Morphing Wing Patents: Top Companies, Trends & White Space 2026
- Half the field sits with a handful of filers. the top 5 assignees combined account for 50.0% of all 124 records in scope, with a long tail of single- and few-filing entrants behind them.
- Filing peaked in 2020 at 29 records and has since cooled. the most recent complete comparison, 2021 to 2024, shows a 33% decline, though 2025 onward is still filling in due to publication lag.
- Claim density is overwhelmingly airframe-specific. B64C (aeroplanes & helicopters) covers 83.1% of records, while adjacent classes like drones (3.2%) and plastics shaping (2.4%) remain comparatively open.
Filing growth compares 2021 (3 records) with 2024 (2) — a three-year span. 2024 is the most recent year we treat as complete: publication lags filing by roughly 18 months, so 2025 onwards are still filling in and any growth rate that ends there would understate the field. Top-5 share is the combined record count of the five largest assignees divided by all 124 records in scope (CR5), not by the ranked leaders only.
What morphing wing patents actually cover
Morphing and adaptive wing structures describe airfoils and control surfaces that change shape in flight rather than relying on discrete hinged surfaces. The patent record in scope spans shape memory actuation, flexible and elastomeric skins, spanwise morphing spars and ribs, and variable camber trailing edges, with filings concentrated in aerospace structural classes but reaching into wind turbine blades and even burner and semiconductor art where flexible-skin or actuator claims overlap. Publication lags filing by roughly 18 months, so any read of the last one to two years understates real filing activity.
The dataset covers 124 published records filed or published between 2015 and mid-2026, drawn from a search string built around morphing wing, variable camber wing and morphing trailing edge terms paired with shape memory actuator, flexible skin, spanwise morphing, elastomeric skin and skin fatigue life concepts. Receiving-office activity is led by the United States, followed by Europe, China, Germany and the WIPO PCT route, indicating this is a field prosecuted internationally rather than in a single jurisdiction.
Let an AI agent run this analysis on your own technology
Pick a task. Every answer cites the patents behind it.
Filing trend and technology composition
Two views of the same 124-record dataset: the year-by-year filing trend, and how records distribute across IPC subclasses. Because a single record can carry more than one IPC class, the class shares below sum to more than 100% of the record total.
Filings rose to a 2020 peak, then eased back
Annual filings climbed from 5 records in 2017 to a peak of 29 in 2020. The most recent complete year-over-year comparison available, 2021 (3 records) against 2024 (2 records), shows a 33% decline over that three-year span. Years from 2025 onward are still filling in as publications catch up to filing dates, so they should not be read as a continued drop.
B64C dominates; adjacent classes stay thin
B64C (aeroplanes & helicopters) appears in 83.1% of the 124 records, confirming this is fundamentally an airframe technology. Wind motors (F03D, 8.1%), turbines (F01D, 6.5%) and solid-state devices (H10N, 6.5%) show the actuation and skin concepts crossing into adjacent machinery, while drones (B64U, 3.2%), semiconductors (H01L, 3.2%) and plastics shaping (B29C, 2.4%) remain comparatively under-filed relative to the core class.
Shares are the percentage of the 124 records in scope. A patent can carry several IPC classes, so the shares add up to more than 100%.
Go deeper on Morphing and Adaptive Wing Structures with Eureka
This page is one run against one query. Ask Eureka your own question about morphing and adaptive wing structures and every answer comes back with the patent numbers behind it.
Try EurekaThe most-cited records anchoring this field
EP2955102B1 — Morphing trailing-edge device for an airfoil
Filed by Airbus Operations GmbH and granted with a priority date of 2019-03-27, this record describes a morphing trailing-edge device for a wing airfoil, sitting squarely in the variable camber and trailing-edge deflection core of this dataset.Abstract summarised from the published record; see the full filing for claim scope.


| # | Publication no. | Patent title | Citations |
|---|---|---|---|
| 1 | US4650140A | Wind edge movable airfoil having variable camber | 156 |
| 2 | US3941334A | Variable camber airfoil | 121 |
| 3 | US3994451A | Variable camber airfoil | 117 |
| 4 | US20060118675A1 | Transformable fluid foil with pivoting spars and ribs | 74 |
| 5 | US6045096A | Variable camber airfoil | 74 |
| 6 | US4053124A | Variable camber airfoil | 74 |
| 7 | US20060144992A1 | Transformable fluid foil with pivoting spars | 59 |
| 8 | US3994452A | Variable camber airfoil | 59 |
| 9 | US3361386A | Vertical or short take-off and landing aircraft | 44 |
| 10 | US2650047A | Variable camber wing | 41 |
Citation counts are measured within the searched corpus and skew toward older filings; treat them as a signal of technical influence rather than of current commercial importance.
Each row carries its publication number; clicking a row searches Eureka by that number.
Put your own technology through the same analysis
Eureka on the web
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 →MCP server & REST API
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 →What the numbers mean for a filing decision
Three patterns stand out once the assignee ranking, filing trend and IPC composition are read together.
The top of the field is dense, the tail is long
The top 5 assignees account for 50.0% of all 124 records in scope, and the top 10 reach 74.2%. With 54 companies in the full ranking, that leaves a wide tail of entities holding only one or two records each — a sign that core variable-camber and trailing-edge claim space is occupied at the top while narrower implementation variants remain contestable.
