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Distributed Electric Propulsion Patents: Top Companies & Trends 2026

Distributed Electric Propulsion Patents: Top Companies & Trends 2026
https://www.patsnap.com/resources/blog/rd-blog/distributed-electric-propulsion-for-air-mobility-patent-landscape/ · Patsnap · data cut-off 2026-07-31 · downloaded from the live page
Patent Landscape · Aerospace Propulsion
Distributed electric propulsion patents for air mobility: who leads and where the field is still open
  • 57.1% concentration. The top 5 of 40 ranked assignees account for 72 of the 126 records in scope — filing here is dominated by a handful of aviation and propulsion specialists, not a broad field of entrants.
  • Filing has flattened, not accelerated. Activity peaked at 21 records in 2024 after a 2022 midpoint of just 3, and the leading filer's own output fell 70% year-on-year in the latest period.
  • Claims cluster in aircraft equipment, not motors. B64D (aircraft equipment) touches 57.9% of the 126 records, far ahead of H02K electric motors at 13.5% — the crowded ground is system integration, not the motor itself.
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126
Published Records
57%
Top-5 Share of All Records
+5%
Filing Growth 2021→2024
US
Leading Jurisdiction

Filing growth compares 2021 (20 records) with 2024 (21) — 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 126 records in scope (CR5), not by the ranked leaders only.

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

What the patent record shows about distributed electric propulsion

Distributed electric propulsion spreads thrust across multiple small electric propulsors rather than a single large engine, and the patent activity in this dataset follows that architecture into aircraft equipment, power distribution and motor design rather than clustering around a single component. Across 126 patent families filed between 2015 and mid-2026, the busiest claim territory is B64D aircraft equipment, covering just under three in five records, with B64C aeroplane and helicopter classifications close behind. Electric vehicle propulsion, marine propulsion, drone-specific classes, motor design and power-grid classes each appear in a smaller but still meaningful share of the same records.

Filing is concentrated at the top of the assignee ranking, but the trend line has cooled since its 2024 peak, and the most recent year is necessarily undercounted because publication typically lags filing by around 18 months. Read the following sections as a map of where claim density already sits and where it has not yet formed, not as a verdict on which approach will win commercially.

Filing activity and technology composition, 2015-2026
  1. 1ARCHER AVIATION INC27
  2. 2THE BOEING CO14
  3. 3AURORA FLIGHT SCIENCES CORP13
  4. 4WARTSILA FINLAND OY12
  5. 5EVOLITO LTD6
  6. 6ASKOLL EVA SPA6
  7. 7POLITECNICO DI MILANO4
  8. 8EUROCOPTER FRANCE SA4
  9. 9VERTICAL AEROSPACE GRP LTD4
  10. 10JAGUAR LAND ROVER LTD3
Source: Patsnap Eureka. Assignee ranking and totals. Derived from a Patsnap search on Distributed Electric Propulsion for Air Mobility 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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The Data

Filing trends and technology composition

Two views of the same 126 records: how filing volume has moved year over year, and how those records distribute across IPC subclasses.

Filing trend, 2017-2026

Filings ran at 13 in 2017, dropped to a low point around the 2022 midpoint of 3, then rose to a peak of 21 in 2024 before easing off. The 2026 figure of 3 is a partial-year count and will rise as later publications land, consistent with the usual 18-month lag between filing and publication.

Filing trend, 2017-20260613192513201720182019202020212022202321202421202532026Most recent year is partial — publication lag means later filings are not yet visible.

IPC subclass composition

B64D aircraft equipment appears in 57.9% of the 126 records and B64C aeroplanes/helicopters in 33.3%, making airframe-level integration the densest claim territory. Electric motor design (H02K), power supply and grid systems (H02J), and vehicle propulsion classes (B60L, B60K) each cover a smaller slice, and because records can carry multiple IPC codes these shares sum to more than 100%.

IPC subclass compositionB64D · Aircraft equipment7357.9%B64C · Aeroplanes & helicopters4233.3%B60L · Electric vehicle propulsion1814.3%B63H · Marine propulsion & steering1713.5%B64U · Unmanned aerial vehicles (dron…1713.5%H02K · Electric motors & generators1713.5%H02J · Power supply & grid systems1411.1%B60K · Vehicle propulsion & drive97.1%Other6249.2%

Shares are the percentage of the 126 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 Distributed Electric Propulsion for Air Mobility covering 2015–2026, data cut-off 2026-07-31. Counts reflect published records only and shift as new filings publish.

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Key Patents

The most-cited records in this dataset

Representative filing
US20220119121A12022-04-21

Integrated Electric Propulsion Unit (US20220119121A1)

THE BOEING COMPANY

This Boeing filing claims an electric propulsion unit combining a housing, AC motor, hollow motor shaft, axially translatable beta rod, variable-pitch propeller, governor, inverter and controller in a single integrated assembly — pitch control is achieved by moving the beta rod inside the hollow shaft rather than through a separate actuation mechanism.Abstract text is drawn directly from the published filing.

