B64C 3/48
By relatively-movable parts of wing structures
Official title: by relatively-movable parts of wing structures
B64C3/48 (By relatively-movable parts of wing structures) appears on 260 US grants and 194 published applications in this corpus.
Search patents in B64C- Granted patents
- 260
- Published applications
- 194
- Assignees
- 104
- Inventors
- 489
- Latest grant
- 22 Sep 2026
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 1976 | 6 | 0 |
| 1977 | 3 | 0 |
| 1978 | 3 | 0 |
| 1979 | 1 | 0 |
| 1980 | 3 | 0 |
| 1981 | 5 | 0 |
| 1982 | 4 | 0 |
| 1983 | 0 | 0 |
| 1984 | 5 | 0 |
| 1985 | 1 | 0 |
| 1986 | 0 | 0 |
| 1987 | 1 | 0 |
| 1988 | 1 | 0 |
| 1989 | 2 | 0 |
| 1990 | 3 | 0 |
| 1991 | 1 | 0 |
| 1992 | 2 | 0 |
| 1993 | 3 | 0 |
| 1994 | 4 | 0 |
| 1995 | 1 | 0 |
| 1996 | 1 | 0 |
| 1997 | 1 | 0 |
| 1998 | 4 | 0 |
| 1999 | 5 | 0 |
| 2000 | 10 | 0 |
| 2001 | 6 | 0 |
| 2002 | 3 | 3 |
| 2003 | 6 | 1 |
| 2004 | 1 | 2 |
| 2005 | 3 | 5 |
| 2006 | 1 | 11 |
| 2007 | 2 | 3 |
| 2008 | 2 | 5 |
| 2009 | 5 | 4 |
| 2010 | 5 | 12 |
| 2011 | 7 | 8 |
| 2012 | 7 | 7 |
| 2013 | 8 | 8 |
| 2014 | 9 | 6 |
| 2015 | 9 | 11 |
| 2016 | 7 | 18 |
| 2017 | 11 | 7 |
| 2018 | 12 | 9 |
| 2019 | 9 | 11 |
| 2020 | 10 | 5 |
| 2021 | 13 | 14 |
| 2022 | 13 | 12 |
| 2023 | 9 | 8 |
| 2024 | 17 | 14 |
| 2025 | 11 | 4 |
| 2026 | 4 | 6 |
By publication year. Applications have been published since 2001. 2026 runs to 8 Oct.
Recent patents
- Chord line and camber adjusting wing22 Sep 2026US 12,741,735 B1
- Wing for an aircraft25 Aug 2026US 12,715,573 B2Airbus Operations GmbH
- Systems and methods for controlling a variable camber flight control system of an aircraft in a cruise flight phase23 Jun 2026US 12,662,234 B2Bombardier Inc.
- Device comprising an asymmetrical adjustable wing profile24 Feb 2026US 12,560,149 B2
- Skin actuated morphing wing11 Nov 2025US 12,466,540 B1
- Control Method for Aerial Vehicle13 Aug 2026US 2026/0233834 A1University of Washington
- Electrostatically actuated deployable space structures13 Aug 2026US 2026/0238143 A1Massachusetts Institute of Technology
- Rib structure with fishbone imitation enabling shape change in the wing via the method of the rear spar rotation30 Jul 2026US 2026/0217358 A1Eskisehir Teknik Universitesi
- Aircraft high-lift device25 Jun 2026US 2026/0175964 A1Airbus Operations S.L.U.
- Aerodynamic Profile body and associated flying object28 May 2026US 2026/0145775 A1Deutsches Zentrum für Luft- und Raumfahrt e. V.
Most cited
By later US patents
- Digital flexural materials134US 9,566,758 B2Massachusetts Institute of Technology · 2017
- Digital flexural materials118US 10,384,416 B2Massachusetts Institute of Technology · 2019
- Adaptive control surface using antagonistic shape memory alloy tendons103US 5,662,294 ALockheed Martin Corporation · 1997
- Method and apparatus for optimizing the aerodynamic effect of an airfoil89US 5,875,998 ADaimler-Benz Aerospace Airbus GmbH · 1999
- Variable camber airfoil84US 3,994,451 AThe Boeing Company · 1976