B64C 1/12
Construction or attachment of skin panels
B64C1/12 (Construction or attachment of skin panels) appears on 857 US grants and 881 published applications in this corpus.
Search patents in B64C- Granted patents
- 857
- Published applications
- 881
- Assignees
- 210
- Inventors
- 1,753
- Latest grant
- 15 Sep 2026
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 1976 | 2 | 0 |
| 1977 | 3 | 0 |
| 1978 | 0 | 0 |
| 1979 | 0 | 0 |
| 1980 | 1 | 0 |
| 1981 | 4 | 0 |
| 1982 | 3 | 0 |
| 1983 | 2 | 0 |
| 1984 | 1 | 0 |
| 1985 | 7 | 0 |
| 1986 | 1 | 0 |
| 1987 | 2 | 0 |
| 1988 | 3 | 0 |
| 1989 | 4 | 0 |
| 1990 | 6 | 0 |
| 1991 | 4 | 0 |
| 1992 | 4 | 0 |
| 1993 | 4 | 0 |
| 1994 | 3 | 0 |
| 1995 | 2 | 0 |
| 1996 | 6 | 0 |
| 1997 | 5 | 0 |
| 1998 | 8 | 0 |
| 1999 | 7 | 0 |
| 2000 | 5 | 0 |
| 2001 | 8 | 3 |
| 2002 | 9 | 9 |
| 2003 | 12 | 8 |
| 2004 | 12 | 9 |
| 2005 | 6 | 18 |
| 2006 | 9 | 16 |
| 2007 | 5 | 10 |
| 2008 | 6 | 28 |
| 2009 | 7 | 34 |
| 2010 | 22 | 38 |
| 2011 | 24 | 23 |
| 2012 | 28 | 35 |
| 2013 | 29 | 35 |
| 2014 | 33 | 37 |
| 2015 | 35 | 55 |
| 2016 | 39 | 47 |
| 2017 | 49 | 61 |
| 2018 | 49 | 66 |
| 2019 | 53 | 78 |
| 2020 | 77 | 54 |
| 2021 | 50 | 69 |
| 2022 | 71 | 36 |
| 2023 | 45 | 36 |
| 2024 | 40 | 24 |
| 2025 | 33 | 31 |
| 2026 | 19 | 21 |
By publication year. Applications have been published since 2001. 2026 runs to 8 Oct.
Recent patents
- Method and apparatus for bonding stringers to a fuselage skin15 Sep 2026US 12,734,764 B2The Boeing Company
- Panel systems and methods for helicopters8 Sep 2026US 12,728,978 B2North West Heli-Structures Incorporated
- Methods of shimming an assembly1 Sep 2026US 12,722,769 B23M Innovative Properties Company
- Aircraft panel18 Aug 2026US 12,709,378 B2Airbus Operations GmbH
- Composite fuselage barrel with improved EME protection and method of making thereof21 Jul 2026US 12,686,485 B2The Boeing Company
- Continuous Aircraft Structure24 Sep 2026US 2026/0285470 A1
- Unmanned aerial vehicles having a skeleton and outer shell17 Sep 2026US 2026/0274393 A1AEVEX Aerospace, LLC
- Aircraft with carbon fiber material and a method of manufacture10 Sep 2026US 2026/0264836 A1JetZero, Inc.
- Shim layer with seal groove3 Sep 2026US 2026/0257807 A1The Boeing Company
- Ramped composite structural member for aircraft, and method of forming the same27 Aug 2026US 2026/0249976 A1Airbus Operations GmbH
Most cited
By later US patents
- Caul and method for bonding and curing intricate composite structures196US 5,242,523 AThe Boeing Company · 1993
- Titanium-polymer hybrid laminates126US 6,114,050 AThe Boeing Company · 2000
- Method for fastening aircraft frame elements to sandwich skin panels covering same using woven fiber connectors120US 4,671,470 ABeech Aircraft Corporation · 1987
- Manufacturing of components of a vehicle using additive layer manufacturing119US 10,442,002 B2Airbus Operations GmbH · 2019
- Geodesic structure forming systems and methods117US 9,789,548 B2The Boeing Company · 2017