B64C 1/38
Constructions adapted to reduce effects of aerodynamic or other external heating
B64C1/38 (Constructions adapted to reduce effects of aerodynamic or other external heating) appears on 160 US grants and 142 published applications in this corpus.
Search patents in B64C- Granted patents
- 160
- Published applications
- 142
- Assignees
- 87
- Inventors
- 381
- Latest grant
- 15 Sep 2026
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 1977 | 2 | 0 |
| 1978 | 0 | 0 |
| 1979 | 0 | 0 |
| 1980 | 0 | 0 |
| 1981 | 1 | 0 |
| 1982 | 1 | 0 |
| 1983 | 0 | 0 |
| 1984 | 1 | 0 |
| 1985 | 0 | 0 |
| 1986 | 0 | 0 |
| 1987 | 3 | 0 |
| 1988 | 3 | 0 |
| 1989 | 3 | 0 |
| 1990 | 7 | 0 |
| 1991 | 8 | 0 |
| 1992 | 4 | 0 |
| 1993 | 3 | 0 |
| 1994 | 5 | 0 |
| 1995 | 2 | 0 |
| 1996 | 2 | 0 |
| 1997 | 2 | 0 |
| 1998 | 0 | 0 |
| 1999 | 1 | 0 |
| 2000 | 1 | 0 |
| 2001 | 0 | 0 |
| 2002 | 1 | 3 |
| 2003 | 0 | 1 |
| 2004 | 2 | 5 |
| 2005 | 4 | 2 |
| 2006 | 3 | 2 |
| 2007 | 2 | 2 |
| 2008 | 0 | 2 |
| 2009 | 0 | 1 |
| 2010 | 2 | 4 |
| 2011 | 2 | 5 |
| 2012 | 2 | 2 |
| 2013 | 2 | 1 |
| 2014 | 6 | 4 |
| 2015 | 2 | 7 |
| 2016 | 6 | 9 |
| 2017 | 3 | 7 |
| 2018 | 4 | 6 |
| 2019 | 8 | 8 |
| 2020 | 5 | 10 |
| 2021 | 5 | 22 |
| 2022 | 19 | 14 |
| 2023 | 9 | 7 |
| 2024 | 13 | 5 |
| 2025 | 4 | 8 |
| 2026 | 7 | 5 |
By publication year. Applications have been published since 2001. 2026 runs to 8 Oct.
Recent patents
- Vehicle having a body with a nose section15 Sep 2026US 12,735,170 B2General Electric Company
- Intelligent temperature control lattice structure based on 4D printing and application thereof1 Sep 2026US 12,722,203 B2Shenyang Research Institute of Foundry Co., Ltd. Cam
- Nose-tip assembly for hypersonic and high-speed vehicles1 Sep 2026US 12,722,768 B1The Boeing Company
- Flutter wind tunnel test model and method of producing flutter wind tunnel test model16 Jun 2026US 12,656,212 B2Subaru Corporation
- Method and system for reducing a temperature differential across a flight vehicle31 Mar 2026US 12,589,872 B2The Boeing Company
- Method and system for reducing a temperature differential across a flight vehicle16 Jul 2026US 2026/0200576 A1The Boeing Company
- Intelligent temperature control lattice structure based on 4d printing and application thereof26 Mar 2026US 2026/0084213 A1Shenyang Research Institute of Foundry Co., Ltd. Cam
- Nose tip structures for flight vehicles26 Mar 2026US 2026/0084799 A1Raytheon Company
- Automated tape layering for a composite19 Mar 2026US 2026/0077565 A1Textron Systems Corporation
- Gradient mitigating heating system29 Jan 2026US 2026/0032787 A1Raytheon Company
Most cited
By later US patents
- Modular liquid skin heat exchanger71US 5,667,168 AE-Systems, Inc. · 1997
- Cooling system for a hypersonic aircraft69US 5,149,018 AThe Boeing Company · 1992
- Multiwall thermal protection system60US 4,344,591 AThe United States of America asrepresented by the Administrator of the National Aeronautics and Space Administration · 1982
- Solar energy absorbing article and method of making same50US 4,002,541 ADesign Systems, Inc. · 1977
- Thermal insulation structure45US 4,849,276 AThe Boeing Company · 1989