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Run your analysis now →A patent landscape on aircraft wing structural health monitoring: filing trends, leading assignees, IPC composition and the claim space still open for new entrants through 2026.
Filing growth = 2021 (3 records) → 2024 (1); 2024 is the last year we treat as complete. Top-5 share = the 5 largest assignees ÷ all 39 records in scope (CR5), not the ranked leaders only.
This landscape draws on 39 published records at the intersection of aircraft or airframe wing structures and structural health monitoring methods — strain sensing, damage or crack detection, and delamination monitoring — filed or published between 2015 and the 2026 data cut-off. The search combines title/abstract language on wing structural health monitoring with IPC classes covering material testing (G01N), structural testing (G01M), and airframe design (B64C), so the set captures both the sensing method and the airframe application, not general SHM claims unrelated to wings.
Because publication lags filing by roughly 18 months, the most recent one to two years in any trend line will always look thinner than the underlying filing activity actually was. Family-level counting is used throughout, which discounts the effect of continuations and multi-jurisdiction refiling by any single applicant.
Two views of the same 39-record set: how filing activity has moved year over year, and which IPC subclasses carry the claim volume.
Filings ran at 2 in 2017 and climbed to a peak of 3 in 2021, the high point of the whole window. From there the documented count fell to 1 by 2024 — a -67% move over that three-year span. Readings for 2025 and 2026 are still incomplete because of publication lag, so this should be read as a plateau after a single peak rather than a confirmed decline.
Publication lags filing by roughly 18 months, so 2025 onwards are still filling in. Growth rates on this page therefore end at 2024; running them to the last bar would understate the field.
G01N (material analysis and testing) appears on 56.4% of the 39 records, well ahead of any other class, with G01L (force and pressure measurement) at 25.6% and G01M (testing machine and structure balance) at 23.1%. B64F, covering ground installations for aircraft, sits at just 12.8% — a sign that most of the documented inventive activity is in the sensing and analysis method rather than in how a monitoring system is installed or serviced on the ground.
Shares are the percentage of the 39 records in scope. A patent can carry several IPC classes, so the shares add up to more than 100%.
This page is one run against one query. Ask Eureka your own question about aircraft wing structural health monitoring patent landscape and every answer comes back with the patent numbers behind it.
Try EurekaA damage sensor for detecting damage within a structure such as aircraft wings or fuselage, or a bridge. The sensor comprises a small piece of triboluminescent material connected via light-guiding fibres or layers to one or more detectors. It may be embedded within the structure or mounted on its surface; impact damage to the triboluminescent material causes light emission that is detected and recorded, with emission intensity usable to gauge damage severity.Filed via PCT (WO97/18451) and granted to QinetiQ in 1999, this remains one of the most-cited records in the set at 36 citations.


| # | Publication no. | Patent title | Citations |
|---|---|---|---|
| 1 | US6076405A | Remote self-powered structure monitor | 113 |
| 2 | US5065630A | Integrated system for aircraft crack detection | 108 |
| 3 | US4026660A | Crack detecting means for rotor blades of rotary wing aircrafts | 55 |
| 4 | US5905260A | Triboluminescent damage sensors | 36 |
| 5 | EP0997714A2 | Remote self-powered structure monitor | 19 |
| 6 | US20160358384A1 | Damage detection and repair system and method using enhanced geolocation | 11 |
| 7 | US20040050164A1 | Non-destructive testing apparatus | 7 |
| 8 | WO2002023165A2 | Apparatus for non-destructively testing material | 5 |
| 9 | WO1997018451A1 | Triboluminescent damage sensors | 5 |
| 10 | CN209656686U | 一种飞机机翼疲劳裂纹检测装置 | 3 |
Ranked by citation count within the searched corpus; older filings accumulate more citations simply by being on file longer, so treat this as a signal of influence rather than of current relevance.
Patent titles are shown in the language they were filed in, not translated, so that each record stays verifiable against the original filing — a translated title will not match in Eureka or in any national register. Each row carries its publication number; clicking a row searches Eureka by that number.
When you want the answer in the next five minutes.
The agent works the prompt against patents and technical literature, citing every source.
Run your analysis now →When it has to run inside your own pipeline.
Patent search, landscape analysis and assignee resolution as MCP tools. Drop them into any agent framework, or call REST directly.
Browse MCP servers →Three findings that shape where a new filer should — and should not — spend claim effort.
Five assignees account for 22 of the 39 records in scope, and the top ten reach 82.1%. That leaves a genuine long tail below rank ten — single-filing universities, individual inventors and smaller suppliers rather than a deep second tier of competitors.
2021 is the high point of the window at three records; by 2024, the last year with reasonably complete data, filings had dropped to one. Given the 18-month publication lag, 2025-2026 figures are not yet reliable enough to call a continued decline.
Material analysis and testing (G01N) is present on well over half of records, while ground-installation infrastructure (B64F) appears on only about one in eight. Vibration and sound-based sensing (G01H) and solid-state device classes (H10N) each sit near a fifth of records, pointing to piezoelectric and acoustic approaches as an active but not yet crowded secondary route.
