B64D 27/14
Within, or attached to, fuselages
Official title: within, or attached to, fuselages
B64D27/14 (Within, or attached to, fuselages) appears on 230 US grants and 276 published applications in this corpus.
Search patents in B64D- Granted patents
- 230
- Published applications
- 276
- Assignees
- 72
- Inventors
- 445
- Latest grant
- 15 Sep 2026
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 1977 | 1 | 0 |
| 1978 | 0 | 0 |
| 1979 | 0 | 0 |
| 1980 | 0 | 0 |
| 1981 | 0 | 0 |
| 1982 | 0 | 0 |
| 1983 | 0 | 0 |
| 1984 | 0 | 0 |
| 1985 | 2 | 0 |
| 1986 | 1 | 0 |
| 1987 | 0 | 0 |
| 1988 | 0 | 0 |
| 1989 | 2 | 0 |
| 1990 | 2 | 0 |
| 1991 | 2 | 0 |
| 1992 | 1 | 0 |
| 1993 | 0 | 0 |
| 1994 | 0 | 0 |
| 1995 | 0 | 0 |
| 1996 | 0 | 0 |
| 1997 | 0 | 0 |
| 1998 | 0 | 0 |
| 1999 | 0 | 0 |
| 2000 | 1 | 0 |
| 2001 | 1 | 1 |
| 2002 | 0 | 1 |
| 2003 | 1 | 0 |
| 2004 | 0 | 1 |
| 2005 | 0 | 0 |
| 2006 | 1 | 1 |
| 2007 | 0 | 1 |
| 2008 | 0 | 5 |
| 2009 | 3 | 6 |
| 2010 | 2 | 3 |
| 2011 | 4 | 14 |
| 2012 | 4 | 6 |
| 2013 | 13 | 7 |
| 2014 | 9 | 13 |
| 2015 | 6 | 11 |
| 2016 | 8 | 11 |
| 2017 | 14 | 21 |
| 2018 | 13 | 36 |
| 2019 | 16 | 17 |
| 2020 | 20 | 31 |
| 2021 | 23 | 20 |
| 2022 | 24 | 10 |
| 2023 | 15 | 17 |
| 2024 | 16 | 12 |
| 2025 | 12 | 13 |
| 2026 | 13 | 18 |
By publication year. Applications have been published since 2001. 2026 runs to 8 Oct.
Recent patents
- Aircraft design and technology15 Sep 2026US 12,735,168 B2Sierra Nevada Corporation
- Exhaust duct1 Sep 2026US 12,722,793 B2BAE SYSTEMS plc
- Hybrid electric aircraft with gyroscopic stabilization control18 Aug 2026US 12,709,388 B2GE Avio S. r. l.
- Aircraft propulsion system with core flowpath inlet forward of fan rotor2 Jun 2026US 12,643,669 B1Rtx Corporation
- Aircraft with boundary layer ingestion device having center position between center position of fuselage and center position of rear end portion of fuselage12 May 2026US 12,623,786 B2Japan Aerospace Exploration Agency
- Aircraft design and technology6 Aug 2026US 2026/0225706 A1Freedom Aircraft Ventures LLC
- Cross debris protection for open rotor propulsion system(s)6 Aug 2026US 2026/0225721 A1Rtx Corporation
- Method and system for assisting with the piloting of a rotary wing aircraft in a fuel economy mode30 Jul 2026US 2026/0217376 A1Safran Helicopter Engines
- Mount system for reverse core engine23 Jul 2026US 2026/0210292 A1Rtx Corporation
- Blended wing aircraft16 Jul 2026US 2026/0200577 A1General Electric Company
Most cited
By later US patents
- Ultra-efficient propulsor with an augmentor fan circumscribing a turbofan98US 8,689,538 B2The Boeing Company · 2014
- Thermal anti-icing system for aircraft82US 5,011,098 AThe Boeing Company · 1991
- Unconventional integrated propulsion systems and methods for blended wing body aircraft77US 7,665,689 B2The Boeing Company · 2010
- Vibration damping aircraft engine attachment64US 5,065,959 AThe Boeing Company · 1991
- Vibration isolating engine mount46US 4,821,980 AThe Boeing Company · 1989