F02K 1/58
Reversers mounted on the inner cone or the nozzle housing or the
Official title: Reversers mounted on the inner cone or the nozzle housing {or the fuselage}
F02K1/58 (Reversers mounted on the inner cone or the nozzle housing or the) appears on 18 US grants and 16 published applications in this corpus.
Search patents in F02K- Granted patents
- 18
- Published applications
- 16
- Assignees
- 15
- Inventors
- 34
- Latest grant
- 25 Mar 2025
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 1976 | 1 | 0 |
| 1977 | 0 | 0 |
| 1978 | 1 | 0 |
| 1979 | 0 | 0 |
| 1980 | 0 | 0 |
| 1981 | 1 | 0 |
| 1982 | 0 | 0 |
| 1983 | 0 | 0 |
| 1984 | 0 | 0 |
| 1985 | 0 | 0 |
| 1986 | 0 | 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 | 0 | 0 |
| 1996 | 0 | 0 |
| 1997 | 0 | 0 |
| 1998 | 1 | 0 |
| 1999 | 0 | 0 |
| 2000 | 0 | 0 |
| 2001 | 0 | 0 |
| 2002 | 0 | 0 |
| 2003 | 0 | 0 |
| 2004 | 0 | 0 |
| 2005 | 0 | 0 |
| 2006 | 0 | 1 |
| 2007 | 0 | 0 |
| 2008 | 0 | 0 |
| 2009 | 0 | 0 |
| 2010 | 0 | 2 |
| 2011 | 0 | 1 |
| 2012 | 1 | 0 |
| 2013 | 0 | 0 |
| 2014 | 0 | 1 |
| 2015 | 1 | 1 |
| 2016 | 0 | 2 |
| 2017 | 1 | 0 |
| 2018 | 2 | 3 |
| 2019 | 1 | 1 |
| 2020 | 2 | 1 |
| 2021 | 2 | 1 |
| 2022 | 1 | 0 |
| 2023 | 0 | 2 |
| 2024 | 2 | 0 |
| 2025 | 1 | 0 |
By publication year. Applications have been published since 2001.
Recent patents
- Thrust reverser with door of a nacelle of a turbojet engine of an aircraft with a system for diverting fluids to the exterior25 Mar 2025US 12,258,924 B2Safran Nacelles
- Gas turbine engine nozzle loft for thrust reverser4 Jun 2024US 12,000,358 B1Pratt & Whitney Canada Corp.
- Variable area nozzle and method for operating same28 May 2024US 11,994,087 B2Rohr, Inc.
- Variable area nozzle exhaust system with integrated thrust reverser29 Mar 2022US 11,286,878 B2Rolls-Royce Cornoration
- Thrust reverser flow limiting valve6 Jul 2021US 11,053,889 B2Woodward, Inc.
- Thrust reverser at the door of a nacelle of a turbojet engine of an aircraft with a system for diverting fluids to the exterior15 Jun 2023US 2023/0184193 A1Safran Nacelles
- Variable area nozzle and method for operating same8 Jun 2023US 2023/0175457 A1Rohr, Inc.
- Variable area nozzle exhaust system with integrated thrust reverser30 Sep 2021US 2021/0301761 A1Rolls-Royce North American Technologies Inc.
- Thrust reverser flow limiting valve23 Jan 2020US 2020/0025142 A1Woodward, Inc.
- Thrust reversal on aircraft fuselage with a wing profile22 Aug 2019US 2019/0256192 A1
Most cited
By later US patents
- Thrust vectoring/reversing systems18US 5,782,431 A1998
- Deformable plug for an aircraft engine exhaust nozzle16US 4,074,859 AThe United States of America as represented by the Secretary of the Air Force · 1978
- Overwing thrust reverser8US 3,981,463 ARohr Industries, Inc. · 1976
- Thrust reverser flow limiting valve6US 10,288,007 B2Woodward, Inc. · 2019
- Variable area nozzle exhaust system with integrated thrust reverser5US 11,286,878 B2Rolls-Royce Cornoration · 2022