F16F 2230/16
Used in a strut, basically rigid
Official title: used in a strut, basically rigid
F16F2230/16 (Used in a strut, basically rigid) appears on 45 US grants and 38 published applications in this corpus.
Search patents in F16F- Granted patents
- 45
- Published applications
- 38
- Assignees
- 42
- Inventors
- 131
- Latest grant
- 17 Feb 2026
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 1982 | 1 | 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 | 2 | 0 |
| 1994 | 2 | 0 |
| 1995 | 0 | 0 |
| 1996 | 1 | 0 |
| 1997 | 2 | 0 |
| 1998 | 1 | 0 |
| 1999 | 1 | 0 |
| 2000 | 1 | 0 |
| 2001 | 6 | 2 |
| 2002 | 0 | 0 |
| 2003 | 0 | 1 |
| 2004 | 1 | 0 |
| 2005 | 0 | 4 |
| 2006 | 1 | 0 |
| 2007 | 3 | 1 |
| 2008 | 0 | 0 |
| 2009 | 0 | 0 |
| 2010 | 0 | 2 |
| 2011 | 1 | 0 |
| 2012 | 1 | 1 |
| 2013 | 0 | 1 |
| 2014 | 0 | 1 |
| 2015 | 2 | 1 |
| 2016 | 2 | 2 |
| 2017 | 0 | 2 |
| 2018 | 1 | 5 |
| 2019 | 5 | 4 |
| 2020 | 2 | 1 |
| 2021 | 1 | 2 |
| 2022 | 1 | 2 |
| 2023 | 1 | 0 |
| 2024 | 2 | 2 |
| 2025 | 2 | 2 |
| 2026 | 2 | 2 |
By publication year. Applications have been published since 2001. 2026 runs to 8 Oct.
Recent patents
- Shock strut variable-area metering unit17 Feb 2026US 12,552,522 B2Goodrich Corporation
- Variable diameter thrust link apparatus20 Jan 2026US 12,529,323 B2General Electric Company
- Temperature compensated landing gear shock strut6 May 2025US 12,291,325 B2Goodrich Corporation
- Vibration isolator with overload protection4 Feb 2025US 12,215,752 B1Blue Canyon Technologies Inc.
- Power strut with different rotational friction torque3 Sep 2024US 12,078,004 B2Magna Automotive Parts (Suzhou) Co., Ltd.
- Vibration of shock struts of an aircraft to relieve a portion of static friction forces acting on the shock struts before determination of aircraft weight and balance1 Oct 2026US 2026/0298757 A1The Boeing Company
- Variable diameter thrust link apparatus21 May 2026US 2026/0139609 A1General Electric Company
- Variable diameter thrust link apparatus27 Mar 2025US 2025/0101881 A1General Electric Company
- Temperature compensated landing gear shock strut23 Jan 2025US 2025/0026471 A1Goodrich Corporation
- Shock strut variable-area metering unit26 Sep 2024US 2024/0317392 A1Goodrich Corporation
Most cited
By later US patents
- Rear suspension with semi-active toe force compliance control48US 7,984,915 B2Honda Motor Co., Ltd. · 2011
- Method and device for filtering the vibratory excitations transmitted between two parts especially between the rotor and the fuselage of a helicopter44US 5,316,240 AAerospatiale Societe Nationale Industrielle · 1994
- Variable stiffness positioning link for a gearbox37US 6,212,974 B1United Technologies Corporation · 2001
- Multi-linkage suspension system including outboard isolators37US 6,328,293 B1Lord Corporation · 2001
- Force (torque) nulling inertially servoed structural interface35US 5,327,061 AHughes Aircraft Company · 1994