Flight Control Redundancy Patents: Who Leads, Where the Gaps Are 2026
- 67.7% concentration. The top five ranked assignees account for 21 of the 31 records in scope — filing has consolidated hard around a small group of aerospace and industrial control specialists.
- One class dominates the claim space. G05B control and regulating systems appears in 71.0% of records, far ahead of gas-turbine plants and digital data processing, each at 32.3%.
- Filing peaked in 2017 and has since gone quiet. Ten records published that year against zero in the most recent complete year — a signal worth checking against the 18-month publication lag before reading too much into it.
Top-5 share is the combined record count of the five largest assignees divided by all 31 records in scope (CR5), not by the ranked leaders only.
What this landscape covers
Flight control redundancy and voting covers the architectures that keep a flight control computer working after a single channel fails: triplex redundancy, dissimilar redundancy, majority-voting logic, channel comparison and the reconfiguration logic that isolates a faulted channel without dropping control authority. The 31 records in scope span command monitor architectures alongside the fault-detection and common-mode-failure protections that make triple- or higher-order voting worth the added hardware cost.
Filings cluster around control-system claims rather than airframe-specific ones, and the receiving-office spread — led by the United States and the European Patent Office, with smaller counts in Canada, Germany, Austria and China — points to a field prosecuted mainly by established aerospace and industrial-control filers rather than a broad international rush.
Filing trend and technology composition
Two views of the same 31 records: when they were filed, and which control, propulsion or data-processing classes they sit in.
Filing trend, 2017–2026
Filings peaked at 10 in 2017 and tapered toward zero by the most recent year. Because publication typically lags filing by around 18 months, the last one to two years understate real filing activity and should not be read as a decline yet.
IPC subclass composition
G05B (control and regulating systems) covers 71.0% of the 31 records, with F02C (gas-turbine plants) and G06F (electric digital data processing) tied at 32.3% each — reflecting that voting and fault-detection logic is claimed as much around engine control as around the flight computer itself. Records can carry more than one class, so these shares sum to well over 100%.
Shares are the percentage of the 31 records in scope. A patent can carry several IPC classes, so the shares add up to more than 100%.
Go deeper on Flight Control Redundancy and Voting with Eureka
This page is one run against one query. Ask Eureka your own question about flight control redundancy and voting and every answer comes back with the patent numbers behind it.
Try EurekaThe most-cited architectures
Multiple redundant computer system combining fault diagnostics and majority voting with dissimilar redundancy technology
A multiple redundant computer system includes three primary processor modules (PPM) and three redundant processor modules (RPM) operating synchronously. Primary and redundant processor modules are dissimilar in hardware and software for decreasing the probability of a common cause system failure. Each primary and redundant processor module receives input data from associated primary and redundant input modules respectively, executes control program and transfers output data to an output module. The output module produces a system output as the result of 2-out-of-3 voting among output data generated by PPMs. In response to PPMs hard failures, the output module still produces the system output.US7877627B1, cited 138 times — the clearest documented example of pairing dissimilar redundancy with 2-out-of-3 output voting in a single claimed system.


| # | Publication no. | Patent title | Citations |
|---|---|---|---|
| 1 | US6550018B1 | Hybrid multiple redundant computer system | 239 |
| 2 | US4622667A | Digital fail operational automatic flight control system utilizing redundant dissimilar data processing | 145 |
| 3 | US7877627B1 | Multiple redundant computer system combining fault diagnostics and majority voting with dissimilar redundancy… | 138 |
| 4 | US5206810A | Redundant actuator control | 55 |
| 5 | US5533188A | Fault-tolerant processing system | 42 |
| 6 | EP0186965A1 | Digital fail operational automatic flight control system utilising redundant dissimilar data processing | 31 |
| 7 | US5210871A | Interprocessor communication for a fault-tolerant, mixed redundancy distributed information processing system | 29 |
| 8 | EP3246547A1 | Controlling a gas turbine considering a sensor failure | 16 |
| 9 | WO2017198528A1 | Controlling a gas turbine considering a sensor failure | 11 |
| 10 | US20190128192A1 | Controlling a gas turbine considering a sensor failure | 10 |
Citation counts are drawn from a searched corpus and skew toward older, foundational filings — treat them as a measure of influence on later work, not of current commercial relevance.
Each row carries its publication number; clicking a row searches Eureka by that number.
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Three findings from the ranking, the IPC breakdown and the citation table that matter more than the raw counts.
Filing has consolidated, not fragmented
With the top five ranked assignees holding 21 of 31 records and the top ten holding 27 (87.1%), this is not a field with many independent small filers. A new entrant is filing into territory already claimed by a handful of aerospace and industrial-control incumbents.
Voting logic is claimed as control architecture, not airframe hardware
B64C (aeroplanes and helicopters) and B64D (aircraft equipment) together cover a minority of records — 16.1% and 3.2% respectively — while G05B and G06F dominate. Redundancy and voting claims are largely written at the control-system and data-processing level, portable across gas-turbine, spacecraft and airframe applications alike.
