Jago Pridie
Inventor
Stats
- 2 US patents issued
- 15 US Applications filed
- most recent filing
This is official USPTO record data
Details
- 2 US Patents Issued
- 15 US Applications Filed
- 65 Total Citation Count
- May 6, 2024 Most Recent Filing
- Sep 25, 2003 Earliest Filing
Work History
| Patent Owner | Applications Filed | Year |
|---|---|---|
| AIRBUS OPERATIONS LIMITED | 2
1 2 2 1 | 2003
2007 2008 2010 2013 |
Inventor Addresses
| Address | Duration |
|---|---|
| Bath, GB | Jan 05, 12 - Apr 16, 13 |
| Bristol, GB | Jul 27, 06 - Jul 10, 18 |
| NANTES, FR | Aug 22, 19 - Aug 06, 20 |
| Nantes, FR | Mar 22, 18 - Jan 16, 24 |
| TOULOUSE, FR | Apr 22, 21 - Aug 24, 23 |
| Toulouse, FR | Jul 29, 21 - Aug 29, 24 |
Technology Profile
| Technology | Matters | |
|---|---|---|
| B28B: | SHAPING CLAY OR OTHER CERAMIC COMPOSITIONS, SLAG OR MIXTURES CONTAINING CEMENTITIOUS MATERIAL, e.g. PLASTER | 1 |
| B29C: | SHAPING OR JOINING OF PLASTICS; SHAPING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL; AFTER- TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING | 15 |
| B29D: | PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE | 4 |
Patents / Publication
| Patents / Publication # | Year of Publication / Issued | Title | Citations |
|---|---|---|---|
| 2024/0286,370 | 2024 | DEVICE FOR MANUFACTURING A STIFFENED PANEL MAKING IT POSSIBLE TO CONTROL THE GEOMETRY OF SAID STIFFENED PANEL, AND METHOD FOR MANUFACTURING A STIFFENED PANEL USING SAID DEVICE | 0 |
| 12005665 | 2024 | Device for manufacturing a stiffened panel making it possible to control the geometry of said stiffened panel, and method for manufacturing a stiffened panel using said device | 0 |
| 11919259 | 2024 | Method for fabricating a central caisson of an aircraft wing made from composite material | 0 |
| 11872769 | 2024 | Method for manufacturing connecting members for connecting an aircraft wing to a center wing box, using preforms | 0 |
| 2023/0264,804 | 2023 | METHOD FOR MANUFACTURING AT LEAST ONE PORTION OF A BOX STRUCTURE OF AN AIRCRAFT COMPRISING A FORMING STEP, AND A CENTRAL WINGBOX THUS OBTAINED | 0 |
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