F02K 1/68
Reversers mounted on the engine housing downstream of the fan exhaust section
F02K1/68 (Reversers mounted on the engine housing downstream of the fan exhaust section) appears on 38 US grants and 36 published applications in this corpus.
Search patents in F02K- Granted patents
- 38
- Published applications
- 36
- Assignees
- 22
- Inventors
- 88
- Latest grant
- 25 Aug 2026
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 1980 | 1 | 0 |
| 1981 | 0 | 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 | 0 | 0 |
| 1991 | 0 | 0 |
| 1992 | 0 | 0 |
| 1993 | 1 | 0 |
| 1994 | 1 | 0 |
| 1995 | 0 | 0 |
| 1996 | 0 | 0 |
| 1997 | 0 | 0 |
| 1998 | 6 | 0 |
| 1999 | 0 | 0 |
| 2000 | 2 | 0 |
| 2001 | 0 | 0 |
| 2002 | 2 | 1 |
| 2003 | 0 | 0 |
| 2004 | 0 | 0 |
| 2005 | 0 | 1 |
| 2006 | 0 | 0 |
| 2007 | 0 | 0 |
| 2008 | 1 | 1 |
| 2009 | 0 | 0 |
| 2010 | 0 | 0 |
| 2011 | 0 | 2 |
| 2012 | 0 | 1 |
| 2013 | 1 | 6 |
| 2014 | 2 | 0 |
| 2015 | 2 | 6 |
| 2016 | 0 | 4 |
| 2017 | 2 | 2 |
| 2018 | 4 | 1 |
| 2019 | 3 | 0 |
| 2020 | 0 | 1 |
| 2021 | 1 | 0 |
| 2022 | 0 | 0 |
| 2023 | 1 | 3 |
| 2024 | 1 | 5 |
| 2025 | 4 | 2 |
| 2026 | 2 | 0 |
By publication year. Applications have been published since 2001. 2026 runs to 8 Oct.
Recent patents
- Electronic device for a measuring rake facilitating data loading25 Aug 2026US 12,716,814 B2Airbus Operations GmbH
- Thrust reverser comprising at least one deployable deflecting membrane5 May 2026US 12,618,382 B2Safran Nacelles
- Thrust diverter for an open rotor aircraft propulsion system24 Jun 2025US 12,338,770 B1Rtx Corporation
- Pressure measuring rake comprising a patched leading edge, in particular for an engine of an aircraft, and more particularly for a bypass turbojet engine6 May 2025US 12,292,349 B2Airbus Operations GmbH
- Multiple turn reverser with side turning vanes15 Apr 2025US 12,276,238 B2The Boeing Company
- Thrust reverser comprising at least one deployable deflecting membrane11 Dec 2025US 2025/0376963 A1Safran Nacelles
- Thrust diverter for an open rotor aircraft propulsion system9 Oct 2025US 2025/0314200 A1Rtx Corporation
- Rear assembly for a turbojet engine nacelle26 Dec 2024US 2024/0426260 A1Safran Nacelles
- Pressure measuring rake comprising a patched leading edge, in particular for an engine of an aircraft, and more particularly for a bypass turbojet engine22 Aug 2024US 2024/0280428 A1Airbus Operations GmbH
- Electronic device for a measuring rake facilitating data loading22 Aug 2024US 2024/0280438 A1Airbus Operations GmbH
Most cited
By later US patents
- Multi axis thrust vectoring for turbo fan engines43US 5,706,649 ABoeing North American, Inc. · 1998
- Thrust reverser for a propfan engine20US 5,343,696 AMTU Motoren-und Turbinen-Union · 1994
- Thrust reverser with extendible pivoting baffle19US 5,852,928 ASociete Hispano-Suiza · 1998
- Target type thrust reverser18US 4,216,923 ABoeing Commercial Airplane Company · 1980
- Thrust vectoring/reversing systems18US 5,782,431 A1998