F05D 2300/133
Titanium
F05D2300/133 (Titanium) appears on 271 US grants and 322 published applications in this corpus.
Search patents in F05D- Granted patents
- 271
- Published applications
- 322
- Assignees
- 92
- Inventors
- 736
- Latest grant
- 6 Oct 2026
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 1981 | 1 | 0 |
| 1982 | 0 | 0 |
| 1983 | 0 | 0 |
| 1984 | 0 | 0 |
| 1985 | 0 | 0 |
| 1986 | 0 | 0 |
| 1987 | 1 | 0 |
| 1988 | 0 | 0 |
| 1989 | 0 | 0 |
| 1990 | 0 | 0 |
| 1991 | 1 | 0 |
| 1992 | 0 | 0 |
| 1993 | 0 | 0 |
| 1994 | 1 | 0 |
| 1995 | 3 | 0 |
| 1996 | 2 | 0 |
| 1997 | 3 | 0 |
| 1998 | 3 | 0 |
| 1999 | 2 | 0 |
| 2000 | 3 | 0 |
| 2001 | 5 | 2 |
| 2002 | 6 | 5 |
| 2003 | 6 | 4 |
| 2004 | 2 | 7 |
| 2005 | 1 | 6 |
| 2006 | 3 | 9 |
| 2007 | 4 | 14 |
| 2008 | 7 | 16 |
| 2009 | 6 | 18 |
| 2010 | 9 | 7 |
| 2011 | 9 | 23 |
| 2012 | 11 | 13 |
| 2013 | 13 | 21 |
| 2014 | 14 | 8 |
| 2015 | 6 | 9 |
| 2016 | 13 | 34 |
| 2017 | 5 | 13 |
| 2018 | 13 | 25 |
| 2019 | 27 | 25 |
| 2020 | 34 | 27 |
| 2021 | 13 | 8 |
| 2022 | 19 | 2 |
| 2023 | 11 | 8 |
| 2024 | 4 | 7 |
| 2025 | 4 | 6 |
| 2026 | 6 | 5 |
By publication year. Applications have been published since 2001. 2026 runs to 8 Oct.
Recent patents
- Airfoils for gas turbine engines6 Oct 2026US 12,753,695 B2General Electric Company
- Facility and method for pairing a shield to a preform for the production of an aircraft turbine engine vane2 Jun 2026US 12,643,296 B2Safran
- Titanium alloy26 May 2026US 12,637,740 B2Centre National De La Recherche Scientifique
- Fire retardant engine casing apparatus12 May 2026US 12,624,648 B2General Electric Company
- Systems and methods for limiting void formation in ceramic matrix composite components21 Apr 2026US 12,606,497 B2General Electric Company
- Airfoils for gas turbine engines3 Sep 2026US 2026/0258729 A1General Electric Company
- Airfoils for gas turbine engines27 Aug 2026US 2026/0251064 A1General Electric Company
- Hollow fan blade with solid state additive manufactured cover skin27 Aug 2026US 2026/0251066 A1Rtx Corporation
- Rotor element for a turbine engine with composite blades linked to a metal disk2 Jul 2026US 2026/0185450 A1Safran Aircraft Engines
- Aircraft propulsion assembly comprising an improved cowling panel29 Jan 2026US 2026/0028939 A1Safran Nacelles
Most cited
By later US patents
- Coated article and method for inhibiting frictional wear between mating titanium alloy substrates in a gas turbine engine90US 6,158,963 AUnited Technologies Corporation · 2000
- Method for producing a titanium metallic composition having titanium boride particles dispersed therein75US 7,410,610 B2General Electric Company · 2008
- Forward swept fan blade72US 5,725,354 AGeneral Electric Company · 1998
- Stator assembly for a rotary machine and clip member for a stator assembly66US 6,409,472 B1United Technologies Corporation · 2002
- Manufacturing of Nitinol parts and forms58US 6,422,010 B1Nitinol Technologies, Inc. · 2002