Eureka can read the same corpus for gaps instead of for coverage: under-claimed branches adjacent to aircraft wing structural health monitoring patent landscape, with the prior art for and against each one.
| Assignee | Co-assignee | Shared families |
|---|---|---|
| University of Warwick | SMITH GORDON | 2 |
| University of Warwick | BATES DANIEL | 2 |
| SMITH GORDON | BATES DANIEL | 2 |
| UK Ministry of Defence | SAGE IAN CHARLES | 1 |
| UK Ministry of Defence | GEDDES NORMAN JAMES | 1 |
Only five co-assignee pairs appear in the dataset, the strongest linking a university with two named individual inventors — evidence that most filings here are made independently rather than through joint development programmes.
The dataset points to specific next steps depending on whether the goal is freedom-to-operate, licensing or new filing strategy.
The five most-cited records, several tied to remote self-powered structure monitoring and early crack-detection systems, define the prior art baseline that any new sensing claim has to clear.
Explore citation network in EurekaB64F coverage is thin relative to the sensing-method classes, suggesting installation, retrofit and ground-service claims around wing SHM systems are comparatively under-claimed.
Run a white space search in EurekaWith 82.1% of records held by the top ten assignees, the remaining filers are mostly single-record entrants — worth monitoring for early signals of new entrants rather than established competitive threats.
Track new entrants in EurekaThe ranked leaders in this 39-record dataset are concentrated at the top: the top five assignees together account for 22 records, or 56.4% of everything in scope, and the leading assignee alone holds seven. Below the top ten, which together reach 82.1%, filing activity thins into a long tail of assignees with one or two records each, including universities and individual inventors. This is a field with a clear leading cluster but no single dominant monopolist.
Filing peaked at three records in 2021, the high point across the 2015-2026 window, and had fallen to one record by 2024 — a -67% change over that three-year span. Because patent publication typically lags actual filing by around 18 months, the apparent low counts in 2025 and 2026 are very likely incomplete rather than evidence of a further decline. The safest read is a single peak year followed by a plateau, not a confirmed downward trend.
The dominant class is G01N, material analysis and testing, present on 56.4% of the 39 records, reflecting how much of the inventive activity sits in sensing and diagnostic method rather than structure. G01L (force and pressure measurement) and G01M (testing machine and structure balance) follow at 25.6% and 23.1%. Airframe-specific classes B64C and B64D, along with vibration-sensing class G01H, each sit around 15-20%, and ground-installation class B64F is the smallest at 12.8%.
US5905260A, QinetiQ's triboluminescent damage sensor patent originally filed via PCT in 1996 and granted in 1999, claims a sensor design using triboluminescent material coupled to detectors via light-guiding fibres or layers, embedded in or mounted on a structure such as an aircraft wing, to detect impact damage through light emission. It is one of the most-cited records in this set at 36 citations. Its claims are specific to that light-emission detection mechanism, so approaches based on strain gauges, fibre Bragg gratings, piezoelectric sensing or acoustic emission are not directly blocked by it, though anyone using triboluminescent materials for damage detection needs to check its claim scope carefully.
The clearest gap by class share is ground-installation and retrofit infrastructure (B64F), covering just 12.8% of the 39 records against 56.4% for core sensing-method claims under G01N. Co-filing is also sparse, with only five co-assignee pairs in the whole dataset, suggesting little joint development activity and room for partnerships between sensor developers and airframers. Given the thin tail below the top ten assignees, there is also room for new entrants to stake out specific sensing modalities, such as combined vibration-and-solid-state approaches (G01H and H10N together sit near 20% each), before the leading cluster extends further into them.
Go past this page: query the whole aircraft wing structural health monitoring patent landscape corpus yourself, in your own scope.
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Disclaimer. This page is generated from Patsnap Eureka data drawn from a limited snapshot of global patent and scientific-literature records, and is provided for general information and reference only.
Patent data carries inherent limitations: recent filings (typically the most recent 18–24 months) are under-counted due to standard publication lag; counts may be reported at either a patent-family or a patent-record basis and are not always directly comparable; classification, applicant-name, and citation data may contain errors, duplicates, or omissions; and the underlying search query defines and constrains the scope shown. As a result, the analysis may be incomplete or inaccurate and may not reflect the full technology landscape.
Nothing on this page constitutes an exhaustive prior-art, novelty, freedom-to-operate, or validity search, nor does it constitute legal, financial, investment, or professional advice, and it should not be relied upon as such. Any patent, commercial, or strategic decision should be verified independently and reviewed with qualified patent, legal, and domain professionals. Patsnap makes no warranties, express or implied, as to the accuracy, completeness, or fitness for any particular purpose of the information presented.
Machine translation. Assignee and organisation names originally recorded in Chinese, Japanese or Korean have been rendered into English by an AI translation step so that the tables stay readable. These renderings are best-effort and may not match a company's registered English name; the original name is what the underlying patent record carries, and it is what any Eureka query launched from this page uses.