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Run your analysis now →Filing growth compares 2021 (9 records) with 2024 (11) — 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 621 records in scope (CR5), not by the ranked leaders only.
Turbofan fan blade design sits at the intersection of aerodynamics, metallurgy and manufacturing process claims. The search set spans 621 records published between 2015 and mid-2026, built around the recurring technical anchors of hollow fan blade construction, wide-chord geometry, blade root and dovetail design, and the joining processes — diffusion bonding and superplastic forming — that turn those geometries into manufacturable parts. Filtering against flutter margin, bird-strike resistance and leading-edge sheath claims keeps the set tied to blades that must survive both aerodynamic loading and foreign-object impact, not generic turbine hardware.
The assignee ranking is unusually top-heavy: five companies account for 84.1% of all records in scope, and the top ten reach 96.9%. That leaves a genuine long tail of single- or low-filing entrants below rank ten, which matters more for freedom-to-operate checks than for identifying who sets the pace.
Publication lag means the most recent one to two years always understate real filing activity; treat 2025 and 2026 as still filling in rather than as a slowdown.
Filings ran from 13 in 2017 to a peak of 27 in 2018, then settled into a steadier band. The cleanest recent read is 2021 to 2024, where filings rose from 9 to 11 records — a 22% increase over that span, and the last stretch not yet thinned out by publication lag.
F01D (turbines and non-positive engines) touches 69.9% of the 621 records, confirming that most filings frame the blade as engine hardware rather than a standalone part. F04D (pumps) and B23P (general metal working) each cross a quarter of records, and the welding/brazing (B23K) and sheet-metal (B21D) classes, each around 15.5-15.8%, mark out the manufacturing-process side of the art as a distinct, heavily claimed track rather than an afterthought to the aerodynamic geometry claims.
Shares are the percentage of the 621 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 turbofan fan blade design and every answer comes back with the patent numbers behind it.
Try EurekaThe filing sets out a method for forming a hollow structure with varying mass distribution from two sheets of a diffusion-bondable, superplastic-formable material. A stop-off material blocks bonding at selected non-peripheral zones, an optional flat core sheet sits between the two outer sheets, and the assembly is first diffusion-bonded then superplastically formed to the contoured target shape.This is the process family underlying hollow wide-chord fan blade manufacture — the technique that let engine makers replace solid titanium blades with lighter hollow ones without losing the joint integrity needed to survive bird-strike loading.


| # | Publication no. | Patent title | Citations |
|---|---|---|---|
| 1 | US5141400A | Wide chord fan blade | 390 |
| 2 | US6039542A | Panel damped hybrid blade | 209 |
| 3 | US5785498A | Composite fan blade trailing edge reinforcement | 163 |
| 4 | US5725355A | Adhesive bonded fan blade | 136 |
| 5 | US4631092A | Method for heat treating cast titanium articles to improve their mechanical properties | 134 |
| 6 | US4882823A | Superplastic forming diffusion bonding process | 119 |
| 7 | EP0926312A2 | Damped turbomachine blade | 115 |
| 8 | US20110211965A1 | Hollow fan blade | 114 |
| 9 | US6669447B2 | Turbomachine blade | 109 |
| 10 | US6033186A | Frequency tuned hybrid blade | 107 |
Citation counts reward older filings that later art had to reference — read them as markers of influence on the field's vocabulary, not as a ranking of current commercial relevance.
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 read-throughs matter more than the raw counts: how concentrated the field is, how the manufacturing-process claims sit apart from the geometry claims, and where citation influence has settled.
With top-5 concentration at 84.1% of all 621 records and the top 10 reaching 96.9%, any new entrant is filing into a space where the dominant claim language is already established by a small group of engine OEMs. Freedom-to-operate work here is mostly a check against a short list, not a broad landscape scan.
Welding/brazing (B23K) and sheet-metal working (B21D) each sit around 15.5% of records — comparable weight to each other and distinct from the F01D aerodynamic-structure claims that dominate at 69.9%. Diffusion bonding and superplastic forming processes are claimed on their own terms, independent of the specific blade geometry they produce.
The most-cited record in the set, on wide-chord fan blade design, carries 390 citations — well ahead of the next tier. That reflects its role as an early reference point for later filings, not a signal that wide-chord claims are still the most active filing target today.