Activity has cooled from its 2020 peak
Filings peaked at 29 records in 2020. The last comparison period that can be treated as complete, 2021 to 2024, shows filings falling from 3 to 2 records, a 33% decline. This should be read as a real cooling in that window, not as a signal about 2025 or 2026, which are still incomplete due to publication lag.
Claims cluster in airframe structure, not in adjacent machinery
B64C covers 83.1% of the 124 records, far ahead of any other class. Wind turbine (F03D, 8.1%) and turbine (F01D, 6.5%) crossover exists, but drone-specific (B64U, 3.2%) and plastics-shaping (B29C, 2.4%) claims are comparatively rare, suggesting less-crowded filing routes for those platforms and manufacturing methods.
Eureka can read the same corpus for gaps instead of for coverage: under-claimed branches adjacent to morphing and adaptive wing structures, with the prior art for and against each one.
Assignees shaping the morphing wing field
The ranked assignee list spans 54 companies and research institutions, from large aerospace manufacturers to university research groups, with filing counts concentrated at the top and a long tail of occasional filers.
One assignee holds a clear lead
The top-ranked assignee holds 25 of the 124 records in scope, well ahead of fifth place at 9 records and tenth place at 4. That gap between first and fifth position indicates a genuine leader rather than a tight cluster at the top.
Joint filings are concentrated in one partnership
Nine co-assignee pairs appear in the dataset, with the strongest pairing recurring 9 times — far more than any other combination, which appears only once or twice. This points to a single long-running collaborative filing relationship rather than a broad pattern of joint development across the field.
Established filers show no latest-year activity
Several of the historically most active assignees, including the field's leading filer and multiple university and government research bodies, show zero recorded filings in the latest year. Given the roughly 18-month publication lag, this likely reflects filings still working through the pipeline rather than an actual halt in R&D.
| Assignee | Recent year | YoY |
|---|---|---|
| Bombardier Inc | 0 | — |
| Brunel University | 0 | — |
| Learjet Inc | 0 | — |
| THE RES FOUNDATION FOR THE STATE UNIV OF NEW YORK | 0 | — |
| IP2IPO Innovations Ltd | 0 | — |
| The Government of the United States as represented by the Secretary of the Air Force | 0 | — |
| Technion Research & Development Foundation Ltd | 0 | — |
| The Boeing Co | 0 | — |
Where to take this analysis
The concentration, trend and class data point to specific next questions for R&D and IP teams working in this space.
Map claim scope against the leading filer
With one assignee holding 25 of 124 records, understanding exactly which trailing-edge and camber mechanisms it has claimed is the first step before filing adjacent variants.
Explore assignee claim scope in EurekaCheck the under-claimed branches before drafting
Drone-specific morphing surfaces and elastomeric skin fatigue methods show thinner filing density than the core airframe class, but that can change quickly once one filer moves.
Run a white space search in EurekaTrack post-2024 filings as they publish
Because publication lags filing by about 18 months, the 2025–2026 dip in the trend chart is an artefact of timing, not a real slowdown — worth re-checking as more records land.
Set a filing alert in EurekaCommon questions on morphing wing patents
The assignee ranking in this dataset covers 54 companies and institutions across 124 records, with the leading assignee alone holding 25 records. The top 5 assignees together account for 50.0% of all records in scope, and the top 10 reach 74.2%, so filing activity is concentrated among a small group of aerospace manufacturers and research institutions rather than spread evenly. Beyond that group, most other entities appear with only one or two filings each, forming a long tail of occasional contributors.
Filings rose steadily through the late 2010s and peaked at 29 records in 2020. Comparing 2021 (3 records) to 2024 (2 records), the last window that can be treated as complete, filings fell by 33%. Data from 2025 onward is still incomplete because publication typically lags filing by about 18 months, so it is too early to call the current trajectory a continued decline.
The overwhelming majority, 83.1% of the 124 records, fall under IPC class B64C, which covers aeroplanes and helicopters, confirming this is primarily an airframe structures technology. Smaller shares extend into wind motors, turbines and solid-state devices, reflecting actuator and flexible-skin concepts shared with other machinery. Because a single record can carry multiple IPC codes, these shares add up to more than 100% of the record total and should not be summed as if they were mutually exclusive categories.
EP2955102B1, filed by Airbus Operations GmbH with a priority date of 2019-03-27, describes a morphing trailing-edge device for a wing airfoil. It sits within the core variable-camber and trailing-edge deflection claim space that this dataset shows is already densely filed by the leading assignees. Anyone designing a competing trailing-edge mechanism should review its specific claim language directly, since a patent landscape summary like this one can indicate where claim density sits but cannot substitute for a freedom-to-operate review of the granted claims.
The class composition data points to several thinner branches relative to the dominant B64C aerospace class: drone-specific variable camber surfaces sit at only 3.2% of records, and flexible-skin manufacturing via plastics shaping methods at 2.4%. These lower shares suggest less-crowded filing routes for platforms and manufacturing processes outside the traditional fixed-wing aircraft context. That said, thin coverage today can close quickly once an established filer moves into the space, so any white-space assessment should be paired with a current freedom-to-operate check before drafting.
Research Morphing and Adaptive Wing Structures in depth with Eureka
Go past this page: query the whole morphing and adaptive wing structures corpus yourself, in your own scope.
Every answer comes back with patent numbers you can open.
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.