US20220119121A1 — patent drawing 1US20220119121A1 — patent drawing 2
View full filing
Most-cited records
#Publication no.Patent titleCitations
1US20170203839A1Hybrid Propulsion Vertical Take-Off and Landing Aircraft241
2US20220119121A1Integrated Electric Propulsion Unit60
3EP3805107A1Hybrid propulsion system for aircraft, method of operating a hybrid propulsion system, and a hybrid aircraft59
4US10926874B2Hybrid propulsion vertical take-off and landing aircraft44
5WO2017123699A1Hybrid propulsion vertical take-off and landing aircraft41
6JP2010161846AAc motor driving unit and electric propulsion unit using same38
7WO2012175624A1Improvement in ship propulsion engine fuel efficiency29
8US20060040573A1Electric propulsion unit25
9US20220234470A1Systems and methods for power distribution in electric aircraft23
10US20150266535A1Electric propulsion unit and torque transmission group for an electric scooter and corresponding scooter22

Citation counts favour older filings that have had more time to accumulate citations inside this corpus; treat them as a measure of influence on the field so far, not of current technical importance.

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 Distributed Electric Propulsion for Air Mobility 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 a filing decision

Three findings from the dataset that should shape where a new filing targets claim space, and where it competes head-on with dense prior art.

Concentration
57.1% of 126
held by top 5 of 40 ranked assignees

A small group holds most of the claim territory

The leader alone accounts for 27 records, and the top 5 combined cover 72 of the 126 records in scope. That leaves a long tail among the remaining 35 ranked assignees, many with only one or two filings, which is typical of a field still being defined by a handful of specialists rather than broad industry adoption.

Top 10 combined reach 73.8% of records.
Momentum
Peak 21 in 2024
then declining into 2026

Growth has flattened since the 2024 peak

Filing volume rose from a 2022 midpoint of just 3 records to a peak of 21 in 2024, but the leading filer's own output fell 70% year-on-year in the most recent period. Combined with several other tracked assignees showing zero filings in the latest year, this points to a field consolidating its existing claims rather than expanding into new ones.

Most recent year is a partial count.
Technology mix
57.9% B64D
vs. 13.5% H02K motors

System integration is claimed more than the motor itself

B64D aircraft equipment and B64C airframe classes dominate the composition, while electric motor design (H02K) and power supply/grid systems (H02J) sit well behind at 13.5% and 11.1% of records respectively. Prior art density is highest around how propulsors integrate with the airframe, not around motor or inverter design in isolation.

Shares sum above 100% because records carry multiple IPC codes.
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Eureka can read the same corpus for gaps instead of for coverage: under-claimed branches adjacent to distributed electric propulsion for air mobility, 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 Distributed Electric Propulsion for Air Mobility 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 gaps sit

The ranked assignee list spans established aerospace primes, eVTOL developers and specialist electric propulsion firms, with filing concentrated among a small number of them.

Leader
27 records
single largest filer in the ranking

The top filer sets the pace, but has slowed

The leading assignee's 27 records make it the largest single contributor to the dataset, yet its latest-year output fell 70% year-on-year, suggesting a pause in new filing rather than a retreat from the space.

Recent-year momentum data.
Long tail
35 of 40 ranked
assignees below the top 5

Most participants file thinly

Beyond the top 5, the remaining ranked assignees — including established aerospace names, motor specialists and academic institutions — hold comparatively few records each, indicating exploratory or defensive filing rather than sustained programmes.

40 companies make up the full ranked list.
Collaboration
7 co-assignee pairs
identified across the dataset

Co-filing is limited and clustered

Only seven co-assignee pairs appear in the dataset, with the strongest links tied to a helicopter-and-aircraft manufacturer pairing and a marine propulsion firm filing jointly with named inventors, pointing to a field where most work is still filed by a single entity rather than through joint ventures.

Strongest pair recurs three times.
🔍
Under-claimed sub-areas worth watching
Branches where filing density is comparatively light relative to the core aircraft-equipment and airframe classes.
Thermal management of distributed invertersPower distribution bus fault isolationPropulsor placement for wing interaction controlFailure-mode reconfiguration across propulsor arraysSpecific-power optimisation for motor-inverter stacks
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Recent-year filing momentum by assignee
AssigneeRecent yearYoY
Archer Aviation Inc.3-70%
The Boeing Company0
Aurora Flight Sciences Corp0
Wartsila Finland Oy0
Askoll EVA S.p.A.0
EVOLITO LTD0-100%
Politecnico di Milano0
Eurocopter France SA0
Source: Patsnap Eureka. Assignee-level momentum. Derived from a Patsnap search on Distributed Electric Propulsion for Air Mobility 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 the goal is freedom-to-operate, competitive tracking or identifying open claim space.

Map claims against a specific propulsor architecture

The IPC composition shows where prior art is dense at the subclass level, but a freedom-to-operate check needs claim-level comparison against a defined architecture, motor count and failure-mode strategy.

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Track the slowing leaders for re-acceleration

Several top assignees show zero filings in the latest year; monitoring their subsequent publications will show whether this is a lull before a new filing wave or a genuine pullback.

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Test claim language in the under-claimed branches

Thermal management, power bus fault isolation and propulsor-array failure modes show comparatively lighter filing density than airframe integration, making them worth a closer novelty check before drafting.

Run a novelty check in Eureka
Source: Patsnap Eureka. Forward-looking reading of the same dataset. Derived from a Patsnap search on Distributed Electric Propulsion for Air Mobility 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 distributed electric propulsion patents

Answers are grounded in the same dataset. Derived from a Patsnap search on Distributed Electric Propulsion for Air Mobility 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.

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