https://www.patsnap.com/resources/blog/rd-blog/electromechanical-flight-control-actuators-patent-landscape/ · Patsnap · data cut-off 2026-07-31 · downloaded from the live page
Patent Landscape · Aircraft Hydraulics & Actuation
Electromechanical Flight Control Actuators: Patent Landscape
  • 43.1% of all 283 records sit with just five assignees, and 66.1% with ten — a field concentrated at the top with a long tail below.
  • Filings fell 80% from 20 in 2021 to 4 in 2024, the last year the dataset treats as complete.
  • B64C aeroplane/helicopter classes cover 42.8% of records while clutch-and-brake (F16D) and digital-processing (G06F) classes each sit near or under 10% — signalling where claim density thins out.
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283
Published Records
43%
Top-5 Share of All Records
-80%
Filing Growth 2021→2024
US
Leading Jurisdiction

Filing growth compares 2021 (20 records) with 2024 (4) — 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 283 records in scope (CR5), not by the ranked leaders only.

Published byPatsnap Research··7 min readSourced from Patsnap Eureka
Overview

What this landscape covers

Electromechanical flight control actuators replace hydraulic power with electric motors and mechanical torque transmission, and the patent activity in this space clusters around the failure-management problem that hydraulics solved for free: what happens when the actuator jams, backdrives, or fights another channel. The search set combines actuator architecture terms — electromechanical actuator, roller screw actuator, electromechanical flight control — with the specific failure-mode and monitoring language that separates a flight-critical design from a generic motor drive: back drive torque, jam mitigation, force fight, no-back brake, torque limiter, actuator health monitoring.

283 published records fall inside this scope between 2015 and the mid-2026 cut-off. Publication lags filing by roughly 18 months, so the 2025-2026 counts in any trend chart are still filling in and should not be read as a slowdown in themselves.

Filing activity and technology composition, 2015-2026
  1. 1GOODRICH ACTUATION SYST38
  2. 2THE BOEING CO33
  3. 3SAFRAN ELECTRONICS & DEFENSE (FR)19
  4. 4BRITAX ROMER KINDERSICHERHEIT GMBH17
  5. 5HAPTX INC15
  6. 6E2M TECH15
  7. 7RIVIAN HOLDINGS LLC13
  8. 8GOODRICH CORP13
  9. 9MESSIER DOWTY12
  10. 10FIMI FAB IMPIANTI MACCHINE INDALI12
Source: Patsnap Eureka. Assignee ranking and totals. Derived from a Patsnap search on Electromechanical Flight Control Actuators covering 2015–2026, data cut-off 2026-07-31. Counts reflect published records only and shift as new filings publish.Run this in Eureka MCP
The Data

Filing trends and technology composition

Two views of the same 283 records: how filing volume moved year over year, and which IPC subclasses carry the claim density.

Filing trend: a 2018 peak, then a steep pull-back

Filings ran at 26 in 2017 and peaked at 29 in 2018. The clearest complete-year comparison in the dataset is 2021 to 2024, where filings dropped from 20 to 4 — an 80% decline. Treat 2025 and 2026 figures as provisional given publication lag, not as confirmation the decline continued.

Filing trend: a 2018 peak, then a steep pull-back08152330262017292018201920202021202220232024202502026Most recent year is partial — publication lag means later filings are not yet visible.

Technology composition: airframe integration dominates, mechanism classes trail

B64C (aeroplanes and helicopters) appears in 42.8% of the 283 records, confirming that most filings frame the actuator as part of an aircraft system rather than a standalone mechanism. F16H gearing/transmission claims sit at 17.3%, and G09B, F16D, G06F, A63F, B60N and B25J each cover a narrower slice — several of them under 10% of records, which is where claim space is thinner rather than exhausted.

