Sebastien PAUTARD
Inventor
Stats
- 4 US patents issued
- 9 US Applications filed
- most recent filing
This is official USPTO record data
Details
- 4 US Patents Issued
- 9 US Applications Filed
- 45 Total Citation Count
- Dec 6, 2022 Most Recent Filing
- Oct 5, 2010 Earliest Filing
Work History
| Patent Owner | Applications Filed | Year |
|---|---|---|
| SAGEM DEFENSE SECURITE | 1
1 1 | 2010
2011 2012 |
| SAFRAN | 2
5 | 2013
2014 |
| SAFRAN ELECTRONICS & DEFENSE | 2
| 2013
|
| SNECMA | 2
3 | 2013
2014 |
Inventor Addresses
| Address | Duration |
|---|---|
| Moissy-Cramayel Cedex, FR | Apr 16, 15 - Apr 16, 15 |
| Moissy-Cramayel, FR | Feb 13, 25 - Feb 13, 25 |
| Palaiseau, FR | Aug 08, 13 - Jan 26, 21 |
| Paris, FR | Jan 16, 14 - Aug 08, 17 |
Technology Profile
| Technology | Matters | |
|---|---|---|
| B29B: | PREPARATION OR PRETREATMENT OF THE MATERIAL TO BE SHAPED; MAKING GRANULES OR PREFORMS; RECOVERY OF PLASTICS OR OTHER CONSTITUENTS OF WASTE MATERIAL CONTAINING PLASTICS | 2 |
| B29C: | SHAPING OR JOINING OF PLASTICS; SHAPING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL; AFTER- TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING | 2 |
| B29D: | PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE | 1 |
Patents / Publication
| Patents / Publication # | Year of Publication / Issued | Title | Citations |
|---|---|---|---|
| 2025/0050,546 | 2025 | METHOD FOR PRODUCING A BLADED COMPONENT FOR AN AIRCRAFT TURBINE ENGINE | 0 |
| 10899051 | 2021 | Method of fabricating a composite material blade having an integrated metal leading edge for a gas turbine aeroengine | 1 |
| 9784112 | 2017 | Turbine engine vane with asymmetrical profile | 0 |
| 9725182 | 2017 | Aircraft throttle control device including a cam coupling | 1 |
| 9470502 | 2016 | Fluxgate with laminar damping of the pendulum and method of assembling a fluxgate | 0 |
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