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Electric Aircraft Propulsion Aerodynamics Patents: Leaders & Trends 2026

Electric Aircraft Propulsion Aerodynamics Patents: Leaders & Trends 2026
https://www.patsnap.com/resources/blog/rd-blog/electric-aircraft-propulsion-aerodynamics-patent-landscape/ · Patsnap · data cut-off 2026-07-31 · downloaded from the live page
Aerospace & Propulsion · Patent Landscape
Electric Aircraft Propulsion Aerodynamics Patents
  • Filings peaked in 2020 at 16 and dropped to a single filing by the 2022 midpoint — the core architecture claims were staked out early.
  • B64D covers all 36 families while thinner classes like F04D (pumps), B64F and H04W sit at single-digit counts — the visible white space.
  • One filing chain dominates citations with 392 and 249-cite records anchoring the series hybrid-electric powertrain architecture most others build around.
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36
Published Records
-100%
3-Yr Growth (lag-adjusted)
US
Leading Jurisdiction
2020
Peak Filing Year
Published byPatsnap Research··8 min readSourced from Patsnap Eureka
Overview

What this patent set covers

This landscape covers patent families at the intersection of electric and hybrid-electric aircraft propulsion and the aerodynamics of ducted fans, propellers, boundary-layer ingestion and distributed propulsion — filtered to IPC classes covering aeroplane control surfaces, electric propulsion units and aircraft structural elements. It is a narrow, technically specific slice: 36 patent families in total, concentrated in aircraft equipment and airframe classes rather than spread evenly across the aerospace patent literature.

Coverage runs from 2015 through the mid-2026 data cut-off, with the United States as the dominant receiving office by a wide margin over Canada, Europe, India and Australia. The filing trend and IPC composition below describe a field where the foundational architecture claims came early and concentrated, leaving a visible set of thinner, adjacent branches still open.

Filing trend and technology composition, 2015–2026
  1. 1Detroit Electric Automobile Company20
  2. 2ZUNUM AERO INC16
Source: Patsnap Eureka. Assignee ranking and totals. Derived from a Patsnap search on Electric Aircraft Propulsion Aerodynamics 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
Filing Data

Filing trends and technology composition

Thirty-six patent families make up this corpus, spread across eight IPC subclasses and filed predominantly through the US patent office. The trend line and technology split below show where claim density sits today and where it has thinned out since the 2020 peak.

Filing activity peaked in 2020, then went flat

Filings rose from zero in 2017 to a peak of 16 in 2020, then fell back sharply — the 2022 midpoint sits at just one filing. Recent-year counts are understated because publication lags filing by roughly 18 months, but the drop from peak is steep enough that it likely reflects a real slowdown in new architectural filings, not just a reporting lag.

Filing activity peaked in 2020, then went flat0510152002017201820191620202021202220232024202502026Most recent year is partial — publication lag means later filings are not yet visible.

Claim density concentrates in airframe and motor classes

B64D (aircraft equipment) covers all 36 records, and B64C (aeroplanes and helicopters) appears in 22 — together these define the propulsion-architecture core of the corpus. H02K (electric motors and generators) at 18 shows steady hardware-side claiming, while G08G and G01C point to navigation and traffic-management concepts filed alongside the propulsion claims. F04D, B64F and H04W each sit in single digits, marking the thinnest branches of the tree.

Claim density concentrates in airframe and motor classesB64D · Aircraft equipment36100.0%B64C · Aeroplanes & helicopters2261.1%H02K · Electric motors & generators1850.0%G08G · Traffic control systems1233.3%G01C · Distance, navigation & gyrosco…925.0%F04D · Non-positive-displacement pumps411.1%B64F · Ground installations for aircr…12.8%H04W · Wireless communication networks12.8%

Shares are the percentage of the 36 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 Electric Aircraft Propulsion Aerodynamics 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 filing that defines the claimed envelope

Representative filing
US11465763B22022-10-11

Hybrid-electric aircraft, and methods, apparatus and systems for facilitating same

ZUNUM AERO, INC.

Hybrid-electric aircraft and a series hybrid powertrain configured to power the aircraft for a medium-haul flight. The series hybrid powertrain includes a plurality of energy storage units, at least one range-extending generator, and a plurality of electric propulsors, each coupled to a distribution bus. The electric propulsors can produce a maximum thrust of at least 15 MW. During a cruise regime, the hybrid-electric aircraft can have an airspeed of at least 0.7 Mach at an altitude of less than 32,000 feet, and the plurality of electric propulsors can have a fan pressure ratio of between 1.15 and 1.19. The hybrid-electric aircraft can have a degree of hybridization of at least 25%.Granted 2022-10-11 to Zunum Aero, Inc.; the numeric operating envelope in this claim recurs across the related, higher-cited filings in the same family.

US11465763B2 — patent drawing 1US11465763B2 — patent drawing 2
View full filing
Most-cited records in this corpus
#Publication no.Patent titleCitations
1US20160236790A1System and methods for implementing regional air transit network using hybrid-electric aircraft392
2US20200290742A1Hybrid-electric aircraft, and methods, apparatus and systems for facilitating same249
3US20180134400A1System and methods for implementing regional air transit network using hybrid-electric aircraft87
4US9561860B2System and methods for implementing regional air transit network using hybrid-electric aircraft69
5US20210107664A1Electric aircraft propulsion system44
6WO2020227837A1Electric aircraft propulsion system37
7US10501194B2System and methods for implementing regional air transit network using hybrid-electric aircraft36
8US20200346769A1System and methods for implementing regional air transit network using hybrid-electric aircraft35
9US20220009644A1Electric aircraft propulsion system28
10EP3657468A1System and methods for implementing regional air transit network using hybrid-electric aircraft18

Ranked by citation count within the searched corpus; older filings accumulate more citations simply by being older, so treat this as a map of influence rather than current activity.