Technology composition: airframe integration dominates, mechanism classes trailB64C · Aeroplanes & helicopters12142.8%F16H · Gearing & transmissions4917.3%G09B · Educational & demonstration ai…3010.6%F16D · Clutches & brakes2910.2%G06F · Electric digital data processi…279.5%A63F · Games & amusements248.5%B60N · Vehicle seats & interior176.0%B25J · Manipulators & robots165.7%Other18063.6%

Shares are the percentage of the 283 records in scope. A patent can carry several IPC classes, so the shares add up to more than 100%.

Source: Patsnap Eureka. Filing trend and technology composition. Derived from a Patsnap search on Electromechanical Flight Control Actuators covering 2015–2026, data cut-off 2026-07-31. Counts reflect published records only and shift as new filings publish.

Go deeper on Electromechanical Flight Control Actuators with Eureka

This page is one run against one query. Ask Eureka your own question about electromechanical flight control actuators and every answer comes back with the patent numbers behind it.

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Key Patents

A representative claim and the most-cited prior art

Representative Filing
US9829055B22017-11-28

Electromechanical actuator comprising a mechanical roller torque limiter (US9829055B2)

SAFRAN ELECTRONICS & DEFENSE

An electromechanical actuator comprising a body and an electric motor driving at least one motion transmission element connected to the body via a brake device, a mechanical torque limiter with rollers, and a unidirectional transmission member. The brake device includes an electrical activator member so that when powered, the unidirectional transmission member is released relative to the body; when unpowered, it is secured to the body and opposes pivoting up to a maximum torque set by the limiter.Filed by Safran Electronics & Defense, 2017-11-28.

US9829055B2 — patent drawing 1US9829055B2 — patent drawing 2
View full filing
Most-cited records in this search
#Publication no.Patent titleCitations
1US20160139666A1Whole-body human-computer interface614
2US5670856AFault tolerant controller arrangement for electric motor driven apparatus88
3US9652037B2Whole-body human-computer interface84
4US5957798AFail-free actuator assembly56
5US20030164422A1Latch device, in particular for latching an airplane landing gear or an airplane landing gear hatch, and a me…52
6US6811118B2Latch device, in particular for latching an airplane landing gear or an airplane landing gear hatch52
7US20170242477A1Whole-body human-computer interface32
8US9904358B2Whole body human-computer interface32
9WO2015002850A1Whole-body human-computer interface32
10US20190127049A1Adaptive feedback control of force fighting in hybrid actuation systems25

Citation counts favour older filings simply because they have had longer to accumulate citations inside this corpus — read them as a signal of influence on later designs, not as a ranking of current relevance.

Each row carries its publication number; clicking a row searches Eureka by that number.

Source: Patsnap Eureka. Citation counts and representative records. Derived from a Patsnap search on Electromechanical Flight Control Actuators covering 2015–2026, data cut-off 2026-07-31. Counts reflect published records only and shift as new filings publish.Run this in Eureka MCP
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Insights

What the numbers mean for strategy

Three findings that shape where to file, where to watch, and where the field still has room.

Concentration
43.1% / top 5
of 283 records

The top of the field is tight, the rest is thin

Five assignees hold 43.1% of all 283 records and ten hold 66.1%. That leaves 37 ranked companies splitting roughly a third of the field, most with single-digit filing counts — a classic leader-plus-long-tail structure rather than a fragmented market.

Source: assignee ranking, 47 companies
Momentum
20 → 4, -80%
2021 to 2024

Filing volume has pulled back sharply from its peak

After peaking at 29 filings in 2018, volume declined to 4 by 2024 — the last year the dataset treats as complete. That drop does not necessarily mean interest has faded; it can also reflect consolidation of claim space by early filers, or a shift toward trade-secret protection of health-monitoring software.

2025-2026 figures are still filling in due to publication lag
Technology mix
42.8% B64C
of 283 records

Airframe-system framing dominates over standalone mechanism claims

Nearly half of records classify under aeroplane/helicopter systems (B64C), while gearing (F16H) trails at 17.3% and clutch/brake mechanism claims (F16D) sit at just 10.2%. Filers are claiming the actuator as installed, not the underlying mechanical sub-assembly in isolation.