Eureka can read the same corpus for gaps instead of for coverage: under-claimed branches adjacent to turbofan fan blade design, with the prior art for and against each one.
The ranking covers 42 companies as returned by the data endpoint — not a top-50 or top-100 cut. Filing counts concentrate hard at the top, and momentum in the most recent tracked year has cooled across the leaders, consistent with publication lag rather than a real pullback.
The top-ranked assignee alone holds 168 of the 621 records in scope, more than the combined total of ranks six through 42. That scale reflects decades of continuation filing across successive fan blade generations rather than a single burst of activity.
Past the top ten, which together hold 96.9% of records, the remaining ranked companies each hold a small handful of filings. That long tail is where research institutes and specialist manufacturing houses sit, often filing around a single process innovation rather than a full blade platform.
Several leading assignees show sharply lower or zero filings in the latest tracked year. Given the roughly 18-month lag between filing and publication, this is expected thinning rather than evidence that engine OEMs have stopped filing in this area.
| Assignee | Recent year | YoY |
|---|---|---|
| Raytheon Technologies Corporation | 1 | -83% |
| United Technologies Corporation | 0 | — |
| Rolls-Royce plc | 0 | — |
| General Electric Company | 0 | -100% |
| SNECMA (Safran Aircraft Engines) | 0 | — |
| Aviadvigatel Open Joint Stock Company | 0 | — |
| Institute for Metals Superplasticity Problems of the Russian Academy of Sciences | 0 | — |
| Ufa Engine Industrial Association Joint Stock Company | 0 | — |
The dataset points to specific follow-up work rather than a single conclusion.
With 84.1% of records held by five assignees, a freedom-to-operate review should start with their dovetail, hollow-core and diffusion-bonding claim families before looking at the long tail.
Run a claim map in EurekaB23K and B21D claims form a track distinct from the aerodynamic geometry claims in F01D — treat process and structure as two separate landscapes when scoping new filings.
Explore process claims in EurekaPublication lag means the current tail understates real activity; a re-run against this same search string in a year will sharpen the 2024-2026 read.
Set up a monitoring search in EurekaOne assignee leads the ranked field with 168 of the 621 records in scope, well ahead of the next four, who together bring the top-five combined share to 84.1% of all records. This level of concentration is typical of jet-engine hardware, where a handful of OEMs have filed continuation patents across successive blade generations. Anyone assessing this space should treat the top five as the primary reference point and the remaining 37 ranked companies as a long tail of narrower, often single-process filings.
Hollow fan blade patents typically claim the internal structure and manufacturing process — most often diffusion bonding combined with superplastic forming — used to reduce blade weight while preserving strength. Wide-chord fan blade patents claim the external aerodynamic profile, a broader blade shape that improves efficiency and can itself benefit from a hollow internal structure. The two concepts are complementary in practice; many commercial fan blades combine a wide-chord profile with hollow internal construction, but the patent claims covering each aspect are usually filed and litigated separately.
The tracked trend shows filings climbing from 13 in 2017 to a peak of 27 in 2018 before settling into a steadier band in following years. The evidence available does not attribute a specific cause to that peak, and reading too much into a single year's spike is risky without matching it to specific product launch cycles at the major engine OEMs. The more reliable recent signal is the 2021-to-2024 span, where filings rose from 9 to 11 records, a 22% increase over three years not yet affected by publication lag.
US4882823A claims a specific superplastic forming and diffusion bonding process — using stop-off material to control where two or three sheets bond and where they instead deform to a contoured shape — rather than the concept of a hollow fan blade in general. A new design using a materially different joining process, sheet arrangement, or stop-off approach would sit outside its specific process claims. Any team pursuing a hollow blade via diffusion bonding should still have counsel review this filing's exact claim scope and family status before finalising a manufacturing process, since it is one of the most-cited records in this dataset.
Diffusion bonding and superplastic forming are the two process anchors built into this search, and they show up heavily inside the B23K (welding/brazing, 15.6% of the 621 records) and B21D (sheet-metal working, 15.5%) IPC classes. B23P, general metal working, is broader still at 28.0% of records. Together these process classes represent a claim space that sits apart from the aerodynamic structure claims concentrated in F01D, meaning a manufacturing-process innovation can often be claimed and defended independently of the blade geometry it produces.
Go past this page: query the whole turbofan fan blade design 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.