F05D 2240/125
Related to the tip of a stator vane
Official title: related to the tip of a stator vane
F05D2240/125 (Related to the tip of a stator vane) appears on 102 US grants and 125 published applications in this corpus.
Search patents in F05D- Granted patents
- 102
- Published applications
- 125
- Assignees
- 46
- Inventors
- 297
- Latest grant
- 28 Jul 2026
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 1997 | 1 | 0 |
| 1998 | 0 | 0 |
| 1999 | 0 | 0 |
| 2000 | 0 | 0 |
| 2001 | 0 | 0 |
| 2002 | 0 | 0 |
| 2003 | 0 | 0 |
| 2004 | 0 | 0 |
| 2005 | 0 | 0 |
| 2006 | 0 | 0 |
| 2007 | 0 | 1 |
| 2008 | 0 | 0 |
| 2009 | 0 | 0 |
| 2010 | 1 | 0 |
| 2011 | 0 | 1 |
| 2012 | 0 | 2 |
| 2013 | 1 | 6 |
| 2014 | 3 | 6 |
| 2015 | 1 | 6 |
| 2016 | 6 | 15 |
| 2017 | 5 | 13 |
| 2018 | 9 | 20 |
| 2019 | 10 | 7 |
| 2020 | 21 | 14 |
| 2021 | 8 | 6 |
| 2022 | 10 | 8 |
| 2023 | 5 | 6 |
| 2024 | 10 | 6 |
| 2025 | 6 | 5 |
| 2026 | 5 | 3 |
By publication year. Applications have been published since 2001. 2026 runs to 8 Oct.
Recent patents
- Guide vane, guide vane cluster, and housing for a gas turbine as well as gas turbine having a platform with an arched wall section to receive a damper28 Jul 2026US 12,692,794 B2MTU Aero Engines AG
- Aircraft engine with stator having varying pitch21 Jul 2026US 12,687,114 B2Pratt & Whitney Canada Corp.
- Turbine nozzle alignment with combustor of gas turbine engines14 Jul 2026US 12,680,460 B1General Electric Company
- Forward load reduction structures for aft-most stages of high pressure compressors14 Jul 2026US 12,680,557 B2General Electric Company
- Sandblasting mask31 Mar 2026US 12,589,466 B2Safran Aero Boosters SA
- Blading system for axial compressors with axially opposing base merged double triangular prism device blades6 Aug 2026US 2026/0226914 A1Spacerolls Aerospace Technologies Private Limited
- Stator part with blade and fin arrangement in a turbomachine23 Jul 2026US 2026/0210253 A1Safran
- Aircraft with an unducted fan propulsor26 Feb 2026US 2026/0054843 A1General Electric Company
- Multi-station edm for vanes18 Dec 2025US 2025/0381607 A1Chromalloy Gas Turbine Corporation
- Engine component6 Nov 2025US 2025/0341166 A1General Electric Company
Most cited
By later US patents
- Turbine airfoil components containing ceramic-based materials and processes therefor19US 8,777,583 B2General Electric Company · 2014
- Airfoil components containing ceramic-based materials and processes therefor19US 9,410,437 B2General Electric Company · 2016
- Turbomachine fan flow-straightener vane, turbomachine assembly comprising such a vane and turbomachine equipped with said vane or said assembly16US 11,377,958 B2Safran Aircraft Engines · 2022
- High order shaped curve region for an airfoil11US 9,017,036 B2United Technologies Corporation · 2015
- Turbine stator vane9US 8,702,375 B1Florida Turbine Technologies, Inc. · 2014