F05D 2250/34
Translated
Official title: translated
F05D2250/34 (Translated) appears on 87 US grants and 68 published applications in this corpus.
Search patents in F05D- Granted patents
- 87
- Published applications
- 68
- Assignees
- 40
- Inventors
- 183
- Latest grant
- 5 May 2026
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 1977 | 1 | 0 |
| 1978 | 1 | 0 |
| 1979 | 0 | 0 |
| 1980 | 0 | 0 |
| 1981 | 0 | 0 |
| 1982 | 0 | 0 |
| 1983 | 0 | 0 |
| 1984 | 2 | 0 |
| 1985 | 1 | 0 |
| 1986 | 1 | 0 |
| 1987 | 1 | 0 |
| 1988 | 0 | 0 |
| 1989 | 1 | 0 |
| 1990 | 1 | 0 |
| 1991 | 1 | 0 |
| 1992 | 2 | 0 |
| 1993 | 1 | 0 |
| 1994 | 2 | 0 |
| 1995 | 1 | 0 |
| 1996 | 0 | 0 |
| 1997 | 0 | 0 |
| 1998 | 2 | 0 |
| 1999 | 2 | 0 |
| 2000 | 1 | 0 |
| 2001 | 2 | 1 |
| 2002 | 5 | 3 |
| 2003 | 0 | 0 |
| 2004 | 1 | 1 |
| 2005 | 0 | 0 |
| 2006 | 1 | 2 |
| 2007 | 0 | 0 |
| 2008 | 0 | 1 |
| 2009 | 2 | 1 |
| 2010 | 0 | 6 |
| 2011 | 0 | 2 |
| 2012 | 3 | 3 |
| 2013 | 3 | 5 |
| 2014 | 1 | 2 |
| 2015 | 5 | 7 |
| 2016 | 2 | 7 |
| 2017 | 6 | 6 |
| 2018 | 7 | 5 |
| 2019 | 6 | 3 |
| 2020 | 6 | 2 |
| 2021 | 0 | 3 |
| 2022 | 6 | 2 |
| 2023 | 3 | 3 |
| 2024 | 4 | 2 |
| 2025 | 2 | 1 |
| 2026 | 1 | 0 |
By publication year. Applications have been published since 2001. 2026 runs to 8 Oct.
Recent patents
- Variable area nozzle for an aircraft engine5 May 2026US 12,618,380 B2Rtx Corporation
- Actuating system for a cascade thrust reverser17 Jun 2025US 12,331,699 B2Safran Nacelles
- Air inlet for an aircraft propulsion unit comprising a member for moving a movable upstream portion and method for using such an air inlet4 Feb 2025US 12,214,893 B2Safran Nacelles
- Articulating slider for nacelle24 Dec 2024US 12,173,668 B2Rohr, Inc.
- Thrust reverser provided with cable kinematics for scoop flaps16 Apr 2024US 11,959,439 B2Safran Nacelles
- Variable area nozzle for an aircraft engine30 Oct 2025US 2025/0334086 A1Rtx Corporation
- Air inlet for an aircraft propulsion unit comprising a member for moving a movable upstream portion and method for using such an air inlet5 Sep 2024US 2024/0294265 A1Safran Nacelles
- Actuating system for a cascade thrust reverser30 May 2024US 2024/0175410 A1Safran Nacelles
- Articulating slider for nacelle30 Nov 2023US 2023/0383710 A1Rohr, Inc.
- Articulating slider for nacelle22 Jun 2023US 2023/0193854 A1Rohr, Inc.
Most cited
By later US patents
- Method for depositing material on the tip of a gas turbine engine airfoil using linear translational welding63US 5,160,822 AGeneral Electric Company · 1992
- Translating sleeve for cascade type thrust reversing system for fan gas turbine engine for an aircraft62US 6,170,254 B2Rohr, Inc. · 2001
- Cooled blade for a gas turbine61US 6,379,118 B2Alstom (Switzerland) Ltd · 2002
- Blocker door frame pressure structure for translating cowl of cascade thrust reverser for aircraft jet engine55US 5,927,647 ARohr, Inc. · 1999
- Plug-type exhaust nozzle having a variable centerbody and translating shroud47US 4,802,629 AThe Boeing Company · 1989