Maxime BRIEND
Inventor
Stats
- 1 US patents issued
- 4 US Applications filed
- most recent filing
This is official USPTO record data
Details
- 1 US Patents Issued
- 4 US Applications Filed
- 14 Total Citation Count
- Sep 8, 2016 Most Recent Filing
- Oct 10, 2014 Earliest Filing
Work History
Patent Owner | Applications Filed | Year |
---|---|---|
SAFRAN | 3
1 | 2014
2015 |
SNECMA | 3
| 2014
|
SAFRAN AIRCRAFT ENGINES | 1
| 2015
|
Inventor Addresses
Address | Duration |
---|---|
Massy, FR | Jun 02, 16 - Oct 10, 17 |
Moissy-Cramayel Cedex, FR | Apr 16, 15 - Sep 07, 17 |
Moissy-Cramayel, FR | Sep 13, 18 - Nov 12, 19 |
Technology Profile
Technology | Matters | |
---|---|---|
B21D: | WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING | 1 |
B23H: | WORKING OF METAL BY THE ACTION OF A HIGH CONCENTRATION OF ELECTRIC CURRENT ON A WORKPIECE USING AN ELECTRODE WHICH TAKES THE PLACE OF A TOOL; SUCH WORKING COMBINED WITH OTHER FORMS OF WORKING OF METAL | 1 |
B23K: | SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM | 1 |
Patents / Publication
Patents / Publication # | Year of Publication / Issued | Title | Citations |
---|---|---|---|
10471556 | 2019 | Method for producing a protective reinforcement for a blade (P) having a curved leading edge or trailing edge | 0 |
2018/0257,185 | 2018 | METHOD FOR PRODUCING A PROTECTIVE REINFORCEMENT FOR A BLADE (P) HAVING A CURVED LEADING EDGE OR TRAILING EDGE | 1 |
9784112 | 2017 | Turbine engine vane with asymmetrical profile | 0 |
2017/0254,212 | 2017 | A GUIDE VANE MADE OF COMPOSITE MATERIAL FOR A GAS TURBINE ENGINE, AND IT'S METHOD OF FABRICATION | 5 |
2016/0153,295 | 2016 | COMPOSITE VANE FOR A TURBINE ENGINE | 7 |
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