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 →Filing growth compares 2021 (13 records) with 2024 (0) — 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 111 records in scope (CR5), not by the ranked leaders only.
Actuator redundancy and force fight control addresses a narrow but consequential engineering problem: when two or more actuators drive the same control surface, small differences in position feedback, load, or timing can cause the actuators to fight each other, wasting energy and stressing the mechanism. The patent record in scope combines dual redundant actuator and actuator control electronics claims with mitigation techniques such as force equalization, load sharing, damping mode switching and cross channel monitoring.
The 111 records in scope run from 2015 through the 2026-07-31 cut-off, concentrated heavily in aerospace flight-control hardware rather than generic motor control, and dominated by a handful of airframe and actuation-system suppliers.
Two views of the same 111 records: how filings have moved year over year, and which IPC subclasses the claims actually sit in.
Filings rose from 7 in 2017 to a peak of 13 in 2021, then fell to 0 by 2024 — a -100% swing over that three-year span. Counts for 2025 and 2026 are not yet representative: publication typically lags filing by around 18 months, so the most recent years will fill in as records publish.
B64C (aeroplanes & helicopters) covers 74.8% of the 111 records, confirming this is fundamentally an airframe control problem rather than a generic actuator one. F15B (fluid-pressure actuators) follows at 27.9%, with G05D, B64F, G05B, B64D, H02P and G06F each covering under 10% — a record can carry several classes, so these shares add up to more than 100%.
Shares are the percentage of the 111 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 actuator redundancy and force fight control and every answer comes back with the patent numbers behind it.
Try EurekaAn actuation system using position sensors for rate feedback and force sensors for delta pressure, feeding a control loop that sums the difference in actuator rates with the difference in actuator forces to generate positioning commands that equalize force across a control surface.Filed by The Boeing Company; published 2012-08-21.


| # | Publication no. | Patent title | Citations |
|---|---|---|---|
| 1 | US5350988A | Digital motor controller | 129 |
| 2 | US20120290153A1 | Flight control system with alternate control path | 83 |
| 3 | US6154686A | Distributed architecture | 75 |
| 4 | US20110251739A1 | Distributed fly-by-wire system | 74 |
| 5 | US6227481B1 | Method and apparatus for controlling force fights in a rotating shaft | 47 |
| 6 | US8935015B2 | Flight control system with alternate control path | 37 |
| 7 | US20100127132A1 | Actuator force equalization controller | 31 |
| 8 | US20070068291A1 | Failure-tolerant redundant actuator system | 31 |
| 9 | WO2015088967A1 | Fiber optic sensing and control system | 27 |
| 10 | EP2374714A2 | Distributed fly-by-wire system | 27 |
Citation counts favour older records simply because they have had longer to accumulate citations inside the corpus — read this as a signal of influence on the field, not of current commercial importance.
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 patterns stand out once records, assignees and dates are cross-tabulated.
Five assignees account for 79 of the 111 records in scope. The tenth-ranked company holds only 3 records, meaning the ranked field of 27 companies has a steep drop after the leaders and a long tail of single- or few-filing entrants.
2021 was the busiest year at 13 filings; by 2024, the last year treatable as complete, published counts had fallen to 0, a -100% swing. Given the roughly 18-month publication lag, this should be read as a slowdown through the visible window rather than a verdict on 2025-26 activity, which is still filling in.
Claims concentrate in aeroplane/helicopter structures (B64C, 74.8%) and fluid-pressure actuator systems (F15B, 27.9%). Digital data processing (G06F) appears in only 4.5% of records, suggesting the control-law and software layer of force-fight mitigation is comparatively under-claimed relative to the mechanical and hydraulic layers.
Eureka can read the same corpus for gaps instead of for coverage: under-claimed branches adjacent to actuator redundancy and force fight control, with the prior art for and against each one.
| Assignee | Co-assignee | Shared families |
|---|---|---|
| Bombardier Inc. | C Series Aircraft Limited Partnership | 2 |
| Bell Helicopter Textron Inc. | SCHULTZ DAVID P | 1 |
| Bell Helicopter Textron Inc. | PRICE IAN L | 1 |
| Bell Helicopter Textron Inc. | FENNY CARLOS A | 1 |
| Bell Helicopter Textron Inc. | CURD DAVID A | 1 |
| Bombardier Inc. | Short Brothers plc | 1 |
Only 6 co-assignee pairs appear across the dataset, and the strongest pair shares just 2 records — most filings in this space are single-assignee, not joint ventures.
