B64C 1/062
Specially adapted to absorb crash loads
Official title: {specially adapted to absorb crash loads}
B64C1/062 (Specially adapted to absorb crash loads) appears on 105 US grants and 114 published applications in this corpus.
Search patents in B64C- Granted patents
- 105
- Published applications
- 114
- Assignees
- 50
- Inventors
- 249
- Latest grant
- 6 Oct 2026
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 1986 | 1 | 0 |
| 1987 | 1 | 0 |
| 1988 | 0 | 0 |
| 1989 | 0 | 0 |
| 1990 | 0 | 0 |
| 1991 | 1 | 0 |
| 1992 | 0 | 0 |
| 1993 | 0 | 0 |
| 1994 | 0 | 0 |
| 1995 | 1 | 0 |
| 1996 | 1 | 0 |
| 1997 | 0 | 0 |
| 1998 | 0 | 0 |
| 1999 | 0 | 0 |
| 2000 | 1 | 0 |
| 2001 | 0 | 1 |
| 2002 | 1 | 0 |
| 2003 | 1 | 0 |
| 2004 | 0 | 3 |
| 2005 | 2 | 6 |
| 2006 | 1 | 3 |
| 2007 | 2 | 3 |
| 2008 | 2 | 7 |
| 2009 | 1 | 4 |
| 2010 | 3 | 8 |
| 2011 | 7 | 8 |
| 2012 | 6 | 3 |
| 2013 | 4 | 8 |
| 2014 | 7 | 3 |
| 2015 | 6 | 11 |
| 2016 | 7 | 4 |
| 2017 | 9 | 4 |
| 2018 | 4 | 6 |
| 2019 | 3 | 5 |
| 2020 | 5 | 3 |
| 2021 | 3 | 0 |
| 2022 | 3 | 4 |
| 2023 | 3 | 3 |
| 2024 | 4 | 10 |
| 2025 | 11 | 5 |
| 2026 | 4 | 2 |
By publication year. Applications have been published since 2001. 2026 runs to 8 Oct.
Recent patents
- Aircraft fuselage section6 Oct 2026US 12,752,903 B2Airbus Operations S.L.U.
- Structural shape mode influencers28 Jul 2026US 12,691,991 B2The Boeing Company
- Detachable battery structure of fuselage3 Feb 2026US 12,542,325 B2Hyundai Motor Company
- Fuselage sub-floor structure with aircraft components having corrugated C-channel27 Jan 2026US 12,534,176 B1Civil Aviation University of China
- Collision load distribution structure of fuselage2 Sep 2025US 12,404,027 B2Hyundai Motor Company
- Protection for an aircraft fuselage18 Jun 2026US 2026/0167316 A1
- Devices and methods for controlled mechanical failure and secondary impact damage mitigation28 May 2026US 2026/0145772 A1Textron Innovations Inc.
- Aircraft fuselage section26 Jun 2025US 2025/0206433 A1Airbus Operations S.L.U.
- Device for absorbing energy by compression, aircraft comprising at least one such device19 Jun 2025US 2025/0196988 A1Airbus Operations GmbH
- Aircraft comprising at least one removable device for absorbing energy by compression19 Jun 2025US 2025/0196989 A1Airbus Operations GmbH
Most cited
By later US patents
- Multi-deck passenger aircraft having impact energy absorbing structures65US 5,542,626 ADeutsche Aerospace Airbus GmbH · 1996
- Composite cruciform structure for joining intersecting structural members of an airframe and the like63US 4,715,560 ALear Fan Corp. · 1987
- Landing assist apparatus interface bulkhead and method of installation62US 7,344,108 B2The Boeing Company · 2008
- Energy absorbing composite aircraft structure56US 4,593,870 ABell Helicopter Textron Inc. · 1986
- Subfloor structure of an aircraft airframe44US 6,427,945 B1Eurocopter Deutschland GmbH · 2002