G01M 5/0016
Investigating the elasticity of structures: of aircraft wings or blades
Official title: {of aircraft wings or blades}
G01M5/0016 (Investigating the elasticity of structures: of aircraft wings or blades) appears on 339 US grants and 406 published applications in this corpus.
Search patents in G01M- Granted patents
- 339
- Published applications
- 406
- Assignees
- 179
- Inventors
- 985
- Latest grant
- 21 Jul 2026
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 1979 | 1 | 0 |
| 1980 | 0 | 0 |
| 1981 | 0 | 0 |
| 1982 | 1 | 0 |
| 1983 | 1 | 0 |
| 1984 | 3 | 0 |
| 1985 | 0 | 0 |
| 1986 | 0 | 0 |
| 1987 | 0 | 0 |
| 1988 | 0 | 0 |
| 1989 | 1 | 0 |
| 1990 | 0 | 0 |
| 1991 | 1 | 0 |
| 1992 | 1 | 0 |
| 1993 | 2 | 0 |
| 1994 | 0 | 0 |
| 1995 | 3 | 0 |
| 1996 | 2 | 0 |
| 1997 | 0 | 0 |
| 1998 | 3 | 0 |
| 1999 | 2 | 0 |
| 2000 | 0 | 0 |
| 2001 | 2 | 1 |
| 2002 | 3 | 1 |
| 2003 | 2 | 3 |
| 2004 | 2 | 2 |
| 2005 | 2 | 1 |
| 2006 | 3 | 0 |
| 2007 | 1 | 4 |
| 2008 | 3 | 7 |
| 2009 | 2 | 3 |
| 2010 | 6 | 15 |
| 2011 | 2 | 14 |
| 2012 | 7 | 14 |
| 2013 | 18 | 23 |
| 2014 | 16 | 18 |
| 2015 | 10 | 19 |
| 2016 | 23 | 24 |
| 2017 | 15 | 40 |
| 2018 | 29 | 33 |
| 2019 | 26 | 25 |
| 2020 | 31 | 33 |
| 2021 | 16 | 23 |
| 2022 | 16 | 25 |
| 2023 | 30 | 26 |
| 2024 | 19 | 22 |
| 2025 | 22 | 16 |
| 2026 | 12 | 14 |
By publication year. Applications have been published since 2001. 2026 runs to 8 Oct.
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Most cited
By later US patents
- System for assessing the integrity of structural systems152US 4,480,480 AScott Science & Technology, Inc. · 1984
- Systems and methods for evaluating component strain123US 9,879,981 B1General Electric Company · 2018
- Diagnostic layer and methods for detecting structural integrity of composite and metallic materials121US 6,370,964 B1The Board of Trustees of the Leland Stanford Junior University · 2002
- Systems and methods for monitoring components119US 9,846,933 B2General Electric Company · 2017
- Non-destructive inspection, testing and evaluation systems for intact aircraft and components and method therefore105US 6,637,266 B12003