https://www.patsnap.com/resources/blog/rd-blog/scramjet-and-hypersonic-propulsion-patent-landscape/ · Patsnap · data cut-off 2026-07-31 · downloaded from the live page
Patent Landscape · Aerospace Propulsion
Scramjet and Hypersonic Propulsion Patents: Filing Trends and Open Claim Space
  • Filing has flattened, not grown. annual filings peaked at 17 in 2023 after climbing from 10 in 2017, with the 2022 midpoint at just 6 — this is a plateauing field, not a runaway one.
  • The US and China dominate filing venue. 48 US and 42 China receiving-office filings dwarf Europe (14), India (10), Japan (6) and the PCT route (5), so venue strategy narrows fast.
  • Co-filing is almost nonexistent. only two co-assignee pairs appear across 146 families, meaning most claim positions here are held solo rather than built through joint development.
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146
Published Records
34%
Top-5 Share of All Records
-17%
3-Yr Growth (lag-adjusted)
US
Leading Jurisdiction
Published byPatsnap Research··7 min readSourced from Patsnap Eureka
Overview

What the scramjet and hypersonic propulsion filing record shows

Scramjet propulsion patenting sits at the intersection of combustion engineering and high-Mach aerodynamics, and the claim language reflects that split: inlet isolator geometry, fuel mixing at supersonic flow velocities, thermal protection of combustor walls, and flame-holding under conditions where residence time is measured in milliseconds. The search set defined here — 146 patent families published between 2015 and 2026 — is deliberately narrow, cutting across jet and reaction propulsion (F02K), gas-turbine plants (F02C) and combustion chamber (F23R) classifications rather than the full universe of hypersonic vehicle art.

Filing activity rose from 10 families in 2017 to a peak of 17 in 2023, then eased back; 2026 figures are still partial because publication lags filing by roughly eighteen months, so the most recent bar in any trend chart understates real activity. The composition skews heavily toward core propulsion (F02K appears in 136 of 146 records) with peripheral disclosure in aircraft equipment, digital processing and even marine and spacecraft classes — evidence that scramjet-specific claims are increasingly being drafted alongside vehicle-integration and control-system content rather than in isolation.

Annual filings, 2017-2026 (partial)
  1. 1GENERAL ELECTRIC CO20
  2. 2HYPERSONIX IP HLDG INC9
  3. 3MITSUBISHI HEAVY IND LTD8
  4. 4LOCKHEED MARTIN CORP6
  5. 5BEIJING AEROSPACE TECH INST6
  6. 6BEIJING POWER MACHINERY INST6
  7. 7NAT UNIV OF DEFENSE TECH5
  8. 8HARBIN INST OF TECH5
  9. 9AEROJET ROCKETDYNE INC5
  10. 10AEROJET GENERAL CORP4
Source: Patsnap Eureka. Assignee ranking and totals. Derived from a Patsnap search on Scramjet and Hypersonic Propulsion 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 trend and technology composition

Two views of the same 146-family dataset: how filing volume has moved year over year, and which IPC subclasses carry the claim weight.

A plateau after a 2023 peak

Filings grew from 10 in 2017 to a high of 17 in 2023, roughly 70% growth over six years, but the 2022 midpoint of 6 shows the climb was uneven rather than steady. With 2026 still an open filing year, current data reads as flat-to-declining rather than confirming a new growth phase.

A plateau after a 2023 peak05101520102017201820192020202120221720232024202542026Most recent year is partial — publication lag means later filings are not yet visible.

F02K dominates; supporting classes are thin

F02K (jet and reaction propulsion) appears in 136 of 146 records, with F02C (gas-turbine plants, 42) and F23R (combustion chambers, 28) as the next-heaviest supporting classes. Aircraft equipment, digital processing, aeroplane, marine and spacecraft classes each register in single digits, indicating that most applicants file core propulsion claims and treat vehicle integration as a secondary disclosure rather than a primary claim target.

F02K dominates; supporting classes are thinF02K · Jet & reaction propulsion13693.2%F02C · Gas-turbine plants4228.8%F23R · Combustion chambers2819.2%B64D · Aircraft equipment85.5%G06F · Electric digital data processi…64.1%B64C · Aeroplanes & helicopters42.7%B63H · Marine propulsion & steering21.4%B64G · Cosmonautics & spacecraft21.4%Other2013.7%

Shares are the percentage of the 146 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 Scramjet and Hypersonic Propulsion 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 documents shaping this field's citation graph

Representative Recent Filing
US20240084764A12024-03-14

Hypersonic vehicle and scramjet engine with variable fuel injection for operation over a large Mach number range

HYPERSONIX IP HOLDINGS, INC.

Airframe-integrated scramjet engines configured to integrate with a hypersonic vehicle airframe, comprising a capture-shape inlet, a combustor for fuel-air combustion, and a nozzle exit shape for expansion of combusted fuel and air to provide hypersonic thrust. Disclosed embodiments include a fixed-geometry engine with a transitioning cross-sectional shape over its full length, configured as a component of a launch vehicle system.Filed by Hypersonix IP Holdings, Inc.; published 2024-03-14.

