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The agent works the prompt against patents and technical literature, citing every source.
Run your analysis now →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.
Two views of the same 146-family dataset: how filing volume has moved year over year, and which IPC subclasses carry the claim weight.
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.
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.
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%.
This page is one run against one query. Ask Eureka your own question about scramjet and hypersonic propulsion and every answer comes back with the patent numbers behind it.
Try EurekaAirframe-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.


| # | Publication no. | Patent title | Citations |
|---|---|---|---|
| 1 | US3864907A | Step cylinder combustor design | 51 |
| 2 | US4903480A | Hypersonic scramjet engine fuel injector | 44 |
| 3 | US4291533A | Supersonic ramjet missile | 43 |
| 4 | US5085048A | Scramjet including integrated inlet and combustor | 35 |
| 5 | US5058826A | Scramjet engine having a low pressure combustion cycle | 30 |
| 6 | US8484980B1 | Dual-mode combustor | 29 |
| 7 | CN112431675A | 一种组合式的超燃冲压发动机冷却循环系统 | 27 |
| 8 | US5660040A | Scramjet fuel injection system having independent fuel supplies for supersonic and hypersonic operation | 26 |
| 9 | US4986068A | Hypersonic scramjet engine fuel injector | 24 |
| 10 | CN107013367A | 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.
When you want the answer in the next five minutes.
The agent works the prompt against patents and technical literature, citing every source.
Run your analysis now →When it has to run inside your own pipeline.
Patent search, landscape analysis and assignee resolution as MCP tools. Drop them into any agent framework, or call REST directly.
Browse MCP servers →Three patterns stand out once family counts, venue choice and co-filing are read together.
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.
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.
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.
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.
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.
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.
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.
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.
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 | Recent year | YoY |
|---|---|---|
| General Electric Company | 0 | — |
| HYPERSONIX IP HLDG INC | 0 | — |
| Mitsubishi Heavy Industries, Ltd. | 0 | — |
| United Technologies Corporation | 0 | — |
| Lockheed Martin Corporation | 0 | — |
| Beijing Institute of Astronautical Systems Engineering | 0 | — |
| Beijing Power Machinery Institute | 0 | — |
| Aerojet | 0 | — |
The filing record raises questions that a static landscape page cannot answer on its own.
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 EurekaZero 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 EurekaVehicle-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 EurekaThe dataset's assignee ranking is led by a mix of established propulsion primes and defence-linked research institutes, including corporate names like General Electric, Mitsubishi Heavy Industries, United Technologies and Lockheed Martin alongside Chinese institutes such as the Beijing Institute of Astronautical Systems Engineering. Notably, every one of these leading assignees shows zero filings in the most recent tracked year, which given an 18-month publication lag likely reflects reporting delay rather than an actual halt in R&D. Anyone using this ranking for competitive tracking should treat it as a picture of historical depth rather than current-year activity.
Filings rose from 10 in 2017 to a peak of 17 in 2023, but the path was uneven — the 2022 midpoint sat at just 6 — and volumes have not held at the 2023 peak since. That pattern reads as a plateau rather than sustained growth. Because the 2026 figures are still incomplete due to publication lag, it is too early to call the recent dip a genuine decline, but there is no clear evidence of accelerating filing activity either.
The United States and China are the two dominant receiving offices, with 48 and 42 filings respectively, far ahead of Europe (14), India (10), Japan (6) and the PCT route (5). This concentration means most substantive claim positions in this field are being tested in US and Chinese patent offices first. A company building a defensive or freedom-to-operate strategy in hypersonic propulsion should prioritise searches in those two jurisdictions before extending to Europe or Japan.
Core propulsion claims under F02K dominate the corpus, appearing in 136 of 146 records, while adjacent areas like variable-geometry inlet actuation, active thermal protection cooling loops, and mode-transition control between scramjet and turbine operation appear far less often. Aircraft equipment and digital-processing content together account for only a small fraction of filings. That gap suggests vehicle-integration and control-software claims around scramjet propulsion remain comparatively under-claimed relative to the combustion and inlet hardware itself.
Collaboration is rare in this dataset: only two co-assignee pairs were identified across 146 patent families. The strongest pairing links two Chinese research institutes, the Beijing Institute of Astronautical Systems Engineering and the Beijing Power Machinery Institute, across six shared families, while a second pair appears only once. This means most patent positions in scramjet propulsion, whether held by corporations or institutes, were developed and filed independently rather than through joint ventures or cross-licensing arrangements visible in the co-filing record.
Go past this page: query the whole scramjet and hypersonic propulsion corpus yourself, in your own scope.
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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.