The foundational art is decades old
The most-cited record, a hybrid multiple redundant computer system, sits well ahead of the next entries, and several of the highest-cited filings date to the 1980s and 1990s. High citation counts here mark influence on the field's vocabulary, not current freedom-to-operate risk.
Eureka can read the same corpus for gaps instead of for coverage: under-claimed branches adjacent to flight control redundancy and voting, with the prior art for and against each one.
Who holds the ranked positions
The ranking returns 15 companies across the 31 records in scope, led by a single assignee at 6 records, with the fifth position holding 2 and the tenth holding 1 — a steep drop-off rather than a gradual one.
A single filer sets the pace
The leading assignee's 6 records is nearly triple the count at fifth place, which sits at 2. That gap is the clearest sign that redundancy and voting architecture claims are not evenly distributed even among the top filers.
A tight cluster behind the leader
Positions two through five sit close together before the count drops again by tenth place, which holds 1 record. This is a field with one clear leader and a compressed group of established aerospace and industrial-control names behind it.
Single-filing entrants fill out the ranking
Beyond the top ten, the remaining ranked assignees hold single records apiece. That pattern is typical of a mature control-engineering niche: most organisations file once around a specific fault-detection or voting scheme rather than building a sustained portfolio.
| Assignee | Recent year | YoY |
|---|---|---|
| Siemens AG | 0 | — |
| Hamilton Sundstrand Corp | 0 | — |
| Honeywell International Inc | 0 | — |
| Sperry Corporation | 0 | — |
| Bombardier Inc | 0 | -100% |
| Embraer SA | 0 | — |
| General Electric Co | 0 | — |
| The University of Akron | 0 | — |
Where to take this analysis
The ranking and IPC breakdown point to specific next steps depending on whether the goal is freedom-to-operate, portfolio strategy or technical scoping.
Check freedom-to-operate against the leader's claim scope
With one assignee holding 6 of 31 records and the top five holding 67.7%, any new triplex or dissimilar-redundancy filing should be checked against the leader's claim language before drafting.
Explore claim scope in EurekaScope the under-claimed sub-areas
Byzantine fault isolation and non-electric variable reconfiguration sit well below G05B's 71.0% density — a narrower search here can surface open claim space faster than a broad keyword sweep.
Run a white space search in EurekaWatch for the publication-lag correction
The drop to zero filings in the most recent year is partly a reporting artefact; re-run the trend once another 18 months of publications land to see whether 2017's peak was structural or cyclical.
Track filing trends in EurekaCommon questions on this landscape
Triplex redundancy refers to an architecture with three parallel processing or actuation channels, where a majority-voting scheme resolves disagreement and isolates a faulted channel. In this dataset it appears alongside dissimilar redundancy, where the three channels additionally use different hardware or software to reduce the chance of a common-mode failure taking out all channels at once. The representative record in this landscape, US7877627B1, is a direct example: three primary and three redundant processor modules with 2-out-of-3 output voting.
The ranking returned by this dataset covers 15 companies across 31 records, led by a single assignee with 6 records — nearly triple the count held at fifth place, which sits at 2. The top five combined account for 21 records, or 67.7% of all records in scope, and the top ten account for 27, or 87.1%. That is a steep concentration curve: a small group of aerospace and industrial-control filers holds most of the documented claim space, with the remaining ranked assignees each holding a single record.
The trend data shows 10 filings in 2017 against zero in the most recent complete year, but that decline should be read cautiously. Patent publication typically lags the actual filing date by around 18 months, so the last one to two years in any dataset are always undercounted relative to what has actually been filed. A genuine slowdown cannot be confirmed until enough time has passed for those recent filings to publish.
US7877627B1 claims a specific combination: three dissimilar primary processor modules paired with three dissimilar redundant processor modules, each fed by its own input modules, with a 2-out-of-3 voting output stage that continues producing output even after hard failures in the primary set. A design that avoids the dissimilar hardware-and-software pairing, or that uses a voting ratio or channel count outside that specific claimed structure, sits outside its literal scope. Anyone building a triplex voting scheme close to this structure should read the full claim set rather than relying on the abstract, since the dissimilarity requirement and the specific 2-out-of-3 output logic are likely the narrowest and most defining limitations.
Relative to G05B control and regulating systems, which covers 71.0% of the 31 records in scope, several adjacent classes show far lower density: G01R electric and magnetic measurement sits at 6.5%, and B64D aircraft equipment and G01C navigation and gyroscopes each sit at 3.2%. That does not guarantee open white space, since a single strong filing can dominate a thin class, but it flags specific, narrower areas — instrument-level fault detection and gyroscope-integrated channel comparison among them — worth a dedicated search before assuming the ground is occupied.
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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.