⚠ Novel chemotype — no close known analogue (best Tanimoto < 0.3). Unexplored chemical space relative to ChEMBL.
Similar compounds — the chemically nearest patent molecules
Nearest neighbours by Morgan-fingerprint cosine across the patent-compound collection, with each neighbour's top predicted target and the predicted targets it shares with this molecule.
| Compound | similarity | top predicted | shared targets | |
|---|---|---|---|---|
| Charcoal, Activated SCHEMBL31633424 | 0.87 | — | — | |
| Charcoal, Activated SCHEMBL30831366 | 0.87 | — | — | |
| Charcoal, Activated SCHEMBL31083577 | 0.87 | — | — | |
| Charcoal, Activated SCHEMBL9466404 | 0.87 | — | — | |
| Charcoal, Activated SCHEMBL498646 | 0.87 | — | — | |
| Charcoal, Activated SCHEMBL1478931 | 0.87 | — | — | |
| Charcoal, Activated SCHEMBL1049306 | 0.82 | — | — | |
| Charcoal, Activated SCHEMBL60093 | 0.82 | — | — | |
| SCHEMBL168044 | 0.82 | — | — | |
| Charcoal, Activated SCHEMBL49255 | 0.82 | — | — |
Similarity is cosine over the 2,048-bit Morgan fingerprint (≈ Tanimoto). Identical fingerprints score 1.00.
Patent provenance — the patents this molecule appears in, and who filed them
Claimed or disclosed in 448 patents — showing the first 20. claimed = in the patent's claims; disclosed = body only.
| Patent | Title | Assignee | Published | Priority | Filing | Country | Status |
|---|---|---|---|---|---|---|---|
| CN-117567158-A | High-entropy ceramic matrix composite material and preparation method thereof | 西北工业大学 | 2024-02-20 | — | — | CN | claimed |
| CN-115515914-B | Method for manufacturing ceramic matrix composite material containing specific interface phase | 冯倩 | 2024-02-09 | — | — | CN | claimed |
| CN-115515914-A | Method for manufacturing ceramic matrix composite material containing specific interface phase | 莱昂内尔·范登布尔克 | 2022-12-23 | — | — | CN | claimed |
| CN-113502456-A | Preparation process of silicon-boron-carbon sputtering target material | 法柯特科技（江苏）有限公司 | 2021-10-15 | — | — | CN | claimed |
| CN-113149680-A | Carbon fiber reinforced silicon-boron-carbon-nitrogen-based ceramic composite material and preparation method thereof | 尚辰(浙江绍兴)复合材料科技有限公司 | 2021-07-23 | — | — | CN | claimed |
| CN-106033757-B | High mobility device with anti-punch through layer and method of forming the same | 台湾积体电路制造股份有限公司 | 2020-03-20 | — | — | CN | claimed |
| CN-109485421-A | Structural ceramics and preparation method thereof based on carbonitride nanometer two-dimensional material toughening | 清华大学深圳研究生院 | 2019-03-19 | — | — | CN | claimed |
| CN-105948748-B | A kind of Si-B-C-N zircon ceramic composite material and preparation method | 哈尔滨工业大学 | 2019-01-29 | — | — | CN | claimed |
| CN-108706978-A | The method that mist projection granulating combination 3DP and CVI prepare carbon/silicon carbide ceramic matrix composite | 西北工业大学 | 2018-10-26 | — | — | CN | claimed |
| CN-105481451-B | Close the preparation method of fat dispersion hafnium boride boron carbide-carbon fiber friction material | 山东理工大学 | 2018-06-26 | — | — | CN | claimed |
| EP-0791028-A4 | HIGH TEMPERATURE THERMOSETS AND CERAMICS DERIVED FROM LINEAR CARBORANE-(SILOXANE OR SILANE)-ACETYLENE COPOLYMERS | US HEALTH (US) | 1998-01-07 | — | — | EP | claimed |
| US-5681870-A | PYROLYSIS OF COPOLYMER | THE UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE NAVY (US) | 1997-10-28 | — | — | US | claimed |
| EP-0791028-A1 | HIGH TEMPERATURE THERMOSETS AND CERAMICS DERIVED FROM LINEAR CARBORANE-(SILOXANE OR SILANE)-ACETYLENE COPOLYMERS | THE GOVERNMENT OF THE UNITED STATES OF AMERICA, as represented by THE SECRETARY OF THE NAVY (US) | 1997-08-27 | — | — | EP | claimed |
| WO-1996014351-A1 | HIGH TEMPERATURE THERMOSETS AND CERAMICS DERIVED FROM LINEAR CARBORANE-(SILOXANE OR SILANE)-ACETYLENE COPOLYMERS | THE GOVERNMENT OF THE UNITED STATES OF AMERICA, REPRESENTED BY THE SECRETARY OF THE NAVY (US) | 1996-05-17 | — | — | WO | claimed |
| US-5483017-A | High temperature thermosets and ceramics derived from linear carborane-(siloxane or silane)-acetylene copolymers | THE UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE NAVY (US) | 1996-01-09 | — | — | US | claimed |
| EP-0483009-B1 | Process for the preparation of a composite refractory material protected against corrosion | EUROP PROPULSION (FR) | 1995-01-18 | — | — | EP | claimed |
| US-5348917-A | Ceramics formed by pyrolysis of either linear or thermosetting carborane (siloxane or silane) acetylene based precursor polymers | THE UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE NAVY (US) | 1994-09-20 | — | — | US | claimed |
| US-5246736-A | Vapor deposition or infiltration to form silicon-boron-carbon system; carbiding, boriding | SOCIETE EUROPEENNE DE PROPULSION (FR) | 1993-09-21 | — | — | US | claimed |
| US-5223461-A | Crosslinking the surface of the green fiber using air oxidation, UV radiation or hydrazine; pyrolyzing in an inert gas; dimensional stability; high tensile strength; aerospace | THE UNITED STATES OF AMERICA AS REPRESENTED BY THE ADMINISTRATOR OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION (US) | 1993-06-29 | — | — | US | claimed |
| US-5130278-A | Preceramic polymers which pyrolyze to form ceramics | THE UNITED STATES OF AMERICA AS REPRESENTED BY THE ADMINISTRATOR OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION (US) | 1992-07-14 | — | — | US | claimed |