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 Electric Aircraft Propulsion Aerodynamics 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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Analysis

What the filing pattern signals

Thirty-six families is a small corpus, so read every proportion here as a signal about where claim attention has gone, not as a market-size estimate. Three patterns stand out once the trend, IPC spread and citation concentration are put side by side.

Trend
16 → 1
filings, 2020 peak to 2022 midpoint

The architectural land grab happened early

Filing volume rose from nothing in 2017 to 16 in 2020 and then collapsed to a single filing by 2022. That shape is consistent with a short window in which the core series hybrid-electric powertrain concepts were claimed, followed by a much quieter period where later filers work around an already-defined architecture rather than proposing new ones.

Most recent year is understated by publication lag; treat the drop as directional, not exact.
Composition
36 / 22 / 18
records in B64D / B64C / H02K

Claim density sits in airframe and motor, not in support systems

Every record in the corpus touches B64D (aircraft equipment), and most also touch B64C (aeroplanes) or H02K (electric motors and generators). Support and integration classes — F04D, B64F, H04W — barely register, which is where a new filer has room to define terms rather than argue around existing ones.

IPC counts overlap; a record can sit in more than one subclass.
Citation concentration
392 cites
on the top-cited record

Influence concentrates in one filing family

The most-cited record draws 392 citations, more than four times the fifth-ranked record's 44. That concentration means the field's foundational thinking is unusually easy to trace to one architecture — series hybrid-electric propulsion for regional air transit — but it also means citation rank tells you about historical influence, not current filing activity.

Older filings accumulate citations simply by being older; weight recent filings on volume, not cites.
Eureka AI Agent
Looking for what nobody has claimed yet?

Eureka can read the same corpus for gaps instead of for coverage: under-claimed branches adjacent to electric aircraft propulsion aerodynamics, with the prior art for and against each one.

Find the white space →
Source: Patsnap Eureka. Co-assignee relationships and derived observations. Derived from a Patsnap search on Electric Aircraft Propulsion Aerodynamics 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 activity has gone quiet

The assignee picture in this corpus is thin at the top and thinner still in the latest year. Recent-year momentum data shows the two tracked assignees at zero filings in the latest year, one of them down 100% year-over-year — consistent with the broader trend of a 2020 peak that has not been repeated.

Filing concentration
36 families
total corpus size

A small, technically specific corpus

At 36 families, this is a narrow landscape rather than a broad one. Concentration in a handful of architecture-defining filings means new entrants are more likely to be negotiating around existing claims than filing into open ground on the propulsion architecture itself.

Family count is the fairer unit here since it neutralises multi-jurisdiction duplication.
Recent momentum
0 filings
latest year, both tracked assignees

Momentum has stalled at the top

Both assignees with recent-year momentum data show zero filings in the latest tracked year, with one down 100% year-over-year. That lines up with the corpus-wide trend line, where the 2020 peak of 16 filings has not been approached since.

Latest-year counts are always the most understated due to publication lag.
Geographic filing
18 of 36
records via United States receiving office

Filing is US-centred with a thin international tail

The United States receives half of this corpus's filings, with Canada, the EPO, Australia and India each accounting for a handful. That pattern suggests the core IP strategy in this field is built around US protection first, with selective international filing rather than broad multi-jurisdiction coverage.

Based on receiving-office counts across the 36-record corpus.
🔍
Under-claimed branches worth checking before you file
These sub-areas show materially thinner IPC coverage than the core architecture classes — a signal worth validating against your own concept before assuming the space is open.
Boundary-layer-ingestion pump integrationDucted-fan variable pitch control linkagesDistributed-propulsor wireless coordinationGround-support charging aerodynamic interfaces
Rank all filers by momentum →
Recent-year filing momentum
AssigneeRecent yearYoY
Detroit Electric Automobile Company0
ZUNUM AERO INC0-100%
Source: Patsnap Eureka. Assignee-level momentum. Derived from a Patsnap search on Electric Aircraft Propulsion Aerodynamics 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 trend and composition data point to a narrow, early-concentrated field with specific gaps. These are the natural next steps for turning that into a filing or freedom-to-operate decision.

Run a freedom-to-operate check against the series-hybrid claim family

If your design touches series hybrid-electric powertrains, compare its thrust, Mach, altitude and hybridization parameters against the numeric envelope in the highest-cited filings before committing to an architecture.

Check claim scope in Eureka

Validate the pump-integration and support-system gaps

F04D, B64F and H04W each show single-digit record counts against a 36-record corpus — test whether that reflects genuine white space or low commercial interest before drafting into it.

Explore white space in Eureka

Track assignee momentum before the next filing wave

With both tracked assignees at zero filings in the latest year, watch for the next uptick in filing activity to see who re-enters the space and with what architecture.

Monitor assignees in Eureka
Source: Patsnap Eureka. Forward-looking reading of the same dataset. Derived from a Patsnap search on Electric Aircraft Propulsion Aerodynamics 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 on electric aircraft propulsion aerodynamics patents

Answers are grounded in the same dataset. Derived from a Patsnap search on Electric Aircraft Propulsion Aerodynamics 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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