F42B 10/665
Characterised by using a nozzle provided with at least a deflector mounted
Official title: {characterised by using a nozzle provided with at least a deflector mounted within the nozzle}
F42B10/665 (Characterised by using a nozzle provided with at least a deflector mounted) appears on 40 US grants and 20 published applications in this corpus.
Search patents in F42B- Granted patents
- 40
- Published applications
- 20
- Assignees
- 23
- Inventors
- 89
- Latest grant
- 11 Aug 2026
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 1976 | 1 | 0 |
| 1977 | 1 | 0 |
| 1978 | 0 | 0 |
| 1979 | 0 | 0 |
| 1980 | 0 | 0 |
| 1981 | 2 | 0 |
| 1982 | 2 | 0 |
| 1983 | 1 | 0 |
| 1984 | 0 | 0 |
| 1985 | 0 | 0 |
| 1986 | 2 | 0 |
| 1987 | 1 | 0 |
| 1988 | 1 | 0 |
| 1989 | 0 | 0 |
| 1990 | 1 | 0 |
| 1991 | 1 | 0 |
| 1992 | 2 | 0 |
| 1993 | 0 | 0 |
| 1994 | 0 | 0 |
| 1995 | 0 | 0 |
| 1996 | 1 | 0 |
| 1997 | 0 | 0 |
| 1998 | 1 | 0 |
| 1999 | 1 | 0 |
| 2000 | 0 | 0 |
| 2001 | 2 | 0 |
| 2002 | 0 | 2 |
| 2003 | 1 | 0 |
| 2004 | 2 | 0 |
| 2005 | 0 | 1 |
| 2006 | 0 | 0 |
| 2007 | 0 | 2 |
| 2008 | 2 | 1 |
| 2009 | 0 | 1 |
| 2010 | 2 | 3 |
| 2011 | 0 | 1 |
| 2012 | 3 | 1 |
| 2013 | 2 | 0 |
| 2014 | 0 | 1 |
| 2015 | 1 | 0 |
| 2016 | 0 | 3 |
| 2017 | 1 | 0 |
| 2018 | 1 | 0 |
| 2019 | 0 | 0 |
| 2020 | 1 | 2 |
| 2021 | 1 | 0 |
| 2022 | 0 | 1 |
| 2023 | 1 | 1 |
| 2024 | 1 | 0 |
| 2025 | 0 | 0 |
| 2026 | 1 | 0 |
By publication year. Applications have been published since 2001. 2026 runs to 8 Oct.
Recent patents
- Fin control actuation system11 Aug 2026US 12,704,361 B2Rafael Advanced Defense Systems Ltd.
- Method for reducing jet tab exposure during thrust vectoring23 Jan 2024US 11,879,416 B1Raytheon Company
- Steering system with power take-off from actuators22 Aug 2023US 11,733,011 B2Raytheon Company
- Device for deflecting a stream of particles for a projectile guided by a link wire17 Aug 2021US 11,092,412 B2Mbda France
- Rocket motor with combustion product deflector23 Jun 2020US 10,690,443 B1Raytheon Company
- Fin control actuation system23 Nov 2023US 2023/0375317 A1Rafael Advanced Defense Systems Ltd.
- Steering system with power take-off from actuators26 May 2022US 2022/0163302 A1Raytheon Company
- Rocket motor with combustion product deflector16 Jul 2020US 2020/0225002 A1Raytheon Company
- Device for deflecting a stream of particles for a projectile guided by a link wire14 May 2020US 2020/0149849 A1Mbda France
- Thrust vectoring device10 Nov 2016US 2016/0326987 A1Mitsubishi Heavy Industries, Ltd.
Most cited
By later US patents
- Missile jet vane control system and method50US 5,806,791 ARaytheon Company · 1998
- Method and apparatus for non-propulsive fin control in an air or sea vehicle using planar actuation45US 6,247,666 B1Lockheed Martin Corporation · 2001
- Propulsion/control modular booster32US 4,364,530 AThe United States of America as represented by the Secretary of the Navy · 1982
- Jet tab control mechanism for thrust vector control24US 4,274,610 AGeneral Dynamics, Pomona Division · 1981
- Aerodynamic control mechanism for thrust vector control22US 4,272,040 AGeneral Dynamics, Pomona Division · 1981