IPC subclass shares, 283 records in scope
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Looking for what nobody has claimed yet?

Eureka can read the same corpus for gaps instead of for coverage: under-claimed branches adjacent to electromechanical flight control actuators, with the prior art for and against each one.

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Source: Patsnap Eureka. Co-assignee relationships and derived observations. Derived from a Patsnap search on Electromechanical Flight Control Actuators covering 2015–2026, data cut-off 2026-07-31. Counts reflect published records only and shift as new filings publish.Run this in Eureka MCP
Players

Who is filing, and where the gate sits

The leader board is short and the entry bar for a top-ten position is modest in absolute terms, which matters for how you read 'concentration' here.

Leader
38 records
single-assignee count

One filer sits well ahead of the pack

The top-ranked assignee holds 38 records against a fifth-place figure of 15 and a tenth-place figure of 12 — a steep drop-off after the leader rather than a gradual taper.

Assignee ranking, 47 companies
Mid-field
15 / 5th place
records

Positions five through ten cluster closely

Fifth place holds 15 records and tenth holds 12 — a narrow three-record spread across six ranking positions, meaning a handful of additional filings could reorder the mid-table.

Assignee ranking, 47 companies
Recent activity
0 in latest year
for several top-10 assignees

Even leading assignees show no filings in the latest year

Several of the highest-ranked assignees, including the top-ranked leader, recorded zero filings in the most recent year captured. Given publication lag, this is as likely to reflect a filing gap still working through the pipeline as an actual pause in R&D.

Recent-year momentum by assignee
🔍
Under-claimed branches worth checking before filing
Composition shares below 10% of the 283 records mark areas with room, not areas without value.
actuator health monitoring algorithmsno-back brake mechanism variantsforce-fight detection between redundant channelsroller-screw torque limiter designsjam-mitigation sensor fusion
Rank all filers by momentum →
Recent-year filing momentum by assignee
AssigneeRecent yearYoY
Goodrich Actuation Systems0
The Boeing Company0
Safran Electronics & Defense0
Britax Römer Kindersicherheit GmbH0
HAPTX INC0
E2M Technologies0
Rivian Holdings LLC0
B.F. Goodrich Corporation0
Source: Patsnap Eureka. Assignee-level momentum. Derived from a Patsnap search on Electromechanical Flight Control Actuators covering 2015–2026, data cut-off 2026-07-31. Counts reflect published records only and shift as new filings publish.Run this in Eureka MCP
What's Next

Where to take this analysis

The dataset points to specific next steps depending on whether you are clearing freedom to operate or scoping new filings.

Check the representative claim against your architecture

US9829055B2's torque-limiter and unidirectional transmission combination is a useful benchmark claim to design around before committing to a roller-screw no-back mechanism.

Explore the claim in Eureka

Watch the under-10% IPC branches

Health-monitoring software (G06F) and clutch/brake mechanism claims (F16D) sit below the airframe-integration share, suggesting narrower but less contested claim space.

Run a white-space search in Eureka

Track assignees with a zero-filing gap

Several top-ranked assignees show no filings in the latest year despite historical leadership — worth monitoring for whether that reflects pipeline lag or a genuine strategic shift.

Set up assignee monitoring in Eureka
Source: Patsnap Eureka. Forward-looking reading of the same dataset. Derived from a Patsnap search on Electromechanical Flight Control Actuators covering 2015–2026, data cut-off 2026-07-31. Counts reflect published records only and shift as new filings publish.Run this in Eureka MCP
FAQ

Common questions about this landscape

Answers are grounded in the same dataset. Derived from a Patsnap search on Electromechanical Flight Control Actuators covering 2015–2026, data cut-off 2026-07-31. Counts reflect published records only and shift as new filings publish.Run this in Eureka MCP

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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.