Casting core
US-2026001121-A1 · Jan 1, 2026 · US
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Saboundji Amar patents
Saboundji Amar is listed as an inventor on 35 patents in our database. Major assignees and classification codes are summarized below.
| Metric | Value |
|---|---|
| Inventor | Saboundji Amar |
| Total patents | 35 |
| First publication | May 23, 2019 |
| Latest publication | Jan 1, 2026 |
Notable patents
Publications ranked by popularity score, then publication date.
Protection against oxidation or corrosion of a hollow part made of a superalloy
US-12454891-B2 · Oct 28, 2025 · US
Sublayer for a nickel-based superalloy for enhancing the lifetime of the parts and implementation method thereof
US-12203153-B2 · Jan 21, 2025 · US
Aircraft part made of superalloy comprising rhenium and/or ruthenium and associated manufacturing method
US-12110581-B2 · Oct 8, 2024 · US
Method for producing a metal bladed element for a turbomachine of an aircraft
US-12084779-B2 · Sep 10, 2024 · US
Method for coating a refractory alloy part, and the part thus coated
US-2024246140-A1 · Jul 25, 2024 · US
Method for protection against corrosion
US-12006577-B2 · Jun 11, 2024 · US
Aircraft part made of superalloy comprising rhenium and/or ruthenium and associated manufacturing method
US-2024093343-A1 · Mar 21, 2024 · US
Turbine part made of superalloy comprising rhenium and/or ruthenium and associated manufacturing method
US-11873736-B2 · Jan 16, 2024 · US
Sublayer for a nickel-based superalloy for enhancing the lifetime of the parts and implementation method thereof
US-2023340645-A1 · Oct 26, 2023 · US
Recent patents
Latest publications not already listed above.
Protection against oxidation or corrosion of a hollow part made of a superalloy
US-2023304409-A1 · Sep 28, 2023 · US
Ceramic coating for foundry core
US-11752541-B2 · Sep 12, 2023 · US
Coating for refractory alloy part
US-11542586-B2 · Jan 3, 2023 · US
Superalloy aircraft part comprising a cooling channel
US-2022356555-A1 · Nov 10, 2022 · US
Method for the protection of a hafnium-free, nickel-based monocrystalline superalloy part against corrosion and oxidation
US-11473185-B2 · Oct 18, 2022 · US
Component protected by an environmental barrier
US-11465943-B2 · Oct 11, 2022 · US
Method for protection against corrosion
US-2022251713-A1 · Aug 11, 2022 · US
Part made of silicon-based ceramic or cmc and method for producing such a part
US-2022204415-A1 · Jun 30, 2022 · US
Turbine component made from superalloy and associated manufacturing method
US-11306599-B2 · Apr 19, 2022 · US
Turbine component made from superalloy comprising rhenium and associated manufacturing process
US-11293290-B2 · Apr 5, 2022 · US
Turbine part made of superalloy comprising rhenium and/or ruthenium and associated manufacturing method
US-2022065111-A1 · Mar 3, 2022 · US
Turbine part made of superalloy comprising rhenium and/or ruthenium and associated manufacturing method
US-11248476-B2 · Feb 15, 2022 · US
Ceramic coating for foundry core
US-2021299743-A1 · Sep 30, 2021 · US
Coating for refractory alloy part
US-2021292882-A1 · Sep 23, 2021 · US
Process for manufacturing a part made of nickle-based superalloy containing hafnium
US-11078567-B2 · Aug 3, 2021 · US
Turbine component made from superalloy comprising rhenium and associated manufacturing process
US-2021199016-A1 · Jul 1, 2021 · US
Method for producing a metal bladed element for a turbomachine of an aircraft
US-2021156034-A1 · May 27, 2021 · US
Part comprising a nickel-based monocrystalline superalloy substrate and method for manufacturing same
US-10982333-B2 · Apr 20, 2021 · US
Turbine component made from superalloy and associated manufacturing method
US-2021062660-A1 · Mar 4, 2021 · US
Component protected by an environmental barrier
US-2020331817-A1 · Oct 22, 2020 · US
Major assignees
Companies most often associated with this inventor's publications.
| Assignee | Patents |
|---|---|
| Safran | 35 |
| Commissariat Energie Atomique | 5 |
| Safran Aircraft Engines | 2 |
Top CPC classifications
Most common classification codes across this inventor's patents.
| CPC | Patents |
|---|---|
| F01D5/288 | 18 |
| F05D2300/175 | 13 |
| C22C19/057 | 13 |
| C23C28/3455 | 11 |
| C23C28/345 | 11 |