F02K 1/10
By distorting the jet pipe or nozzle
Official title: by distorting the jet pipe or nozzle
F02K1/10 (By distorting the jet pipe or nozzle) appears on 31 US grants and 32 published applications in this corpus.
Search patents in F02K- Granted patents
- 31
- Published applications
- 32
- Assignees
- 16
- Inventors
- 66
- Latest grant
- 8 Sep 2026
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 1986 | 1 | 0 |
| 1987 | 0 | 0 |
| 1988 | 0 | 0 |
| 1989 | 0 | 0 |
| 1990 | 0 | 0 |
| 1991 | 0 | 0 |
| 1992 | 0 | 0 |
| 1993 | 0 | 0 |
| 1994 | 0 | 0 |
| 1995 | 1 | 0 |
| 1996 | 0 | 0 |
| 1997 | 0 | 0 |
| 1998 | 0 | 0 |
| 1999 | 0 | 0 |
| 2000 | 1 | 0 |
| 2001 | 0 | 0 |
| 2002 | 0 | 0 |
| 2003 | 1 | 1 |
| 2004 | 0 | 1 |
| 2005 | 0 | 0 |
| 2006 | 0 | 0 |
| 2007 | 0 | 0 |
| 2008 | 0 | 2 |
| 2009 | 0 | 5 |
| 2010 | 1 | 3 |
| 2011 | 1 | 1 |
| 2012 | 3 | 1 |
| 2013 | 3 | 1 |
| 2014 | 0 | 2 |
| 2015 | 2 | 2 |
| 2016 | 2 | 4 |
| 2017 | 2 | 1 |
| 2018 | 3 | 1 |
| 2019 | 3 | 0 |
| 2020 | 0 | 1 |
| 2021 | 0 | 1 |
| 2022 | 1 | 0 |
| 2023 | 1 | 2 |
| 2024 | 1 | 1 |
| 2025 | 1 | 0 |
| 2026 | 3 | 2 |
By publication year. Applications have been published since 2001. 2026 runs to 8 Oct.
Recent patents
- Jet nozzle effective area control system for gas turbine engine8 Sep 2026US 12,729,658 B2Pratt & Whitney Canada Corp.
- Aircraft powerplant exhaust section with flow diverter1 Sep 2026US 12,723,555 B2Pratt & Whitney Canada Corp.
- Variable geometry nozzle utilizing magnetic fluid10 Mar 2026US 12,569,863 B2Hamilton Sundstrand Corporation
- Propulsion system with downstream section having deformable shape-memory material and actuators extending in different consecutive angular sectors1 Apr 2025US 12,264,637 B2Safran
- Propulsion system for an aircraft19 Mar 2024US 11,932,410 B2Safran
- Aircraft powerplant exhaust section with flow diverter2 Apr 2026US 2026/0092578 A1Pratt & Whitney Canada Corp.
- Jet nozzle effective area control system for gas turbine engine26 Feb 2026US 2026/0055741 A1Pratt & Whitney Canada Corp.
- Propulsion system for an aircraft14 Mar 2024US 2024/0084761 A1Safran
- Variable geometry nozzle utilizing magnetic fluid28 Dec 2023US 2023/0415174 A1Hamilton Sundstrand Corporation
- Propulsion system for an aircraft11 May 2023US 2023/0145551 A1Safran
Most cited
By later US patents
- High stiffness shape memory alloy actuated aerostructure20US 8,434,293 B2The Boeing Company · 2013
- Gas turbine engine exhaust nozzle having a composite article having a shape memory material member18US 8,291,710 B2ROLLS-ROYCE plc · 2012
- Thrust reverser with throat trimming capability15US 6,027,071 A2000
- Thermally graded adaptive multifunctional cellular structures with shape memory alloys13US 10,053,239 B2The Boeing Company · 2018
- Apparatus and method for thrust vector control13US 6,622,472 B2Gateway Space Transport, Inc. · 2003