F02K 1/50
Deflecting outwardly a portion of the jet by retractable scoop-like baffles
F02K1/50 (Deflecting outwardly a portion of the jet by retractable scoop-like baffles) appears on 13 US grants and 10 published applications in this corpus.
Search patents in F02K- Granted patents
- 13
- Published applications
- 10
- Assignees
- 9
- Inventors
- 16
- Latest grant
- 8 Apr 2025
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 | 0 | 0 |
| 1988 | 1 | 0 |
| 1989 | 0 | 0 |
| 1990 | 1 | 0 |
| 1991 | 0 | 0 |
| 1992 | 0 | 0 |
| 1993 | 0 | 0 |
| 1994 | 0 | 0 |
| 1995 | 0 | 0 |
| 1996 | 0 | 0 |
| 1997 | 0 | 0 |
| 1998 | 2 | 0 |
| 1999 | 0 | 0 |
| 2000 | 0 | 0 |
| 2001 | 0 | 0 |
| 2002 | 0 | 1 |
| 2003 | 1 | 1 |
| 2004 | 1 | 0 |
| 2005 | 0 | 1 |
| 2006 | 1 | 1 |
| 2007 | 0 | 0 |
| 2008 | 0 | 2 |
| 2009 | 0 | 0 |
| 2010 | 1 | 1 |
| 2011 | 0 | 0 |
| 2012 | 2 | 0 |
| 2013 | 0 | 0 |
| 2014 | 0 | 1 |
| 2015 | 0 | 0 |
| 2016 | 0 | 0 |
| 2017 | 0 | 0 |
| 2018 | 0 | 0 |
| 2019 | 0 | 0 |
| 2020 | 0 | 0 |
| 2021 | 0 | 0 |
| 2022 | 0 | 0 |
| 2023 | 0 | 0 |
| 2024 | 1 | 2 |
| 2025 | 1 | 0 |
By publication year. Applications have been published since 2001.
Recent patents
- Thrust reverser cascade with one or more flow disrupters8 Apr 2025US 12,270,356 B2Rohr, Inc.
- Thrust reverser cascade with one or more flow stabilizers16 Jan 2024US 11,873,781 B1Rohr, Inc.
- Gas turbine engine with a variable exit area fan nozzle, nacelle assembly of such a engine, and corresponding operating method4 Sep 2012US 8,256,225 B2United Technologies Corporation
- Turbojet engine with attenuated jet noise17 Jan 2012US 8,096,105 B2Airbus Operations GmbH
- Turbofan gas turbine engine and nacelle arrangement30 Mar 2010US 7,685,805 B2Pratt & Whitney Canada Corp.
- Thrust reverser cascade with one or more flow stabilizers1 Feb 2024US 2024/0035428 A1Rohr, Inc.
- Thrust reverser cascade with one or more flow disrupters1 Feb 2024US 2024/0035429 A1Rohr, Inc.
- Gas turbine engine exhaust nozzle29 May 2014US 2014/0145008 A1ROLLS-ROYCE plc
- Gas turbine engine with a variable exit area fan nozzle, nacelle assembly of such a engine, and corresponding operating method14 Jan 2010US 2010/0008764 A1United Technologies Corporation
- Turbojet Engine with Attenuated Jet Noise6 Nov 2008US 2008/0271431 A1Airbus France
Most cited
By later US patents
- Confluent variable exhaust nozzle56US 6,751,944 B2The NORDAM Group, Inc. · 2004
- Turbofan variable fan nozzle46US 6,983,588 B2The NORDAM Group, Inc. · 2006
- Exhaust flow guide for jet noise reduction23US 6,505,706 B2Pratt & Whitney Canada Corp. · 2003
- Noise-suppressing jet engine nozzles and method20US 4,280,587 AThe Boeing Company · 1981
- Variable geometry nozzle19US 4,754,924 A1988