F42B 10/02
Stabilising arrangements
F42B10/02 (Stabilising arrangements) appears on 1,024 US grants and 643 published applications in this corpus.
Search patents in F42B- Granted patents
- 1,024
- Published applications
- 643
- Assignees
- 302
- Inventors
- 1,589
- Latest grant
- 22 Sep 2026
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 1976 | 17 | 0 |
| 1977 | 11 | 0 |
| 1978 | 6 | 0 |
| 1979 | 11 | 0 |
| 1980 | 8 | 0 |
| 1981 | 6 | 0 |
| 1982 | 13 | 0 |
| 1983 | 7 | 0 |
| 1984 | 7 | 0 |
| 1985 | 15 | 0 |
| 1986 | 16 | 0 |
| 1987 | 31 | 0 |
| 1988 | 17 | 0 |
| 1989 | 23 | 0 |
| 1990 | 8 | 0 |
| 1991 | 22 | 0 |
| 1992 | 23 | 0 |
| 1993 | 12 | 0 |
| 1994 | 5 | 0 |
| 1995 | 9 | 0 |
| 1996 | 7 | 0 |
| 1997 | 11 | 0 |
| 1998 | 11 | 0 |
| 1999 | 9 | 0 |
| 2000 | 10 | 0 |
| 2001 | 11 | 3 |
| 2002 | 12 | 2 |
| 2003 | 8 | 14 |
| 2004 | 21 | 21 |
| 2005 | 25 | 24 |
| 2006 | 24 | 21 |
| 2007 | 16 | 24 |
| 2008 | 11 | 19 |
| 2009 | 16 | 14 |
| 2010 | 25 | 35 |
| 2011 | 21 | 20 |
| 2012 | 35 | 34 |
| 2013 | 30 | 19 |
| 2014 | 33 | 25 |
| 2015 | 26 | 15 |
| 2016 | 25 | 43 |
| 2017 | 37 | 43 |
| 2018 | 25 | 32 |
| 2019 | 41 | 33 |
| 2020 | 38 | 51 |
| 2021 | 50 | 35 |
| 2022 | 41 | 38 |
| 2023 | 45 | 20 |
| 2024 | 41 | 24 |
| 2025 | 25 | 18 |
| 2026 | 27 | 16 |
By publication year. Applications have been published since 2001. 2026 runs to 8 Oct.
Subgroups
Granted patents
- F42B 10/14Using fins spread or deployed after launch516
- F42B 10/26Using spin228
- F42B 10/04Using fixed fins193
- F42B 10/22Projectiles of cannelured type93
- F42B 10/12Using fins longitudinally-slidable with respect to the projectile or missile25
- F42B 10/025Using giratory or oscillating masses for stabilising projectile trajectory17
Recent patents
- Projectile22 Sep 2026US D1,148,948 S1G9 Holdings, LLC · Design
- Deployable canard for aerodynamic aiding of ejectable strongback separation15 Sep 2026US 12,736,316 B1Raytheon Company
- Regulation of aerodynamic loads on aircraft and missiles using azimuthally-controllable, segmented aerodynamic forebody bleed actuation25 Aug 2026US 12,716,701 B2Georgia Tech Research Corporation
- Projectile and fuze with fin18 Aug 2026US 12,710,256 B2Bae Systems Bofors AB
- Enhanced payload delivery18 Aug 2026US 12,710,257 B2Helix Defense
- Midair item dispenser systems and methods8 Oct 2026US 2026/0307790 A1
- System for controlling wing sweep angle and unmanned aerial vehicle including the same1 Oct 2026US 2026/0296690 A1Hanwha Aerospace Co., Ltd.
- Tail assembly for a guided and fin-stabilized projectile1 Oct 2026US 2026/0298596 A1
- Module for projectile10 Sep 2026US 2026/0266241 A1Israel Aerospace Industries Ltd.
- Deployable flap for high-g maneuvers27 Aug 2026US 2026/0251430 A1The Charles Stark Draper Laboratory, Inc.
Most cited
By later US patents
- Grooved projectiles221US 4,718,348 A1988
- Projectile with enhanced ballistics188US 9,709,368 B2G9 Holdings, LLC · 2017
- Unmanned craft126US 4,410,151 AVereinigte Flugtechnische Werke-Fokker GmbH · 1983
- Apparatus and methods for variable sweep body conformal wing with application to projectiles, missiles, and unmanned air vehicles115US 6,923,404 B1ZONA Technology, Inc. · 2005
- Airborne vehicle having deployable wing and control surface104US 6,186,443 B1International Dynamics Corporation · 2001