B64C 9/26
By multiple flaps
Official title: by multiple flaps
B64C9/26 (By multiple flaps) appears on 46 US grants and 45 published applications in this corpus.
Search patents in B64C- Granted patents
- 46
- Published applications
- 45
- Assignees
- 19
- Inventors
- 75
- Latest grant
- 16 Jun 2026
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 1976 | 1 | 0 |
| 1977 | 0 | 0 |
| 1978 | 0 | 0 |
| 1979 | 0 | 0 |
| 1980 | 0 | 0 |
| 1981 | 1 | 0 |
| 1982 | 0 | 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 | 1 | 0 |
| 1994 | 0 | 0 |
| 1995 | 0 | 0 |
| 1996 | 0 | 0 |
| 1997 | 0 | 0 |
| 1998 | 0 | 0 |
| 1999 | 0 | 0 |
| 2000 | 1 | 0 |
| 2001 | 1 | 0 |
| 2002 | 0 | 1 |
| 2003 | 0 | 0 |
| 2004 | 1 | 0 |
| 2005 | 0 | 0 |
| 2006 | 0 | 1 |
| 2007 | 0 | 0 |
| 2008 | 1 | 0 |
| 2009 | 0 | 0 |
| 2010 | 0 | 0 |
| 2011 | 0 | 3 |
| 2012 | 0 | 1 |
| 2013 | 2 | 0 |
| 2014 | 2 | 1 |
| 2015 | 1 | 0 |
| 2016 | 1 | 1 |
| 2017 | 0 | 1 |
| 2018 | 0 | 2 |
| 2019 | 0 | 3 |
| 2020 | 5 | 7 |
| 2021 | 4 | 3 |
| 2022 | 6 | 6 |
| 2023 | 6 | 2 |
| 2024 | 6 | 9 |
| 2025 | 5 | 0 |
| 2026 | 1 | 4 |
By publication year. Applications have been published since 2001. 2026 runs to 8 Oct.
Recent patents
- Monitoring adaptable segments of an airfoil16 Jun 2026US 12,654,875 B2Airbus Operations GmbH
- Aerial vehicles, cooperative flying systems, and methods of operating the same21 Oct 2025US 12,448,124 B2The Boeing Company
- Wing for an aircraft including a high lift body track with roller unit14 Oct 2025US 12,441,459 B2Airbus Operations GmbH
- Flight control surface with leading edge device within wing12 Aug 2025US 12,384,518 B2Airbus Operations GmbH
- Aerodynamic system for an aircraft29 Jul 2025US 12,371,148 B2Airbus Operations GmbH
- Flying object and control method therefor1 Oct 2026US 2026/0296642 A1Honda Motor Co., Ltd.
- High lift arrangement for an aircraft wing20 Aug 2026US 2026/0242052 A1Airbus Operations GmbH
- Control surface movement mechanism2 Jul 2026US 2026/0184420 A1Tusas- Turk Havacilik Ve Uzay Sanayii Anonim Sirketi
- Support assembly for a high lift body, high lift body arrangement, as well as wing and aircraft comprising same23 Apr 2026US 2026/0109449 A1Airbus Operations GmbH
- Aerodynamic system for an aircraft17 Oct 2024US 2024/0343382 A1Airbus Operations GmbH
Most cited
By later US patents
- Leading edge vortex flap for wings65US 4,293,110 AThe Boeing Company · 1981
- Actuating system for wing leading-edge slats47US 3,949,957 ASociete Nationale Industrielle Aerospatiale · 1976
- Single surface independent aircraft control38US 6,227,498 B1Northrop Grumman Corporation · 2001
- Systems and methods for aircraft lift enhancement30US 11,305,869 B1Wayfarer Aircraft Research and Development Inc. · 2022
- Variable camber continuous aerodynamic control surfaces and methods for active wing shaping control25US 9,227,721 B1The United States of America as Represented by the Administrator of the National Aeronautics & Space Administration (NASA) · 2016