The ranking covers all 27 companies the data endpoint returns for this search — not a top-50 or top-100 cut. The leader holds 26 records; by fifth place that has already dropped to 7, and by tenth place to 3.
The top-ranked assignee's 26 records make it the single largest holder in the dataset, well ahead of the rest of the top five, whose fifth-place holder has just 7 records.
Record counts fall from 7 at fifth place to 3 at tenth, and the top 10 combined still only reach 104 of 111 records (93.7%) — meaning the remaining 17 ranked companies share just 7 records between them.
Every one of the leading assignees shows 0 filings in the latest year on record, consistent with the broader -100% swing from the 2021 peak. This likely reflects publication lag as much as any real pullback, since 2025-26 filings are still working through to publication.
| Assignee | Recent year | YoY |
|---|---|---|
| Bell Helicopter Textron Inc. | 0 | — |
| The Boeing Company | 0 | — |
| Honeywell International Inc. | 0 | — |
| Textron Innovations Inc. | 0 | -100% |
| United Technologies Corporation | 0 | — |
| Goodrich Actuation Systems | 0 | — |
| Embraer S.A. | 0 | — |
| Bombardier Inc. | 0 | — |
The dataset points to specific follow-up questions rather than a single conclusion.
G06F digital-processing claims cover only 4.5% of records, well behind the mechanical and hydraulic classes. Before assuming this is closed, run a targeted search on control-law and diagnostic algorithms specifically.
Explore white space in EurekaWith 26 of 111 records, the top assignee sets the boundary most new filings will need to design around. Track its recent filings even though the latest-year count reads as zero under publication lag.
Track assignee activity in EurekaThe -100% swing from 2021 to 2024 is real for completed years, but 2025-26 figures are not yet reliable given the roughly 18-month publication lag. Revisit the trend chart in six to twelve months.
Set a trend alert in EurekaIn this dataset, it is a filing that claims a system with two or more actuators driving the same load path, plus some mechanism for coordinating them — position feedback, force sensing, or a control loop that reconciles differences between channels. The search combined this concept with force-fight mitigation terms like force equalization, load sharing and cross channel monitoring, which is why the results cluster heavily around aircraft flight-control surfaces rather than generic multi-actuator machinery. Not every dual-actuator patent qualifies; the mitigation element is what puts a record in scope here.
The ranking covers 27 companies with a steep concentration at the top: the leading assignee holds 26 of the 111 records in scope, and the top five together account for 71.2% of all records. By the tenth-ranked company, holdings have dropped to just 3 records, and the remaining companies in the ranking each hold a handful or fewer. This is a field with a small number of entrenched aerospace and actuation-system suppliers rather than many equally-sized competitors.
Filings peaked at 13 in 2021 and the visible count falls to 0 by 2024, a -100% change over that span. Part of this is a genuine cooling, but part of it is a publication-lag artefact: patent applications typically take around 18 months to publish, so 2025 and 2026 figures in any dataset are always undercounted at the time of analysis. Treat 2024 as the last year that can be read with confidence, and expect the two most recent years to revise upward as more records publish.
US8245967B2, assigned to The Boeing Company, claims a feedback control loop that combines rate-feedback differences from position sensors with force differences from delta-pressure sensors to compute a positioning command that equalizes force across a control surface. It is one of the more structurally specific claims in the corpus, so a new design that avoids either the rate-difference term or the force-difference summation, or that computes equalization by a materially different control strategy, has room to design around it. It is not a blanket claim over all force equalization approaches.
IPC composition shows heavy concentration in B64C (74.8% of records) and F15B (27.9%), with G05D, G05B, B64D, H02P and G06F each under 10%. The G06F digital-processing share, at just 4.5%, stands out as thin relative to how software-defined modern flight-control law has become, suggesting algorithmic and diagnostic approaches to force-fight mitigation are comparatively under-claimed against the mechanical and hydraulic core.
Go past this page: query the whole actuator redundancy and force fight control 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.