F05D 2230/233
Electron beam welding
F05D2230/233 (Electron beam welding) appears on 78 US grants and 133 published applications in this corpus.
Search patents in F05D- Granted patents
- 78
- Published applications
- 133
- Assignees
- 49
- Inventors
- 333
- Latest grant
- 17 Feb 2026
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 2002 | 1 | 1 |
| 2003 | 0 | 0 |
| 2004 | 0 | 1 |
| 2005 | 1 | 1 |
| 2006 | 0 | 3 |
| 2007 | 1 | 3 |
| 2008 | 0 | 4 |
| 2009 | 0 | 3 |
| 2010 | 1 | 6 |
| 2011 | 2 | 6 |
| 2012 | 4 | 6 |
| 2013 | 1 | 8 |
| 2014 | 4 | 4 |
| 2015 | 7 | 3 |
| 2016 | 4 | 17 |
| 2017 | 2 | 9 |
| 2018 | 4 | 11 |
| 2019 | 11 | 13 |
| 2020 | 8 | 9 |
| 2021 | 8 | 2 |
| 2022 | 5 | 3 |
| 2023 | 4 | 4 |
| 2024 | 4 | 8 |
| 2025 | 5 | 4 |
| 2026 | 1 | 4 |
By publication year. 2026 runs to 8 Oct.
Recent patents
- Adaptive component overhaul using structured light scan data17 Feb 2026US 12,551,974 B2Pratt & Whitney Canada Corp.
- System and method for forming single crystal components using additive manufacturing tooling18 Nov 2025US 12,472,553 B2SingleX AB
- Adaptive manufacturing using structured light data15 Jul 2025US 12,358,232 B2Pratt & Whitney Canada Corp.
- Method for producing a part by selective melting of powder24 Jun 2025US 12,337,528 B2Safran Aircraft Engines
- Airfoil joining apparatus and methods27 May 2025US 12,312,973 B2General Electric Company
- Expander and method of manufacturing24 Sep 2026US 2026/0286848 A1Nuovo Pignone Tecnologie Srl
- Adaptive component overhaul using structured light scan data18 Jun 2026US 2026/0166659 A1Pratt & Whitney Canada Corp.
- Method for manufacturing a metal protection device for the leading edge of a blade incorporating a de-icing system and protection device obtained by this method11 Jun 2026US 2026/0160170 A1Safran
- Clearance control system for blade outer air seal28 May 2026US 2026/0146544 A1Rtx Corporation
- Airfoil joining apparatus and methods14 Aug 2025US 2025/0257659 A1General Electric Company
Most cited
By later US patents
- Apparatus and process for refining features in an additive manufactured part23US 10,006,293 B1Florida Turbine Technologies, Inc. · 2018
- Method for forming a directionally solidified replacement body for a component using additive manufacturing23US 9,452,474 B2United Technologies Corporation · 2016
- Rocket engine having a transition attachment between a combustion chamber and an injector14US 6,381,949 B12002
- Methods for making near net shape airfoil leading edge protection13US 8,240,046 B2General Electric Company · 2012
- Turbine blade having a constant thickness airfoil skin13US 8,292,583 B2Siemens Energy, Inc. · 2012