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1.
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COMPUTER SYSTEMS FOR AND METHODS OF IDENTIFYING NON-ELEMENTAL MATERIALS BASED ON ATOMISTIC PROPERTIES
Application Number |
CA2017051449 |
Publication Number |
2018/098588 |
Status |
In Force |
Filing Date |
2017-12-01 |
Publication Date |
2018-06-07 |
Owner |
LUMIANT CORPORATION (Canada)
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Inventor |
- Pisarski, Pawel Michal
- Holloway, Scott Richard
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Abstract
Disclosed are computer systems for and methods of identifying non-elemental materials based on atomistic properties. The computer systems and methods may permit the identification of non-elemental materials having one or more desired material properties which may be specified in the form of user input. The materials identified may be known or predicted by the computer systems and the methods to exhibit the desired material properties.
IPC Classes ?
- G09F 19/00 - Advertising or display means not otherwise provided for
- G01N 37/00 - Details not covered by any other group of this subclass
- G06F 15/18 - in which a program is changed according to experience gained by the computer itself during a complete run; Learning machines (adaptive control systems G05B 13/00;artificial intelligence G06N)
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2.
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METALLIC MATRIX COMPOSITE WITH HIGH STRENGTH TITANIUM ALUMINIDE ALLOY MATRIX AND IN SITU FORMED ALUMINUM OXIDE REINFORCEMENT
Application Number |
CA2017050542 |
Publication Number |
2017/190245 |
Status |
In Force |
Filing Date |
2017-05-04 |
Publication Date |
2017-11-09 |
Owner |
LUMIANT CORPORATION (Canada)
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Inventor |
Holloway, Scott Richard
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Abstract
Metallic matrix composites include a high strength titanium aluminide alloy matrix and an in situ formed aluminum oxide reinforcement. The atomic percentage of aluminum in the titanium aluminide alloy matrix can vary from 40% to 48%. Included are methods of making the metallic matrix composites, in particular, through the performance of an exothermic chemical reaction. The metallic matrix composites can exhibit low porosity.
IPC Classes ?
- C04B 35/515 - Shaped ceramic products characterised by their compositionCeramic compositionsProcessing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxides
- C04B 35/65 - Reaction sintering of free metal- or free silicon-containing compositions
- C04B 35/78 - Ceramic products containing macroscopic reinforcing agents containing non-metallic materials
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3.
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TITANIUM SILICIDE MATRIX COMPOSITE WITH IN SITU FORMED TITANIUM CARBIDE REINFORCEMENT
Application Number |
CA2017050543 |
Publication Number |
2017/190246 |
Status |
In Force |
Filing Date |
2017-05-04 |
Publication Date |
2017-11-09 |
Owner |
LUMIANT CORPORATION (Canada)
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Inventor |
Holloway, Scott Richard
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Abstract
Metallic matrix composites include a titanium silicide matrix and an in situ formed titanium carbide reinforcement. The atomic percentage of silicon in the titanium silicide matrix can vary from 20.0% to 70.0%. Included are methods of making the metallic matrix composites, in particular, through the performance of an exothermic chemical reaction. The metallic matrix composites can exhibit low porosity.
IPC Classes ?
- C04B 35/58 - Shaped ceramic products characterised by their compositionCeramic compositionsProcessing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxides based on borides, nitrides or silicides
- C04B 35/65 - Reaction sintering of free metal- or free silicon-containing compositions
- C04B 35/78 - Ceramic products containing macroscopic reinforcing agents containing non-metallic materials
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4.
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METALLIC COMPOUNDS AND METALLIC MATRIX COMPOSITES MADE USING COMPRESSION ACTIVATED SYNTHESIS
Application Number |
CA2017050540 |
Publication Number |
2017/190243 |
Status |
In Force |
Filing Date |
2017-05-04 |
Publication Date |
2017-11-09 |
Owner |
LUMIANT CORPORATION (Canada)
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Inventor |
- Holloway, Scott Richard
- Manley, Richard
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Abstract
Articles are manufactured using self-propagating high-temperature synthesis (SHS) reactions. Particulates including reactants can be blended to form a particulate blend. The particulate blend can be preformed. The preform article can be heated to a pre-heat temperature being below an auto-activation temperature and above a minimum compression activated synthesis temperature. Compressive stress can be exerted on the preform article at the pre-heat temperature to initiate the SHS reaction between the reactants and thereby form a product metallic compound. At approximately peak temperature, a flow stress of the product metallic compound can be exceeded to substantially reduce porosity and thereby form a shaped substantially dense article.
IPC Classes ?
- C04B 35/65 - Reaction sintering of free metal- or free silicon-containing compositions
- B22F 3/23 - Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sinteringApparatus specially adapted therefor involving a self-propagating high-temperature synthesis or reaction sintering step
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5.
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METALLIC MATRIX COMPOSITES SYNTHESIZED WITH UNIFORM IN SITU FORMED REINFORCEMENT
Application Number |
CA2017050544 |
Publication Number |
2017/190247 |
Status |
In Force |
Filing Date |
2017-05-04 |
Publication Date |
2017-11-09 |
Owner |
LUMIANT CORPORATION (Canada)
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Inventor |
Holloway, Scott Richard
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Abstract
Metallic matrix composites are synthesized by mixing a first reactant, a second reactant and a nucleator compound to obtain a reaction mixture, and heating the reaction mixture to an auto-activation temperature to initiate a self- propagating high-temperature synthesis reaction between the first and second reactants. The metallic matrix composite can include a metallic matrix and an in situ formed reinforcement. The reinforcement can be formed of discrete particles substantially uniformly dispersed within the metallic matrix. Each of the particles can have a reinforcement constituent disposed about a core formed of the nucleator compound.
IPC Classes ?
- C04B 35/65 - Reaction sintering of free metal- or free silicon-containing compositions
- B22F 3/23 - Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sinteringApparatus specially adapted therefor involving a self-propagating high-temperature synthesis or reaction sintering step
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6.
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LUMIANT CORPORATION
Application Number |
159667700 |
Status |
Registered |
Filing Date |
2012-10-02 |
Registration Date |
2014-12-04 |
Owner |
LUMIANT CORPORATION (Canada)
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NICE Classes ? |
- 40 - Treatment of materials; recycling, air and water treatment,
- 42 - Scientific, technological and industrial services, research and design
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Goods & Services
(1) Design and manufacture of inorganic composite materials to the order and specification of others for use in manufacturing goods comprising composite materials, namely metal composite materials and ceramic composite materials.
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