F05D 2240/00
Components
F05D2240/00 (Components) appears on 14,901 US grants and 16,900 published applications in this corpus.
Search patents in F05D- Granted patents
- 14,901
- Published applications
- 16,900
- Assignees
- 1,401
- Inventors
- 18,788
- Latest grant
- 6 Oct 2026
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 1976 | 7 | 0 |
| 1977 | 15 | 0 |
| 1978 | 11 | 0 |
| 1979 | 9 | 0 |
| 1980 | 17 | 0 |
| 1981 | 17 | 0 |
| 1982 | 9 | 0 |
| 1983 | 5 | 0 |
| 1984 | 5 | 0 |
| 1985 | 12 | 0 |
| 1986 | 10 | 0 |
| 1987 | 16 | 0 |
| 1988 | 13 | 0 |
| 1989 | 12 | 0 |
| 1990 | 14 | 0 |
| 1991 | 5 | 0 |
| 1992 | 31 | 0 |
| 1993 | 28 | 0 |
| 1994 | 26 | 0 |
| 1995 | 19 | 0 |
| 1996 | 31 | 0 |
| 1997 | 34 | 0 |
| 1998 | 37 | 0 |
| 1999 | 43 | 0 |
| 2000 | 63 | 0 |
| 2001 | 77 | 20 |
| 2002 | 102 | 64 |
| 2003 | 83 | 72 |
| 2004 | 78 | 117 |
| 2005 | 78 | 150 |
| 2006 | 109 | 152 |
| 2007 | 87 | 219 |
| 2008 | 96 | 230 |
| 2009 | 141 | 260 |
| 2010 | 163 | 366 |
| 2011 | 184 | 316 |
| 2012 | 338 | 383 |
| 2013 | 292 | 564 |
| 2014 | 354 | 484 |
| 2015 | 360 | 679 |
| 2016 | 407 | 1626 |
| 2017 | 597 | 1386 |
| 2018 | 1007 | 1511 |
| 2019 | 1542 | 1434 |
| 2020 | 1765 | 1610 |
| 2021 | 1483 | 1189 |
| 2022 | 1475 | 1057 |
| 2023 | 1194 | 964 |
| 2024 | 1058 | 813 |
| 2025 | 883 | 679 |
| 2026 | 459 | 555 |
By publication year. Applications have been published since 2001. 2026 runs to 8 Oct.
Subgroups
Granted patents
- F05D 2240/10StatorsIndexing code6,035
- F05D 2240/20RotorsIndexing code3,981
- F05D 2240/55SealsIndexing code2,624
- F05D 2240/80Platforms for stationary or moving bladesIndexing code1,735
- F05D 2240/35Combustors or associated equipmentIndexing code1,602
- F05D 2240/50BearingsIndexing code1,286
- F05D 2240/60ShaftsIndexing code889
- F05D 2240/90Mounting on supporting structures or systemsIndexing code386
Recent patents
- Aircraft with an unducted fan propulsor6 Oct 2026US 12,752,923 B2General Electric Company
- Airfoils for gas turbine engines6 Oct 2026US 12,753,695 B2General Electric Company
- Turbine engine with a blade assembly having a set of cooling conduits6 Oct 2026US 12,753,696 B2General Electric Company
- 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
- Method for attaching a metal reinforcement on a leading edge of a turbomachine blade8 Oct 2026US 2026/0307338 A1Safran Aerospace Composites
- Turbine engine rotor blade with tip shelf8 Oct 2026US 2026/0309032 A1Rtx Corporation
- Turbine engine component with a cooling aperture8 Oct 2026US 2026/0309034 A1
- Turbine engine having an airfoil with a set of cooling holes8 Oct 2026US 2026/0309035 A1
- Assembly for maintaining and retaining a gas turbine engine component8 Oct 2026US 2026/0309037 A1Rtx Corporation
Most cited
By later US patents
- Coupling system for a planetary gear train525US 5,433,674 AUnited Technologies Corporation · 1995
- Expandable impeller pump391US 7,393,181 B2Datascope Investment Corp. · 2008
- Flexible shaft for gas turbine engine391US 7,926,260 B2United Technologies Corporation · 2011
- Low solidity turbofan352US 7,374,403 B2General Electric Company · 2008
- Mobile, modular, electrically powered system for use in fracturing underground formations using liquid petroleum gas341US 9,140,110 B2Evolution Well Services, LLC · 2015