F02K 1/1292
Of three series of flaps, the upstream series having its flaps hinged
Official title: {of three series of flaps, the upstream series having its flaps hinged at their upstream ends on a fixed structure, the internal downstream series having its flaps hinged at their upstream ends on the downstream ends of the flaps of the upstream series and at their downstream ends on the downstream ends of the flaps of the external downstream series hinged at their upstream ends on a substantially axially movable structure}
F02K1/1292 (Of three series of flaps, the upstream series having its flaps hinged) appears on 61 US grants and 21 published applications in this corpus.
Search patents in F02K- Granted patents
- 61
- Published applications
- 21
- Assignees
- 17
- Inventors
- 98
- Latest grant
- 16 Dec 2025
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 1976 | 1 | 0 |
| 1977 | 1 | 0 |
| 1978 | 0 | 0 |
| 1979 | 0 | 0 |
| 1980 | 0 | 0 |
| 1981 | 0 | 0 |
| 1982 | 0 | 0 |
| 1983 | 0 | 0 |
| 1984 | 4 | 0 |
| 1985 | 3 | 0 |
| 1986 | 1 | 0 |
| 1987 | 0 | 0 |
| 1988 | 2 | 0 |
| 1989 | 0 | 0 |
| 1990 | 2 | 0 |
| 1991 | 3 | 0 |
| 1992 | 3 | 0 |
| 1993 | 3 | 0 |
| 1994 | 4 | 0 |
| 1995 | 1 | 0 |
| 1996 | 4 | 0 |
| 1997 | 0 | 0 |
| 1998 | 0 | 0 |
| 1999 | 1 | 0 |
| 2000 | 0 | 0 |
| 2001 | 4 | 0 |
| 2002 | 4 | 0 |
| 2003 | 0 | 0 |
| 2004 | 0 | 0 |
| 2005 | 1 | 5 |
| 2006 | 3 | 1 |
| 2007 | 2 | 3 |
| 2008 | 0 | 0 |
| 2009 | 2 | 1 |
| 2010 | 1 | 1 |
| 2011 | 0 | 0 |
| 2012 | 0 | 0 |
| 2013 | 0 | 0 |
| 2014 | 1 | 1 |
| 2015 | 0 | 1 |
| 2016 | 0 | 2 |
| 2017 | 1 | 1 |
| 2018 | 2 | 0 |
| 2019 | 2 | 0 |
| 2020 | 0 | 0 |
| 2021 | 0 | 0 |
| 2022 | 0 | 1 |
| 2023 | 2 | 3 |
| 2024 | 2 | 0 |
| 2025 | 1 | 1 |
By publication year. Applications have been published since 2001.
Recent patents
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- Variable area nozzle and method for operating same8 Jun 2023US 2023/0175457 A1Rohr, Inc.
- Mixed flow exhaust thrust reverser with area control nozzle systems and methods25 May 2023US 2023/0160355 A1Rohr, Inc.
- Convergent-divergent flap pair for a variable-geometry turbojet engine nozzle comprising cooling air circulation ducts connected through contact surfaces15 Sep 2022US 2022/0290631 A1Safran Aircraft Engines
Most cited
By later US patents
- Axisymmetric vectoring exhaust nozzle79US 4,994,660 AHitachi, Ltd. · 1991
- Nozzle construction providing for thermal growth40US 3,972,475 AUnited Technologies Corporation · 1976
- Axisymmetric vectoring exhaust nozzle thermal shield38US 5,485,959 AGeneral Electric Company · 1996
- Thrust vectorable exhaust nozzle37US 4,000,854 AGeneral Electric Company · 1977
- Nozzle with thrust vectoring in the yaw direction37US 4,978,071 AGeneral Electric Company · 1990