F05D 2240/124
Related to the suction side of a stator vane
Official title: related to the suction side of a stator vane
F05D2240/124 (Related to the suction side of a stator vane) appears on 146 US grants and 169 published applications in this corpus.
Search patents in F05D- Granted patents
- 146
- Published applications
- 169
- Assignees
- 43
- Inventors
- 332
- Latest grant
- 14 Jul 2026
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 2008 | 0 | 1 |
| 2009 | 0 | 1 |
| 2010 | 0 | 0 |
| 2011 | 0 | 1 |
| 2012 | 2 | 0 |
| 2013 | 0 | 0 |
| 2014 | 1 | 6 |
| 2015 | 0 | 3 |
| 2016 | 3 | 13 |
| 2017 | 1 | 16 |
| 2018 | 13 | 33 |
| 2019 | 35 | 18 |
| 2020 | 24 | 19 |
| 2021 | 9 | 20 |
| 2022 | 24 | 9 |
| 2023 | 15 | 12 |
| 2024 | 8 | 5 |
| 2025 | 9 | 4 |
| 2026 | 2 | 8 |
By publication year. 2026 runs to 8 Oct.
Recent patents
- Turbine nozzle alignment with combustor of gas turbine engines14 Jul 2026US 12,680,460 B1General Electric Company
- Coating for aluminum alloy aerostructures24 Feb 2026US 12,560,092 B2Rtx Corporation
- Turbine vane for a gas turbine engine25 Nov 2025US 12,480,406 B2Rtx Corporation
- Composite component having an additively printed inner portion11 Nov 2025US 12,467,369 B2General Electric Company
- Fan blade or vane with improved bird impact capability12 Aug 2025US 12,385,399 B2Rtx Corporation
- Coating for Aluminum Alloy Aerostructures2 Jul 2026US 2026/0185451 A1Rtx Corporation
- Aerofoil component for a high-pressure or intermediate-pressure turbine25 Jun 2026US 2026/0176974 A1ROLLS-ROYCE plc
- Gas Turbine Engine Slotted Strut25 Jun 2026US 2026/0176978 A1Pratt & Whitney Canada Corp.
- Turbine stator vane and gas turbine2 Apr 2026US 2026/0092528 A1Mitsubishi Heavy Industries, Ltd.
- Turbine vane for a gas turbine engine26 Mar 2026US 2026/0085614 A1Rtx Corporation
Most cited
By later US patents
- Turbine blade31US 8,092,175 B2Siemens Aktiengesellschaft · 2012
- Modulated hybrid variable area turbine nozzle for gas turbine engine27US 10,253,648 B2General Electric Company · 2019
- Airfoil shape for first stage compressor stator vane20US 10,087,952 B2General Electric Company · 2018
- Turbine airfoil trailing edge coolant passage created by cover12US 10,233,761 B2General Electric Company · 2019
- Vibration damping for structural guide vanes10US 9,957,824 B2United Technologies Corporation · 2018