B64C 2009/143
Comprising independently adjustable elements for closing or opening the slot between the
Official title: {comprising independently adjustable elements for closing or opening the slot between the main wing and leading or trailing edge flaps}
B64C2009/143 (Comprising independently adjustable elements for closing or opening the slot between the) appears on 62 US grants and 64 published applications in this corpus.
Search patents in B64C- Granted patents
- 62
- Published applications
- 64
- Assignees
- 24
- Inventors
- 118
- Latest grant
- 16 Jun 2026
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 1989 | 1 | 0 |
| 1990 | 0 | 0 |
| 1991 | 0 | 0 |
| 1992 | 0 | 0 |
| 1993 | 0 | 0 |
| 1994 | 0 | 0 |
| 1995 | 0 | 0 |
| 1996 | 0 | 0 |
| 1997 | 0 | 0 |
| 1998 | 0 | 0 |
| 1999 | 0 | 0 |
| 2000 | 0 | 0 |
| 2001 | 0 | 0 |
| 2002 | 0 | 0 |
| 2003 | 0 | 0 |
| 2004 | 0 | 0 |
| 2005 | 0 | 1 |
| 2006 | 1 | 1 |
| 2007 | 1 | 3 |
| 2008 | 1 | 2 |
| 2009 | 2 | 2 |
| 2010 | 3 | 6 |
| 2011 | 2 | 5 |
| 2012 | 2 | 6 |
| 2013 | 6 | 3 |
| 2014 | 5 | 2 |
| 2015 | 6 | 3 |
| 2016 | 1 | 1 |
| 2017 | 4 | 6 |
| 2018 | 2 | 1 |
| 2019 | 1 | 3 |
| 2020 | 4 | 4 |
| 2021 | 3 | 1 |
| 2022 | 3 | 4 |
| 2023 | 4 | 3 |
| 2024 | 4 | 4 |
| 2025 | 5 | 3 |
| 2026 | 1 | 0 |
By publication year. Applications have been published since 2001. 2026 runs to 8 Oct.
Recent patents
- Wing for an aircraft16 Jun 2026US 12,654,841 B2Airbus Operations GmbH
- Leading-edge droop actuation system2 Dec 2025US 12,486,020 B2The Boeing Company
- Wing assemblies and aircraft with gap-adjustment assemblies for slats14 Oct 2025US 12,441,455 B1The Boeing Company
- Rotary EMA1 Jul 2025US 12,345,323 B2Goodrich Actuation Systems Limited
- Wing for an aircraft29 Apr 2025US 12,286,229 B2Airbus Operations GmbH
- Leading-edge droop actuation system12 Jun 2025US 2025/0187718 A1The Boeing Company
- Rotary ema24 Apr 2025US 2025/0129843 A1Goodrich Actuation Systems Limited
- Single Flap Drive System For Decentralized Flap Architectures16 Jan 2025US 2025/0019067 A1Airbus Operations GmbH
- Control device for an aircraft19 Dec 2024US 2024/0417065 A1Airbus Operations GmbH
- Wing for an aircraft30 May 2024US 2024/0174346 A1Airbus Operations GmbH
Most cited
By later US patents
- Method and spoiler system for ensuring the aerodynamic continuity of the upper surface of an aircraft36US 6,981,676 B2Airbus France · 2006
- Seal assemblies for use with drooped spoilers and other control surfaces on aircraft24US 7,611,099 B2The Boeing Company · 2009
- Aerospace vehicle leading edge slat devices and corresponding methods22US 7,322,547 B2The Boeing Company · 2008
- System for reducing aerodynamic noise at a supplementary wing of an aircraft22US 7,766,281 B2Airbus Deutschland GmbH · 2010
- Wing flap operation18US 4,834,326 AMBB GmbH · 1989