F05D 2240/10
Stators
F05D2240/10 (Stators) appears on 6,035 US grants and 6,808 published applications in this corpus.
Search patents in F05D- Granted patents
- 6,035
- Published applications
- 6,808
- Assignees
- 543
- Inventors
- 8,680
- Latest grant
- 6 Oct 2026
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 1976 | 2 | 0 |
| 1977 | 4 | 0 |
| 1978 | 2 | 0 |
| 1979 | 3 | 0 |
| 1980 | 8 | 0 |
| 1981 | 1 | 0 |
| 1982 | 3 | 0 |
| 1983 | 0 | 0 |
| 1984 | 3 | 0 |
| 1985 | 2 | 0 |
| 1986 | 3 | 0 |
| 1987 | 2 | 0 |
| 1988 | 3 | 0 |
| 1989 | 3 | 0 |
| 1990 | 2 | 0 |
| 1991 | 3 | 0 |
| 1992 | 12 | 0 |
| 1993 | 11 | 0 |
| 1994 | 7 | 0 |
| 1995 | 4 | 0 |
| 1996 | 12 | 0 |
| 1997 | 7 | 0 |
| 1998 | 8 | 0 |
| 1999 | 7 | 0 |
| 2000 | 15 | 0 |
| 2001 | 23 | 5 |
| 2002 | 26 | 19 |
| 2003 | 27 | 18 |
| 2004 | 17 | 32 |
| 2005 | 27 | 54 |
| 2006 | 38 | 56 |
| 2007 | 34 | 85 |
| 2008 | 44 | 99 |
| 2009 | 59 | 115 |
| 2010 | 76 | 161 |
| 2011 | 82 | 126 |
| 2012 | 138 | 161 |
| 2013 | 124 | 191 |
| 2014 | 132 | 175 |
| 2015 | 162 | 245 |
| 2016 | 145 | 656 |
| 2017 | 203 | 521 |
| 2018 | 382 | 627 |
| 2019 | 647 | 627 |
| 2020 | 789 | 729 |
| 2021 | 652 | 474 |
| 2022 | 600 | 422 |
| 2023 | 497 | 393 |
| 2024 | 446 | 321 |
| 2025 | 362 | 269 |
| 2026 | 176 | 227 |
By publication year. Applications have been published since 2001. 2026 runs to 8 Oct.
Subgroups
Granted patents
Recent patents
- Stator device for disposition within a given turbine casing of a turbomachine, connection system for a turbmachine, and turbomachine6 Oct 2026US 12,753,702 B2MTU Aero Engines AG
- Bearing for turbomachine variable pitch stator vane pivot, stator vane comprising such a bearing and turbomachine comprising such stator vanes6 Oct 2026US 12,753,705 B2Safran Aircraft Engines
- Air bleed slots for gas turbine engines6 Oct 2026US 12,753,725 B1Pratt & Whitney Canada Corp.
- Turbine tip shroud removal feature29 Sep 2026US 12,747,667 B2Solar Turbines Incorporated
- Gas turbine engines having self-cooling seals and methods of operating the same29 Sep 2026US 12,747,672 B1Honeywell Aerospace US LLC
- Turbine engine component with a cooling aperture8 Oct 2026US 2026/0309042 A1General Electric Company
- Ceramic matrix composite seal repair8 Oct 2026US 2026/0309044 A1Rtx Corporation
- Entryway system including a divided volute turbocharger8 Oct 2026US 2026/0309073 A1BorgWarner Inc.
- Gas turbine engine comprising an ejector8 Oct 2026US 2026/0309081 A1ROLLS-ROYCE plc
- Abrasive flow machining process for a meridionally divided turbine housing, and a masking fixture used in said process1 Oct 2026US 2026/0295774 A1Garrett Transportation I Inc.
Most cited
By later US patents
- Counter rotating aircraft gas turbine engine with high overall pressure ratio compressor248US 6,732,502 B2General Electric Company · 2004
- Coolable airfoil for a gas turbine engine160US 6,099,251 AUnited Technologies Corporation · 2000
- System for providing mobile power138US 11,105,266 B2Yantai Jereh Petroleum Equipment & Technologies Co., Ltd. · 2021
- Mid turbine frame for gas turbine engine136US 8,091,371 B2Pratt & Whitney Canada Corp. · 2012
- Low-pressure turbine shroud124US 5,188,507 AGeneral Electric Company · 1993