F02K 1/566
By blocking the rearward discharge by means of a translatable member
Official title: {by blocking the rearward discharge by means of a translatable member}
F02K1/566 (By blocking the rearward discharge by means of a translatable member) appears on 37 US grants and 39 published applications in this corpus.
Search patents in F02K- Granted patents
- 37
- Published applications
- 39
- Assignees
- 19
- Inventors
- 70
- Latest grant
- 1 Oct 2024
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 | 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 | 1 | 0 |
| 1998 | 0 | 0 |
| 1999 | 0 | 0 |
| 2000 | 0 | 0 |
| 2001 | 0 | 0 |
| 2002 | 0 | 2 |
| 2003 | 3 | 0 |
| 2004 | 0 | 0 |
| 2005 | 0 | 0 |
| 2006 | 0 | 0 |
| 2007 | 0 | 0 |
| 2008 | 0 | 4 |
| 2009 | 0 | 1 |
| 2010 | 3 | 0 |
| 2011 | 1 | 0 |
| 2012 | 0 | 0 |
| 2013 | 1 | 5 |
| 2014 | 2 | 7 |
| 2015 | 2 | 6 |
| 2016 | 5 | 4 |
| 2017 | 4 | 2 |
| 2018 | 3 | 3 |
| 2019 | 3 | 3 |
| 2020 | 3 | 1 |
| 2021 | 1 | 0 |
| 2022 | 1 | 0 |
| 2023 | 0 | 0 |
| 2024 | 3 | 1 |
By publication year. Applications have been published since 2001.
Recent patents
- Thrust reverser for turbojet engine1 Oct 2024US 12,104,555 B2Safran Nacelles
- Plug nozzle for high mach gas turbine engines2 Jul 2024US 12,025,074 B1Rolls-Royce North American Technologies Inc.
- Method of manufacture of plug nozzle with thrust reverser6 Feb 2024US 11,891,964 B1Rolls-Royce North American Technologies Inc.
- Turbofan comprising a set of rotatable blades for blocking off the bypass flow duct2 Aug 2022US 11,401,886 B2Airbus Operations GmbH
- Nacelle6 Apr 2021US 10,968,864 B2Rohr, Inc.
- Thrust reverser for turbojet engine27 Jun 2024US 2024/0209812 A1Safran Nacelles
- Turbofan comprising a set of rotatable blades for blocking off the bypass flow duct15 Oct 2020US 2020/0325848 A1Airbus Operations GmbH
- Nacelle19 Dec 2019US 2019/0383233 A1Rohr, Inc.
- Thrust reversal on aircraft fuselage with a wing profile22 Aug 2019US 2019/0256192 A1
- Moveable exhaust plug21 Mar 2019US 2019/0085789 A1United Technologies Corporation
Most cited
By later US patents
- Cascade-type thrust reverser40US 6,546,715 B1Rohr, Inc. · 2003
- Pivoting fairings for a thrust reverser19US 7,735,778 B2Pratt & Whitney Canada Corp. · 2010
- Exhaust nozzle of a gas turbine engine16US 5,699,966 AGeneral Electric Company · 1997
- Nacelle13US 8,727,275 B2Rohr, Inc. · 2014
- Aircraft propulsive power unit9US 6,663,042 B2Short Brothers PLC · 2003