F42B 10/666
Characterised by using a nozzle rotatable about an axis transverse to the
Official title: {characterised by using a nozzle rotatable about an axis transverse to the axis of the projectile}
F42B10/666 (Characterised by using a nozzle rotatable about an axis transverse to the) appears on 24 US grants and 7 published applications in this corpus.
Search patents in F42B- Granted patents
- 24
- Published applications
- 7
- Assignees
- 15
- Inventors
- 35
- Latest grant
- 22 Sep 2020
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 1977 | 1 | 0 |
| 1978 | 0 | 0 |
| 1979 | 1 | 0 |
| 1980 | 0 | 0 |
| 1981 | 0 | 0 |
| 1982 | 0 | 0 |
| 1983 | 0 | 0 |
| 1984 | 1 | 0 |
| 1985 | 0 | 0 |
| 1986 | 0 | 0 |
| 1987 | 1 | 0 |
| 1988 | 1 | 0 |
| 1989 | 2 | 0 |
| 1990 | 0 | 0 |
| 1991 | 1 | 0 |
| 1992 | 0 | 0 |
| 1993 | 0 | 0 |
| 1994 | 0 | 0 |
| 1995 | 0 | 0 |
| 1996 | 1 | 0 |
| 1997 | 3 | 0 |
| 1998 | 0 | 0 |
| 1999 | 1 | 0 |
| 2000 | 0 | 0 |
| 2001 | 1 | 0 |
| 2002 | 0 | 1 |
| 2003 | 1 | 0 |
| 2004 | 0 | 0 |
| 2005 | 0 | 0 |
| 2006 | 0 | 1 |
| 2007 | 1 | 0 |
| 2008 | 0 | 1 |
| 2009 | 0 | 1 |
| 2010 | 3 | 0 |
| 2011 | 0 | 0 |
| 2012 | 0 | 1 |
| 2013 | 0 | 0 |
| 2014 | 1 | 0 |
| 2015 | 1 | 0 |
| 2016 | 0 | 1 |
| 2017 | 0 | 0 |
| 2018 | 1 | 1 |
| 2019 | 1 | 0 |
| 2020 | 1 | 0 |
By publication year. Applications have been published since 2001.
Recent patents
- Lock control device of drive gear and lock control device of actuator22 Sep 2020US 10,781,902 B2Sinfonia Technology Co., Ltd.
- Flexible energy management kill vehicle for exo-atmospheric intercept20 Aug 2019US 10,386,165 B1Lockheed Martin Corporation
- Drag reduction system24 Jul 2018US 10,030,951 B2BAE SYSTEMS plc
- Tail thruster control for projectiles13 Oct 2015US 9,157,714 B1BAE Systems Information and Electronic Systems Integration Inc.
- Tail thruster control for projectiles7 Jan 2014US 8,624,171 B2BAE Systems Information and Electronic Systems Integration Inc.
- Lock control device of drive gear and lock control device of actuator4 Oct 2018US 2018/0283512 A1Sinfonia Technology Co., Ltd.
- Drag reduction system5 May 2016US 2016/0123711 A1BAE SYSTEMS plc
- Tail thruster control for projectiles1 Mar 2012US 2012/0048991 A1BAE Systems Information and Electronic Systems Integration Inc.
- Aircraft spiraling mechanism with jet assistance - f12 Nov 2009US 2009/0277990 A1
- Aircraft spiraling mechanism with jet assistance - D25 Sep 2008US 2008/0230649 A1
Most cited
By later US patents
- Propulsion of underwater vehicles using differential and vectored thrust32US 6,581,537 B2The Penn State Research Foundation · 2003
- Detachable thrust vector mechanism for an aeronautical vehicle29US 4,844,380 AHughes Aircraft Company · 1989
- Missile control system and method29US 7,287,725 B2Raytheon Company · 2007
- Steering of an aerodynamic vehicle24US 4,163,534 AVereinigte Flugtechnische Werke-Fokker GmbH · 1979
- Differential yoke-aerofin thrust vector control system24US 5,630,564 AVersatron Corporation · 1997