F05D 2230/238
Soldering
F05D2230/238 (Soldering) appears on 40 US grants and 63 published applications in this corpus.
Search patents in F05D- Granted patents
- 40
- Published applications
- 63
- Assignees
- 27
- Inventors
- 164
- Latest grant
- 3 Jun 2025
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 2007 | 0 | 1 |
| 2008 | 0 | 3 |
| 2009 | 0 | 4 |
| 2010 | 0 | 5 |
| 2011 | 3 | 3 |
| 2012 | 2 | 4 |
| 2013 | 2 | 4 |
| 2014 | 2 | 0 |
| 2015 | 2 | 7 |
| 2016 | 2 | 8 |
| 2017 | 4 | 5 |
| 2018 | 4 | 6 |
| 2019 | 3 | 1 |
| 2020 | 3 | 5 |
| 2021 | 5 | 1 |
| 2022 | 1 | 2 |
| 2023 | 3 | 1 |
| 2024 | 2 | 2 |
| 2025 | 2 | 0 |
| 2026 | 0 | 1 |
By publication year. 2026 runs to 8 Oct.
Recent patents
- Stator vane assembly for an aircraft turbine engine compressor3 Jun 2025US 12,320,275 B2Safran Aero Boosters SA
- Cooling jacket of a hollow blade of a distributor14 Jan 2025US 12,196,105 B2Safran Aircraft Engines
- Combustor for rocket engine and method for manufacturing it24 Sep 2024US 12,098,691 B2InterStellar Technologies Corporation
- Method for manufacturing a structural surface heat exchanger for a nacelle30 Jan 2024US 11,883,874 B2Safran Nacelles
- Blade for a turbine engine, associated turbine engine distributor and turbine engine24 Oct 2023US 11,795,828 B2Safran Aircraft Engines
- Tandem guide vane component for a stator stage and method for manufacturing a tandem guide vane component18 Jun 2026US 2026/0168517 A1Rolls-Royce Deutschland Ltd & Co KG
- Cooling jacket of a hollow blade of a distributor15 Aug 2024US 2024/0271535 A1Safran Aircraft Engines
- Stator vane assembly for an aircraft turbine engine compressor11 Apr 2024US 2024/0117747 A1Safran Aero Boosters SA
- Combustor for rocket engine and method for manufacturing it27 Apr 2023US 2023/0125860 A1InterStellar Technologies Corporation
- Blade for a turbine engine, associated turbine engine distributor and turbine engine2 Jun 2022US 2022/0170377 A1Safran Aircraft Engines
Most cited
By later US patents
- Method for forming a directionally solidified replacement body for a component using additive manufacturing23US 9,452,474 B2United Technologies Corporation · 2016
- Method of producing or repairing turbine or engine components, and a component, namely a turbine or engine component21US 8,555,500 B2MTU Aero Engines AG · 2013
- Damping inlay for turbine blades7US 10,041,359 B2Ansaldo Energia Switzerland AG · 2018
- Nozzle for a turbomachine turbine7US 8,662,835 B2Snecma · 2014
- Method for the soldering repair of a component in a vacuum and an adjusted partial oxygen pressure6US 7,874,473 B2MTU Aero Engines AG · 2011