28/04 , C04B35/505 , C04B35/632 , C04B35/495 , C04B35/16 , C04B35/58 , C04B35/50 , C04B35/457 , C04B28/34 , C04B35/56 , C04B35/111 , C04B35/515 , C04B35/486 , C04B35/636 , C04B33/04 , C04B35/447 , C04B35/565 , C04B35/453 , C04B35/46 , C04B35/49 , C04B35/634 , C04B35/08 , C04B35/14 , C04B35/553 , B29C64/165 , B29C64/188 , B29C64/112 , B29C64/124 , B29C64/118 , B22F1/107 , B33Y70/10 , B33Y40/20 , B28B1/00 , C09D11/033 , C09D11/037 , C09D11/32 , C09D11/36 , C09D11/38 , C09D11/52
Abstract: The present invention relates to a suspension comprising 50-95% by weight of the total suspension (w/w) of at least one metallic material and/or ceramic material and/or polymeric material and/or solid carbon containing material; and at least 5% by weight of the total suspension of one or more fatty acids or derivatives thereof. In addition, the invention relates to uses of such suspension in 3D printing processes.
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公开(公告)号:US11584694B2
公开(公告)日:2023-02-21
申请号:US17248309
申请日:2021-01-19
Applicant: II-VI Delaware, Inc
Inventor: Jon Coppola , Nicholas Coombs , Jiwen Wang , Michael K. Aghajanian
IPC: C04B35/565 , C04B41/45 , C04B35/563 , C04B41/50 , H01L21/687
Abstract: A reaction-bonded silicon carbide (SiC) body is produced by: providing a preform including ceramic elements and carbon, and one or more surface features; providing a powder which includes diamond particles and carbon; locating the powder in the surface feature(s); and infiltrating the preform and the powder with molten silicon (Si) to form reaction-bonded SiC in the preform, and to form reaction-bonded SiC coatings on the diamond particles. The present disclosure also relates to a device/component which includes: a main body portion and discrete elements located at least partially within the main body portion. The main body portion may include reaction-bonded SiC and Si, but not diamond, while the discrete elements include diamond particles, reaction-bonded SiC coatings surrounding the diamond particles, and Si. According to the present disclosure, diamond may be advantageously located only where it is needed.
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公开(公告)号:US11364654B2
公开(公告)日:2022-06-21
申请号:US16717356
申请日:2019-12-17
Applicant: UT-Battelle, LLC
Inventor: Corson L. Cramer , Richard A. Lowden , Kinga A. Unocic , Jacob W. McMurray , Amelia M. Elliott
IPC: B28B1/00 , B28B17/00 , C04B35/563 , C04B38/00 , C04B35/565 , C04B35/632 , C04B38/06 , B33Y10/00 , B33Y30/00 , B33Y70/00 , B33Y80/00
Abstract: A method for indirect additive manufacturing of an object constructed of boron carbide, silicon carbide, and free silicon, comprising: (i) producing a porous preform constructed of boron carbide and silicon carbide by an indirect ceramic additive manufacturing (ICAM) process in which particles of a powder mixture become bonded together with an organic binder, wherein the powder mixture comprises: a) boron carbide particles, and b) silicon carbide particles, wherein at least 80 vol % of the silicon carbide particles are larger than the boron carbide particles; and wherein the boron carbide and silicon carbide particles are each included in an amount of 40-60 wt. % of the powder mixture, provided that the foregoing amounts sum to at least 95 wt. %; (ii) subjecting the porous preform to a temperature of 500-900° C. to volatilize the organic binder; and (iii) infiltrating molten silicon into pores of the porous preform to produce the object.
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公开(公告)号:US11299430B2
公开(公告)日:2022-04-12
申请号:US15822203
申请日:2017-11-26
Applicant: HRL Laboratories, LLC
Inventor: Zak C. Eckel , Tobias A. Schaedler , John H. Martin , Kenneth Cante
IPC: C04B35/56 , C09D11/037 , B29C64/379 , B33Y40/00 , C04B35/58 , C04B35/589 , C08L83/08 , C04B35/571 , C04B35/597 , C04B35/515 , C04B35/117 , C04B35/14 , C04B35/44 , C04B35/46 , C04B35/488 , C04B35/532 , C04B35/563 , C04B35/565 , C04B35/581 , C04B35/80 , B33Y70/00 , C04B35/622 , C04B35/628 , C04B35/634 , C04B35/64 , B29C64/10 , C09D7/61 , B28B1/00 , C09D11/03 , C09D11/101 , C09D11/102 , B33Y80/00 , C09D7/40 , C09D7/62 , C09D5/33 , B29C35/08 , B29C64/129 , B29C71/02 , C08G77/18 , C08G77/20 , C08G77/28 , B29K105/00 , C08K3/34 , B33Y10/00 , B29K83/00 , B29K509/04 , C08K7/00 , C08K7/10 , C08K9/04
Abstract: This invention provides resin formulations which may be used for 3D printing and pyrolyzing to produce a ceramic matrix composite. The resin formulations contain a solid-phase filler, to provide high thermal stability and mechanical strength (e.g., fracture toughness) in the final ceramic material. The invention provides direct, free-form 3D printing of a preceramic polymer loaded with a solid-phase filler, followed by converting the preceramic polymer to a 3D-printed ceramic matrix composite with potentially complex 3D shapes or in the form of large parts. Other variations provide active solid-phase functional additives as solid-phase fillers, to perform or enhance at least one chemical, physical, mechanical, or electrical function within the ceramic structure as it is being formed as well as in the final structure. Solid-phase functional additives actively improve the final ceramic structure through one or more changes actively induced by the additives during pyrolysis or other thermal treatment.
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公开(公告)号:US20210269364A1
公开(公告)日:2021-09-02
申请号:US17184081
申请日:2021-02-24
Applicant: KOREA INSTITUTE OF SCIENCE AND TECHNOLOGY
Inventor: Sang Whan PARK , Mi Rae YOUM , SUNG IL YUN , Jun Hyung PARK
IPC: C04B35/563 , C04B35/645
Abstract: The present disclosure provides a boron carbide composite material having a novel composition with excellent mechanical properties, and a production method therefor. The boron carbide composite material has high fracture toughness and may be applied as a lightweight bulletproof ceramic material. The boron carbide composite material is a boron carbide/silicon carbide/titanium boride/graphite (B4C—SiC—TiB2—C) composite material. The composite material may overcome a technical limitation on increasing the fracture toughness of the boron carbide composite material, and may be produced as a high-density boron carbide composite material using a reactive hot-pressing sintering process at a relatively low temperature. The boron carbide composite material having excellent mechanical properties may be applied to general industrial wear-resistant parts and nuclear-power-related industrial parts, and particularly, may be actively used as a lightweight bulletproof material for personal use and for military aircraft including helicopters.
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