US20240084764A1 — patent drawing 1US20240084764A1 — patent drawing 2
View full filing
Most-cited records in the dataset
#Publication no.Patent titleCitations
1US3864907AStep cylinder combustor design51
2US4903480AHypersonic scramjet engine fuel injector44
3US4291533ASupersonic ramjet missile43
4US5085048AScramjet including integrated inlet and combustor35
5US5058826AScramjet engine having a low pressure combustion cycle30
6US8484980B1Dual-mode combustor29
7CN112431675A一种组合式的超燃冲压发动机冷却循环系统27
8US5660040AScramjet fuel injection system having independent fuel supplies for supersonic and hypersonic operation26
9US4986068AHypersonic scramjet engine fuel injector24
10CN107013367A涡轮基双燃烧室冲压组合循环发动机23

Citation counts accumulate over time and favour older records; treat this table as a map of foundational influence, not of which claims are strongest today.

Patent titles are shown in the language they were filed in, not translated, so that each record stays verifiable against the original filing — a translated title will not match in Eureka or in any national register. 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 Scramjet and Hypersonic Propulsion 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 filing strategy

Three patterns stand out once family counts, venue choice and co-filing are read together.

Filing Trend
17 in 2023
peak annual filings

Growth has stalled after a single strong year

Filings rose from 10 in 2017 to 17 in 2023 but the 2022 midpoint of 6 shows the path was uneven, and volumes have not sustained the 2023 peak. Anyone reading this as an accelerating field should weight the plateau at least as heavily as the peak.

Based on 146 published families, 2015-2026.
Venue Choice
48 US / 42 China
leading receiving offices

Filing strategy is a two-jurisdiction game

The US and China together account for the large majority of receiving-office activity, with Europe, India, Japan and the PCT route each trailing well behind. A defensive filing programme that skips either the US or China is leaving the two most active venues uncovered.

Receiving office counts across the full dataset.
Collaboration
2 pairs
co-assignee pairings found

Solo filing is the norm, not joint development

Only two co-assignee pairs appear across 146 families, and the strongest of them links two research institutes rather than a commercial partnership. Most patent positions here were built independently, which matters for anyone scouting for licensing or joint-venture partners.

Co-assignee pairs identified across the dataset.
Technology Mix
136 of 146
records touching F02K

Core propulsion claims dominate the corpus

F02K appears in 136 of 146 records, with F02C and F23R as the main supporting classes; aircraft equipment and digital-processing content appears in only a handful of filings. Vehicle-integration and control-software claims remain a comparatively open adjacent space.

IPC subclass counts, full dataset.
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 scramjet and hypersonic propulsion, 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 Scramjet and Hypersonic Propulsion 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 holds the ground, and where the momentum has gone quiet

The assignee list includes established propulsion primes and defence-linked research institutes; recent-year activity from the largest historical filers has gone quiet across the board.

Momentum Signal
0 in latest year
for the largest historical filers

Recent-year filing has gone quiet across the leaderboard

General Electric, Hypersonix IP Holdings, Mitsubishi Heavy Industries, United Technologies, Lockheed Martin and the Beijing Institute of Astronautical Systems Engineering all show zero filings in the latest tracked year. That is consistent with publication lag rather than withdrawal, but it means the visible leaderboard is built on older activity.

Recent-year momentum, top assignees by family count.
Institutional Filers
6 families
strongest co-assignee pairing

Chinese research institutes co-file more than commercial rivals

The strongest co-assignee link in the dataset pairs the Beijing Institute of Astronautical Systems Engineering with the Beijing Power Machinery Institute across six families, the densest joint-filing relationship found. Commercial assignees in the dataset largely file alone.

Strongest co-assignee pair by shared family count.
Long Tail
146 families
total in ranking

A long tail sits behind a small set of repeat filers

With only two co-assignee pairs found across the full set, most of the 146 families trace to single, independent assignees. That points to a field where a handful of institutional and corporate filers hold most of the depth, and the remainder is single-filing entrants staking narrow claims.

Assignee ranking, full dataset.
🔍
Under-claimed branches worth checking before filing
These sub-areas show thin representation relative to the core propulsion classes and are worth a freedom-to-operate check before drafting.
Variable-geometry inlet actuationActive thermal protection cooling loopsFuel-air mixing enhancement at hypersonic MachScramjet-to-turbine mode transition controlOnboard combustion diagnostics software
Rank all filers by momentum →
Recent-year filing momentum by assignee
AssigneeRecent yearYoY
General Electric Company0
HYPERSONIX IP HLDG INC0
Mitsubishi Heavy Industries, Ltd.0
United Technologies Corporation0
Lockheed Martin Corporation0
Beijing Institute of Astronautical Systems Engineering0
Beijing Power Machinery Institute0
Aerojet0
Source: Patsnap Eureka. Assignee-level momentum. Derived from a Patsnap search on Scramjet and Hypersonic Propulsion 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 filing record raises questions that a static landscape page cannot answer on its own.

Check freedom-to-operate against the cited core patents

The most-cited records in this dataset, several dating to the 1970s through 1990s, still anchor claim language that later filings build on. A freedom-to-operate review should start there rather than with recent filings alone.

Explore citation trees in Eureka

Track when the quiet assignees resume filing

Zero recent-year activity from the largest historical filers is consistent with publication lag, but the next 12-18 months of data will show whether that is a real slowdown or a reporting gap.

Set up filing alerts in Eureka

Map the under-claimed integration branches

Vehicle-integration and control-software content appears in only a handful of the 146 families. A deeper claim-chart pass on those adjacent classes could surface drafting room that core-propulsion searches miss.

Run a white space search in Eureka
Source: Patsnap Eureka. Forward-looking reading of the same dataset. Derived from a Patsnap search on Scramjet and Hypersonic Propulsion 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 scramjet and hypersonic propulsion patents

Answers are grounded in the same dataset. Derived from a Patsnap search on Scramjet and Hypersonic Propulsion 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.